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0.0172
GENERALOCT 08 001
TABLE OF CONTENTS
0 GENERAL
1 EMERGENCY PROCEDURES
2 PROCEDURES FOLLOWING FAILURES
3 NORMAL PROCEDURES
4 OPS DATA
5 MANAGEMENT PAGES
6 NORMAL CHECK LIST
COMMENTS ON PARTS 1 AND 2
LAYOUT
RThe boxed items correspond to actions performed by memory by thecrew within a minimum period of time
: highlights a precondition to apply an action
: highlights the moment when an action is to be applied
PROCEDURES INITIATION
No action will be taken (apart from depressing MC/MW pushbutton) :
RR
- until flight path is stabilized- under 400 ft above runway, except propeller feathering after enginefailure during approach at reduced power if go around is considered
RRR
At flight crew discretion, one reset of a system failure associated withan amber caution (except PEC SGL CH) may be performed byselecting OFF then ON related pushbutton.
Flight Crew may reengage a tripped circuit breaker only if he/shejudges it necessary for a safe continuation of the flight. In this caseonly one reengagement should be attempted.
If the failure alert disappears, continue normal operation and recordthe event in the maintenance log. If not, apply the associated failureprocedure.
Before performing a procedure, the crew must assess the situation asa whole, taking into consideration the failures, when fully identified,and the flight constraints imposed.
TASK SHARING
For all procedures, the general task sharing stated below isapplicable. The pilot flying remains pilot flying throughout theprocedure.
PF, Pilot Flying, responsible for :- PL- flight path and airspeed control- aircraft configuration- navigation
PNF, Pilot Non Flying, responsiblefor :
- Check List reading- execution of required actions- actions on OVHD panel- CL- communications
The AFCS is always coupled to the PF side (CPL selection)
ANALYSIS OF CONSEQUENCES OF A FAILURE ON FLIGHT
Basic airmanship calls for a management review of the remainingaircraft capabilities under the responsibility of CM1.
EM
ER
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NC
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1.01
72
EMERGENCY SEP 07 001
1 - EMERGENCY PROCEDURES Content 1/1 IN FLIGHT ENG FIRE OR SEVERE MECHANICAL DAMAGE 1.02
R ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE 1.02 ON GROUND EMER EVACUATION 1.02 BOTH ENGINES FLAME OUT 1.03
ENG FLAME OUT AT TAKE OFF 1.04 BOMB ON BOARD 1.04
COCKPIT DOOR SECURITY SYSTEM 1.04A R SMOKE 1.05 R ELECTRICAL SMK 1.05A R AIR COND SMOKE 1.05A FWD SMK 1.06 AFT SMK 1.06
R AUX AFT COMPT SMK 1.06 DUAL DC GEN LOSS 1.07
R EMERGENCY DESCENT 1.07A DITCHING 1.08 FORCED LANDING 1.08A SEVERE ICING 1.09
1.02
72
EMERGENCY SEP 07 001
IN FLIGHT ENG FIRE
OR SEVERE MECHANICAL DAMAGE
PL affected side .................................................................................. FI CL affected side .................................................. FTR THEN FUEL SO FIRE HANDLE affected side..........................................................PULL
After 10 seconds FIRST AGENT affected side.................................................. DISCH
If fire after further 30 seconds SECOND AGENT affected side ............................................ DISCH LAND ASAP SINGLE ENG OPERATION procedure (2.04)............................APPLY
ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE
PL 1 + 2............................................................GI / REVERSE AS RQD
When aircraft stopped PARKING BRAKE ............................................................. ENGAGE CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLE affected side ....................................................PULL FIRST AGENT affected side.................................................. DISCH If fire after further 30 seconds SECOND AGENT affected side ........................................ DISCH If evacuation required ON GROUND EMER EVACUATION procedure (1.02) ...APPLY
ON GROUND EMER EVACUATION
AIRCRAFT / PARKING BRAKE ................................ STOP / ENGAGE ATC (VHF 1) ............................................................................. NOTIFY CL 1 + 2 ............................................................... FTR THEN FUEL SO MIN CAB LIGHT ............................................................................... ON CABIN CREW (PA)................................................................... NOTIFY FIRE HANDLES 1 + 2....................................................................PULL AGENTS ...................................................................................AS RQD ENG START ROTARY SELECTOR...................OFF / START ABORT FUEL PUMPS 1 + 2........................................................................ OFF EVACUATION (PA) .................................................................INITIATE
Before leaving aircraft BAT ............................................................................................ OFF
1.03
72
EMERGENCY SEP 07 100
BOTH ENGINES FLAME OUT
PL 1 + 2............................................................................................... FI
If NH drops below 30 % (no automatic relight) CL 1 + 2 .......................................................... FTR THEN FUEL SO FUEL SUPPLY .....................................................................CHECK OPTIMUM SPEED.................................................................. VmHB CAPT EHSI................................................................................ OFF COMMUNICATIONS .............................................................. VHF 1 ENG START ROTARY SELECTOR........................... START A & B
ENG 2 RELIGHT ENG 2 START PB .................................................................. ON When NH above 10 % CL 2 ..................................................................................FTR ENG 2 RELIGHT ....................................................MONITOR CL 2 then PL 2...........................................................AS RQD
ENG 1 RELIGHT ENG 1 START PB .................................................................. ON When NH above 10 % CL 1 ..................................................................................FTR ENG 1 RELIGHT ....................................................MONITOR CL 1 then PL 1...........................................................AS RQD
If neither engine starts CL 1 + 2 .......................................................... FTR THEN FUEL SO ENG START ROTARY SELECTOR..............OFF / START ABORT FUEL PUMPS 1 + 2................................................................... OFF FORCED LANDING (1.08A) or DITCHING (1.08) procedure ........... ...............................................................................................APPLY
CAUTION: Do not select AVIONICS VENT EXHAUST MODE to OVBD
If engine(s) recovered CL / PL engine(s) recovered................................................AS RQD If one engine not recovered CL engine NON recovered ........................ FTR THEN FUEL SO SYSTEMS affected.......................................................... RESTORE
Mod : 3973 or 4371 or 4457
1.04
72
EMERGENCY SEP 07 030
ENG FLAME OUT AT TAKE OFF
UPTRIM .....................................................................................CHECK
If no UPTRIM PL 1 + 2 ................................................. ADVANCE TO THE RAMP AUTOFEATHER ........................................................................CHECK
Above 400 ft AGL PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO
If damage suspected FIRE HANDLE affected side ....................................................PULL SINGLE ENG OPERATION procedure (2.04).......................APPLY
If no damage suspected ENG RESTART IN FLIGHT procedure (2.08) .......................APPLY If unsuccessful SINGLE ENG OPERATION procedure (2.04)..................APPLY
BOMB ON BOARD
AUTO PRESS - LANDING ELEVATION .................. CABIN ALTITUDE FLIGHT LEVEL................................ DESCEND TO CABIN ALTITUDE AVOID LOAD FACTORS HANDLE BOMB CAREFULLY - AVOID SHOCKS
When Z aircraft = Z cabin APPROACH CONFIG: FLAPS 15 GEAR DOWN ......... SELECTED AUTO PRESS.........................................................................DUMP SERVICE DOOR ................................................................UNLOCK PLACE BOMB NEAR SERVICE DOOR PREFERABLY IN A BAG ATTACHED TO THE DOOR HANDLE SURROUND IT WITH DAMPING MATERIAL CABIN ATTENDANT OXYGEN AND FIRE EXTINGUISHER........... ............................................................................ MOVE FORWARD PAX................................... MOVE FORWARD / CRASH POSITION LAND ASAP
Mod : 4111
1.05A72
EMERGENCYSEP 10 001
ELECTRICAL SMOKE
SMOKE procedure (1.05) ...........................................................APPLYAVIONICS VENT EXHAUST MODE ........................................... OVBDAIR FLOW......................................................................................HIGHDC SVCE AND UTLY BUS............................................................. OFFDC BTC.......................................................................................... ISOLACW GEN 1 + 2.............................................................................. OFFSUSPECTED EQUIPMENTS......................................................... OFF
If smoke origin not identifiedLAND ASAPACW TOTAL LOSS procedure (2.16A) .................................APPLY
If smoke origin identifiedNOT AFFECTED EQUIPMENTS .................................... RESTORE
When P < 1 PSIOVBD VALVE ................................................................FULL OPENAVIONICS VENT EXHAUST MODE......................................NORM
AIR COND SMOKE
R
SMOKE procedure (1.05) ...........................................................APPLYPACK VALVE 1............................................................................... OFFMAX FL ..................................................................................200 / MEA
If smoke persistsPACK VALVE 1 ........................................................................... ONPACK VALVE 2 ......................................................................... OFFCAUTION: Evacuation of air conditioning smoke may trigger
electrical smoke warning. Disregard it.ENGINES PARAMETERS......................... CAREFULLY MONITOR
If any anomaly occurs, such as:- amber engine caution illumination associated to local ITT alert- total loss of NL indication- engine abnormality clearly identified (NH, NL, ITT indications,
noise, surge…)
CAUTION: Confirm which engine is showing signs of abnormaloperation in order to avoid shutting down safe engine.
PL affected side ............................................................................. FICL affected side.............................................. FTR THEN FUEL SOSINGLE ENG OPERATION procedure (2.04).......................APPLY
1.0972
EMERGENCYSEP 04 001
SEVERE ICINGR
MINIMUM ICING SPEED ............................ INCREASE RED BUG by 10 ktPWR MGT .......................................................................................... MCTCL / PL ................................................................................... 100% / MCTAP (if engaged).......FIRMLY HOLD CONTROL WHEEL and DISENGAGESEVERE ICING CONDITIONS .....................................................ESCAPEATC...............................................................................................NOTIFY
n If an unusual roll response or uncommanded roll controlmovement is observed :
Push firmly on the control wheel FLAPS ..................................................................................... 15
n If the flaps are extended, do not retract them until the airframe isclear of ice.
n If the aircraft is not clear of ice :GPWS..........................................................FLAP/GPWS OVRDSTEEP SLOPE APPROACH (≥4.5°).......................PROHIBITEDAPP/LDG CONF.........................................MAINTAIN FLAPS 15
with "REDUCED FLAPS APP/LDG icing speeds" + 5 ktMultiply landing distance FLAPS 30 by 1.91.
DETECTIONVisual cue identifying severe icing is characterized by ice covering all or asubstantial part of the unheated portion of either side window
and / orUnexpected decrease in speed or rate of climb
and / orThe following secondary indications :. Water splashing and streaming on the windshield. Unusually extensive ice accreted on the airframe in areas not normally
observed to collect ice. Accumulation of ice on the lower surface of the wing aft of the protected
areas. Accumulation of ice on propeller spinner farther aft than normally
observed
The following weather conditions may be conducive to severe in-flighticing :. Visible rain at temperatures close to 0°C ambient air temperature (SAT). Droplets that splash or splatter on impact at temperatures close to 0°C
ambient air temperature (SAT)
Eng : PW124
1.10
72
EMERGENCY MAY 11 050
RECOVERY AFTER STALL or ABNORMAL ROLL CONTROL
CONTROL WHEEL........................................................ PUSH FIRMLY
If flaps 0° configuration FLAPS........................................................................................... 15° PWR MGT...................................................................................MCT CL / PL ........................................................................... 100% / MCT ATC ....................................................................................... NOTIFY If flaps are extended PWR MGT...................................................................................MCT CL / PL ........................................................................... 100% / MCT ATC ....................................................................................... NOTIFY
Note: this procedure is applicable whatever the LDG GEAR position is
(DOWN or UP)
RR UNRELIABLE AIRSPEED INDICATION
R
AP/YD/FD BARS .............................................................. OFF/OFF/STBY
PITCH AND TQ......................................................................... MAINTAIN If at take off or GA below 1500 ft:
PITCH IMMEDIATELY........................................................................8°
ICING / VOLCANIC ASHES CONDITIONS.................................ESCAPE PROBE HEATING, DE-/ANTI-ICING...................................... CHECK ON APM..................................................................................................... OFF
WARNING: respect STALL alarm. Note: Use any GPS speed information if available.
Take off phase, at or above acceleration altitude ALTITUDE.................................... MAINTAIN AT LEAST 30 SECONDS FLAPS..................................................................................................0° PITCH ..................................................................................................8° Note: Use climb table here after to adjust pitch if required. AFTER TAKE OFF normal procedure .........................................APPLY LAND AT THE NEAREST SUITABLE AIRPORT
Climb TLU ............................................................................................ LO SPD PWR MGT........................................................................................ CLB PL 1 + 2.......................................................................................NOTCH
Altitude (ft) 5000 10000 15000 20000 Normal conditions pitch 7° 5° 4° 3° Icing conditions pitch 6° 4° 3° 2°
Continuing next page …/…
Mod : 3973 or 4371 or 4457 Eng : PW124
1.11
72
EMERGENCY MAY 11 050
UNRELIABLE AIRSPEED INDICATION (CONT’D)
Cruise
ALTITUDE ............................................................................... MAINTAIN TLU............................................................................................... HI SPD Note: Average pitch around 0° at cruise speed PWR MGT .........................................................................................CRZ PL 1 + 2 ........................................................................................NOTCH
Descent TLU............................................................................................... HI SPD PITCH........................................................................MAINTAIN AT -2.5° PL 1 + 2 ........................................................................ ADJUST 30% TQ DESCENT normal procedure ........................................................APPLY
Initial Approach TLU.............................................................................................. LO SPD APPROACH normal procedure .....................................................APPLY CAUTION: Transition from clean configuration to LDG configuration is to be performed in level flight - REFER TO ALTIMETER - (if possible 30 seconds between each step). Note: Refer to following tables to adjust TQ:
TQ (Altitude of 3000ft) Aircraft configuration
- Average speed 14 T
18 T
22 T
Flaps 0° - 180 kt 45% 45% 50% FLAPS .................................................................................................15°
Flaps 15° - 150 kt 40% 40% 45% LDG GEAR ....................................................................................DOWN PWR MGT ........................................................................................... TO FLAPS .................................................................................................30°
Flaps 30° - 130 kt 45% 45% 50%
Final Approach PL 1 + 2 ........................................................................ ADJUST 35% TQ BEFORE LANDING normal procedure .........................................APPLY Note: Set an average pitch of -5° for a 3° slope approach.
Mod : 3973 or 4371 or 4457 Eng : PW124
1.04A72
EMERGENCYSEP 04 200
COCKPIT DOOR SECURITY SYSTEM
RRRRRRRR
Electrical Power LostMove the manual lock bolts to CLOSE positionNote : When the door is locked with the manual bolts, the
emergency access to the cockpit is unavailable. It isrecommended that at least two crew members remain inthe cockpit during that time.
Cockpit Door Jammed
l When cockpit exit requiredRemove the inspection seals from the two latches of the door left
panel (facing the door)Actuate the two corresponding latches as per placardsCOCKPIT DOOR LOCKING SYSTEM ............................... OFFDisconnect PLUG from the doorPush and remove corresponding door panel
Mod : 5377 + (5434 or 8330)
1.05
72
EMERGENCY SEP 07 001
SMOKE
CREW OXY MASKS.............................................................ON / 100% GOGGLES................................................................................AS RQD CREW COMMUNICATIONS ..............................................ESTABLISH RECIRC FANS 1 + 2 ...................................................................... OFF AP ..................................................................................................... ON SMOKE SOURCE.................................................................. IDENTIFY
If source not identified or electrical smoke suspected Note: ELEC light may be activated by an air conditioning smoke source ELECTRICAL SMOKE procedure (1.05A) ............................APPLY
If air conditioning smoke identified AIR COND SMOKE procedure (1.05A) .................................APPLY
If FWD SMK illuminated or smoke in FWD zone of aircraft FWD SMOKE procedure (1.06).............................................APPLY
If AFT SMK illuminated or smoke in AFT zone of aircraft AFT SMOKE procedure (1.06) ..............................................APPLY
If AUX AFT COMPT SMK illuminated (depending on models) AUX AFT COMPT SMK procedure (1.06) .............................APPLY
1.05A
72
EMERGENCY SEP 07 001
ELECTRICAL SMOKE
AVIONICS VENT EXHAUST MODE ........................................... OVBD AIR FLOW......................................................................................HIGH DC SVCE AND UTLY BUS............................................................. OFF DC BTC.......................................................................................... ISOL ACW GEN 1 + 2.............................................................................. OFF SUSPECTED EQUIPMENTS......................................................... OFF
If smoke origin not identified LAND ASAP ACW TOTAL LOSS procedure (2.16) ...................................APPLY
If smoke origin identified NOT AFFECTED EQUIPMENTS .................................... RESTORE
When ΔP < 1 PSI OVBD VALVE ............................................................... FULL OPEN AVIONICS VENT EXHAUST MODE......................................NORM
AIR COND SMOKE
PACK VALVE 1............................................................................... OFF MAX FL ..................................................................................200 / MEA
If smoke persists PACK VALVE 1 ........................................................................... ON PACK VALVE 2 ......................................................................... OFF CAUTION: Evacuation of air conditioning smoke may trigger
electrical smoke warning. Disregard it. ENGINES PARAMETERS......................... CAREFULLY MONITOR
If any anomaly occurs, such as: - amber engine warning illumination associated to local ITT alert - total loss of NL indication - engine abnormality clearly identified (NH, NL, ITT indications,
noise, surge…) WARNING: Confirm which engine is showing signs of abnormal
operation in order to avoid shutting down safe engine. PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY
1.06
72
EMERGENCY SEP 07 002
FWD SMK
1) PASSENGERS VERSION CABIN CREW (PA).............................................................. ADVISE AVIONICS VENT EXHAUST MODE...................................... OVBD AIR FLOW ................................................................................HIGH EXTRACT AIR FLOW LEVER (RH MAINT PANEL)..........CLOSED CABIN CREW WITH PORTABLE EXTINGUISHER, LOCATE AND KILL SOURCE OF SMOKE When ΔP < 1 PSI OVBD VALVE.......................................................... FULL OPEN AVIONICS VENT EXHAUST MODE.................................NORM
2) CARGO VERSION CAB PRESS MODE SEL...........................................................MAN CAB ALT................................................................ MAX INCREASE ENG 2 BLEED (Except when in single bleed operation)........... OFF PACK VALVE 2 (Except when in single pack operation) .......... OFF CAB VENT AIR FLOW .............................................................. OFF FLIGHT COMPT TEMP SEL .....................................................HOT
CAUTION: LAND ASAP. If a quick landing is not possible, climb and maintain minimum FL160; FL200 is recommended.
Note: Smoke alert may be generated during smoke evacuation process.
AFT SMK
1) PASSENGERS VERSION CABIN CREW (PA).......................................ADVISE FOR ACTION AIR FLOW ................................................................................HIGH
2) CARGO VERSION CAB PRESS MODE SEL...........................................................MAN CAB ALT................................................................ MAX INCREASE ENG 2 BLEED (Except when in single bleed operation)........... OFF PACK VALVE 2 (Except when in single pack operation) .......... OFF CAB VENT AIR FLOW .............................................................. OFF FLIGHT COMPT TEMP SEL .....................................................HOT
CAUTION: LAND ASAP. If a quick landing is not possible, climb and maintain minimum FL160; FL200 is recommended.
Note: Smoke alert may be generated during smoke evacuation process.
AUX AFT COMPT SMK (depending on models)
AUX AFT COMPT AGENT ......................................................... DISCH
Model : 102-202-212-212A
1.07
72
EMERGENCY OCT 08 001
DUAL DC GEN LOSS
R R
DC GEN 1 + 2...................................................................OFF then ON
If no generator recovered LAND ASAP MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN AVIONICS VENT EXHAUST MODE...................................... OVBD BAT SW .................................................................................. OVRD CAPT EHSI................................................................................ OFF ATC (VHF 1 or HF or HF 2) ................................................. NOTIFY MIN CAB LIGHT ........................................................................ OFF Note: NAV lights switch set to ON is necessary to provide IEP
illumination STICK PUSHER / SHAKER ...................................................... OFF STICK PUSHER / SHAKER FAULT procedure (2.21) ..........APPLY SIDE WINDOWS ANTI-ICING................................................... OFF HF (If installed) .......................................................................... OFF ADC SW....................................................................SET TO ADC 1 ATC SW.................................................................... SET TO ATC 1 TLU ................................................................. MAN MODE LO SPD When TLU LO SPD illuminates TLU.....................................................................................AUTO
CAUTION: Avoid large rudder input if IAS above 180 kt MAIN BATTERY CHARGE (on LH maintenance panel) ......CHECK BUS EQUIPMENT LISTS.....................................................CHECK If STBY BUS UNDV light illuminates STBY BUS...............For approach, OVRD only when necessary Before descent PAX INSTRUCTIONS .................................................... USE PA HYD X FEED .......................................................................... ON
Note: Selecting HYD X FEED ON allows to recover green hydraulic system
At touch down IDLE GATE LEVER .............................................................PULL
1.07A
72
EMERGENCY SEP 07 100
EMERGENCY DESCENT
OXYGEN MASKS / CREW COMMUNICATIONS ....................AS RQD GOOGLES................................................................................AS RQD DESCENT................................................................................INITIATE PL 1 + 2............................................................................................... FI CL 1 + 2 .............................................................................100% OVRD
OXYGEN PAX SUPPLY ...........................................................AS RQD SPEED........... MMO / VMO (or less if structural damage is suspected) SIGNS............................................................................................... ON ATC........................................................................................... NOTIFY MEA ...........................................................................................CHECK
Mod : 3973 or 4371 or 4457
1.08
72
EMERGENCY SEP 07 001
DITCHING
Preparation (time permitting) ATC (VHF1 or HF or HF2) ................................................... NOTIFY CABIN CREW (PA).............................................................. NOTIFY SIGNS.......................................................................................... ON GPWS........................................................................................ OFF TERR (If Enhanced GPWS installed) ........................................ OFF CABIN AND COCKPIT .................................................... PREPARE
- Loose equipment secured - Survival equipment prepared - belts and shoulder harnesses locked
AUTO PRESS - LDG ELEVATION.............................................SET Approach
If ΔP≠0 AUTO PRESS.....................................................................DUMP PACKS 1 + 2.............................................................................. OFF OVBD VALVE ............................................................. FULL CLOSE FLAPS (If available).......................................................................30 LDG GEAR LEVER ......................................................................UP
30 seconds before impact or 1250 ft above sea level DITCH PB .................................................................................... ON ENG START ROTARY SELECTOR..............OFF / START ABORT CABIN REPORT............................................................. OBTAINED
Before ditching (200 ft) MINIMIZE IMPACT SLOPE OPTIMAL PITCH ATTITUDE FOR IMPACT ................................. 9° BRACE FOR IMPACT ..........................................................ORDER CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLES 1 + 2 ..............................................................PULL FUEL PUMPS 1 + 2................................................................... OFF
Note: In case of night ditching, shutting down both engines may be performed at captain discretion, immediately after the impact (avoiding loss of landing lights during flare out).
After ditching Note: After ditching, one aft door will be under the water line. CABIN CREW (PA).............................................................. NOTIFY EVACUATION ....................................................................INITIATE Before leaving aircraft BAT........................................................................................ OFF
1.08A
72
EMERGENCY SEP 07 001
FORCED LANDING
Preparation (time permitting)
ATC (VHF1 or HF or HF2) ................................................... NOTIFY CABIN CREW (PA).............................................................. NOTIFY SIGNS.......................................................................................... ON GPWS........................................................................................ OFF TERR (If Enhanced GPWS installed) ........................................ OFF CABIN AND COCKPIT .................................................... PREPARE
- loose equipment secured - survival equipment prepared - belts and shoulder harnesses locked
AUTO PRESS - LDG ELEVATION.............................................SET
Approach FLAPS (If available).......................................................................30 LDG GEAR LEVER .............................................................AS RQD AUTO PRESS.........................................................................DUMP ENG START ROTARY SELECTOR..............OFF / START ABORT CABIN REPORT............................................................. OBTAINED
Before impact (200 ft) BRACE FOR IMPACT ..........................................................ORDER CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLES 1 + 2 ..............................................................PULL FUEL PUMPS 1 + 2................................................................... OFF
Note: In case of night forced landing, shutting down both engines may be performed at captain discretion, immediately after the impact (avoiding loss of landing lights during flare out).
After impact, when aircraft stopped CABIN CREW (PA).............................................................. NOTIFY AGENTS ................................................................................ DISCH EVACUATION ....................................................................INITIATE Before leaving aircraft BAT........................................................................................ OFF
1.0972
EMERGENCYSEP 04 001
SEVERE ICINGR
MINIMUM ICING SPEED ............................ INCREASE RED BUG by 10 ktPWR MGT .......................................................................................... MCTCL / PL ................................................................................... 100% / MCTAP (if engaged).......FIRMLY HOLD CONTROL WHEEL and DISENGAGESEVERE ICING CONDITIONS .....................................................ESCAPEATC...............................................................................................NOTIFY
n If an unusual roll response or uncommanded roll controlmovement is observed :
Push firmly on the control wheel FLAPS ..................................................................................... 15
n If the flaps are extended, do not retract them until the airframe isclear of ice.
n If the aircraft is not clear of ice :GPWS..........................................................FLAP/GPWS OVRDSTEEP SLOPE APPROACH (≥4.5°).......................PROHIBITEDAPP/LDG CONF.........................................MAINTAIN FLAPS 15
with "REDUCED FLAPS APP/LDG icing speeds" + 5 ktMultiply landing distance FLAPS 30 by 1.91.
DETECTIONVisual cue identifying severe icing is characterized by ice covering all or asubstantial part of the unheated portion of either side window
and / orUnexpected decrease in speed or rate of climb
and / orThe following secondary indications :. Water splashing and streaming on the windshield. Unusually extensive ice accreted on the airframe in areas not normally
observed to collect ice. Accumulation of ice on the lower surface of the wing aft of the protected
areas. Accumulation of ice on propeller spinner farther aft than normally
observed
The following weather conditions may be conducive to severe in-flighticing :. Visible rain at temperatures close to 0°C ambient air temperature (SAT). Droplets that splash or splatter on impact at temperatures close to 0°C
ambient air temperature (SAT)
Eng : PW124
FOLL
OW
ING
PR
OC
ED
UR
ES
2.0172
FOLLOWING FAILURESSEP 10 001
2 - PROCEDURES FOLLOWING FAILURESContent 1/3
POWER PLANTSINGLE ENG OPERATION………………………………………………………. 2.04START FAULT……………………………………………………………………... 2.04X START FAIL……………………………………………………………………… 2.04ABNORMAL PARAMETERS DURING START………………………………… 2.05EXCESSIVE ITT DURING START………………………………………………. 2.05NO ITT DURING START………………………………………………………….. 2.05NO NH DURING START………………………………………………………….. 2.05
R ENG NAC OVHT 2.06ABNORMAL ENG PARAMETERS IN FLIGHT………………………………… 2.06FIRE LOOP FAULT……………………………………………………………….. 2.06ABNORMAL PROP BRK…………………………………………………………. 2.07ENG RESTART IN FLIGHT………………………………………………………. 2.08ENG STALL………………………………………………………………………… 2.08ONE EEC FAULT………………………………………………………………….. 2.09BOTH EEC FAULT………………………………………………………………… 2.09ENG FLAME OUT…………………………………………………………………. 2.10IDLE GATE FAIL…………………………………………………………………… 2.10SYNPHR FAIL (if applicable) ……………………………………………………. 2.10ACL PNEUMATIC ACTUATOR BLOCKING (if applicable) ……………………. 2.10A
R UNCOMMANDED 100% NP ON ONE OR TWO PROPELLERS (if applicable) …………… 2.10APEC SGL CH (if applicable) ……………………………………………………… 2.10APEC FAULT (if applicable) ……………………………………………………….. 2.10ALO PITCH IN FLIGHT……………………………………………………………... 2.11ENG OVER LIMIT…………………………………………………………………. 2.11PROP OVER LIMIT……………………………………………………………….. 2.11ENG OIL TEMP BELOW 45°C…………………………………………………… 2.12ENG OIL TEMP HIGH…………………………………………………………….. 2.12ENG OIL LO PR……………………………………………………………………. 2.12ENG BOOST FAULT (if applicable) …………………………………………….. 2.12A
FUELFUEL ABNORMAL TEMP………………………………………………………… 2.13FUEL CLOG………………………………………………………………………… 2.13FEED LO PR……………………………………………………………………….. 2.13FUEL LEAK ALERT CONDITION……………………………………………….. 2.14FUEL LO LVL………………………………………………………………………. 2.14FUEL LEAK………………………………………………………………………… 2.14
ELECDC BUS 1 OFF ……………………………………………………………………. 2.15AC BUS 1 OFF ……………………………………………………………………. 2.15DC BUS 2 OFF ……………………………………………………………………. 2.15AAC BUS 2 OFF ……………………………………………………………………. 2.15AACW BUS 1 OFF / ACW BUS 2 OFF…………………………………………… 2.16ACW TOTAL LOSS……………………………………………………………….. 2.16ADC ESS BUS OFF………………………………………………………………… 2.17DC EMER BUS OFF………………………………………………………………. 2.17DC GEN FAULT……………………………………………………………………. 2.18INV FAULT…………………………………………………………………………. 2.18ACW GEN FAULT…………………………………………………………………. 2.18DC SVCE/UTLY BUS SHED……………………………………………………… 2.18BAT CHG FAULT………………………………………………………………….. 2.18DUAL BAT CHG LOSS……………………………………………………………. 2.18BAT DISCHARGE IN FLIGHT (if applicable) …………………………………... 2.18
STBY BUSSES AND BAT ONLY LOST EQUIPMENT LISTS………………...2.18A2.18B
ESS BUS AND EMER BUS LOST EQUIPMENT LISTS……………………….Cargo configuration only…..
2.422.42A
2.02
72
FOLLOWING FAILURES OCT 08 001
2 - PROCEDURES FOLLOWING FAILURES Content 2/3 HYDRAULIC HYD LO LVL 2.19 BOTH MAIN HYD PUMPS LOSS 2.19 BOTH HYD SYS LOSS 2.20 HYD LO PR / HYD OVHT 2.20 FLIGHT CONTROL FLAPS UNLK 2.21 FLAPS JAM / UNCOUPLED / ASYM 2.21 REDUCED FLAPS LANDING 2.21
R STICK PUSHER / SHAKER FAULT 2.21 PITCH TRIM ASYM (LOCAL LIGHT) 2.22 PITCH TRIM INOPERATIVE 2.22 RUDDER RELEASABLE CENTER UNIT FAIL 2.22 PITCH DISCONNECT 2.22
R PITCH RECONNECTION ON GROUND (If applicable) 2.22A TLU FAULT 2.22A AIL LOCK LIT (if applicable) 2.22A ELEVATOR JAM 2.23 AILERON JAM / SPOILER JAM 2.23 RUDDER JAM 2.23 LANDING GEAR LDG GEAR GRAVITY EXTENSION 2.24 LANDING WITH ABNORMAL LDG GEAR 2.24 LDG GEAR UNSAFE INDICATION 2.25 LDG GEAR RETRACTION IMPOSSIBLE 2.25 ANTI-SKID FAULT 2.25 BRK TEMP HOT 2.25 AIR BLEED VALVE FAULT 2.26 BLEED OVHT 2.26 BLEED LEAK 2.26 X VALVE OPEN 2.26 PACK VALVE FAULT 2.26 BOTH PACK VALVES FAULT 2.26 RECIRC FAN FAULT 2.26 DUCT OVHT 2.26A EXCESS CAB ALT 2.26A AUTO PRESS FAULT 2.26A
R EXCESS CAB ΔP 2.26A AVIONICS VENT EXHAUST MODE FAULT 2.27 OVBD VALVE FAULT 2.27
2.03
72
FOLLOWING FAILURES SEP 10 001
2 - PROCEDURES FOLLOWING FAILURES Content 3/3 ANTI ICE AFR AIR BLEED FAULT …………………………………………………………. 2.28 DE-ICING AIR FRAME FAULT ………………………………………………….. 2.28 DE-ICING MODE SEL FAULT …………………………………………………… 2.28 MODE SEL AUTO FAULT (if applicable) ………………………………………. 2.28 ICE DETECT FAULT ……………………………………………………………… 2.29 DE- / ANTI-ICING ENG FAULT …………………………………………………. 2.29 ANTI-ICING PROP FAULT ………………………………………………………. 2.29 ANTI-ICING HORNS FAULT …………………………………………………….. 2.29 SIDE WINDOW / WINDSHIELD HTG FAULT …………………………………. 2.29 PROBES HTG FAULT ……………………………………………………………. 2.29 AUTO PILOT
AILERON MISTRIM (ADU message)
or EXCESSIVE LATERAL TRIM REQUIRED ………………………………….. or ABNORMAL FLIGHT CHARACTERISTICS
2.30
PITCH MISTRIM (ADU message) ………………………………………………. 2.30 PITCH TRIM FAIL (ADU message) (if applicable) …………………………….. 2.30 DADC DATA INVALID (ADU message) ………………………………………… 2.30 MPC APM FAULT ……………………………………………………………………….. 2.30A DEGRADED PERF ……………………………………………………………….. 2.30A INCREASE SPEED ………………………………………………………………. 2.30A AVIONICS AUDIO SEL FAULT ……………………………………………………………….. 2.31 AHRS A / ERECT FAIL …………………………………………………………… 2.31 EFIS COMP ………………………………………………………………………... 2.31 ADC SW FAULT …………………………………………………………………... 2.31 ADU FAILURE …………………………………………………………………….. 2.32 ADC FAULT ……………………………………………………………………….. 2.32 AHRS FAIL ………………………………………………………………………… 2.32 SGU FAIL ………………………………………………………………………….. 2.32 CRT FAIL ………………………………………………………………………….. 2.32 MISCELLANEOUS COCKPIT DOOR CONTROL PANEL FAULT (if installed) …………………… 2.32A VOLCANIC ASH ENCOUNTER………………… ………………………………. 2.32A LOSS OF RADIO ALTIMETER INFORMATION ………………………………. 2.33
R SMK DET FANS FAULT …………………………………………………………. 2.33 DOORS UNLK IN FLIGHT ………………………………………………………. 2.33 COCKPIT WINDOW CRACKED ………………………………………………… 2.33 OXYGEN LO PR ………………………………………………………………….. 2.33 MFC MFC 1A FAULT …………………………………………………………………… 2.34 MFC 1B FAULT …………………………………………………………………… 2.34 MFC 2A FAULT …………………………………………………………………… 2.35 MFC 2B FAULT …………………………………………………………………… 2.35 MFC 1A + 1B FAULT ……………………………………………………………... 2.36 MFC 1A + 2A FAULT ……………………………………………………………... 2.37 MFC 1A + 2B FAULT ……………………………………………………………... 2.38 MFC 1B + 2A FAULT ……………………………………………………………... 2.39 MFC 2A + 2B FAULT ……………………………………………………………... 2.40 MFC 1B + 2B FAULT ……………………………………………………………... 2.41
ELEC Section for EMER & ESS BUS lost equipment lists…………….………
Cargo configuration only…… 2.42 2.42A
2.04
72
FOLLOWING FAILURES POWER PLANT
APR 08 500
SINGLE ENG OPERATION
LAND ASAP PWR MGT 1 + 2 .......................................... TO if necessary then MCT FUEL PUMP affected side.............................................................. OFF DC GEN affected side .................................................................... OFF ACW GEN affected side ................................................................. OFF PACK affected side......................................................................... OFF BLEED affected side....................................................................... OFF TCAS (if installed) ................................................................... TA ONLY OIL PRESSURE ON FAILED ENGINE .................................MONITOR Note: In icing conditions, FLAPS 15 will be selected to improve drift down
performances and single engine ceiling. Note: Refer to pages (4.61) and (4.62) to determine single engine gross
ceiling. Note: If during the flight, a positive oil pressure has been noted on the
failed engine for a noticeable period of time, maintenance must be informed.
Note: monitor fuel balance. Recommended operational maximum fuel unbalance is 200 kg (440 lb).
When FUEL CROSS FEED is required FUEL PUMP affected side........................................................... ON FUEL X FEED.............................................................................. ON FUEL PUMP operating engine .................................................. OFF
For approach MAX APPROACH SLOPE for Steep Slope Approach ............... 5.5° BLEED NOT AFFECTED .......................................................... OFF CL live engine...............................................................100% OVRD
APPROACH SPEED ........................... NOT LESS THAN 1.1VMCA Note: Refer to page (4.64) to determine 1.1VMCA.
Note: At touch down, do not reduce below FI before nose wheel is on the ground.
START FAULT
ENG START ROTARY SELECTOR...................OFF / START ABORT
If above 45 % NH START ON LIGHT....................................CHECK EXTINGUISHED START ............................................................. TO BE CONTINUED
X START FAIL
CONTINUE NORMAL ENGINE START INFORM MAINTENANCE
Mod : 3973 or 4371 or 4457
2.0572
FOLLOWING FAILURESPOWER PLANT
OCT 08 001
ABNORMAL PARAMETERSDURING START
If ITT tends to exceed 900°C, or no ITT, or no NHCL affected side ................................................................ FUEL SOENG START ROTARY SELECTOR..............OFF / START ABORT
Then refer to relevant procedure:
EXCESSIVE ITT DURING START procedure (2.05)
NO ITT DURING START procedure (2.05)
NO NH DURING START procedure (2.05)
EXCESSIVE ITT DURING START
When NH below 30 %ENG START ROTARY SELECTOR.....................................CRANKSTART PB ................................................................................... ON
After 15 secondsENG START ROTARY SELECTOR ........OFF / START ABORT
CAUTION: If ITT exceeds 950°C, maintenance action is due.
Note: BLEED VALVE may be selected OFF in order to reduce ITT.
NO ITT DURING START
After 30 seconds, to allow fuel drainingENG START ROTARY SELECTOR.....................................CRANKSTART PB ................................................................................... ON
After 15 secondsENG START ROTARY SELECTOR ........OFF / START ABORT
NO NH DURING START
R
Note: On BAT only, OIL PRESS IND is not available.
ENG START ROTARY SELECTOR...................START A or START B
START PB ........................................................................................ ON
After 10 seconds
If OIL pressure increasesCL ..........................................................................................FTRContinue START procedure, being informed NH indicator isinoperative.
If OIL pressure does not increasesENG START ROTARY SELECTOR ........OFF / START ABORTSuspect starter motor failure. Maintenance action is due.
2.0672
FOLLOWING FAILURESPOWER PLANT
SEP 10 001
R ENG NAC OVHT
RR
R
RR
If during Hotel mode operationPL affected side .............................................................................GICL affected side.............................................. FTR THEN FUEL SO
If during taxiAIRCRAFT...............................................................................STOPPL affected side .............................SLIGHTLY INCREASE POWER
If unsuccessful within 30 secondsPL affected side........................................................................GICL affected side......................................... FTR THEN FUEL SO
ABNORMAL ENG PARAMETERSIN FLIGHT
RRRRRRRRRR
If Intermittent fluctuations or unrealistic steady indicationATPCS....................................................................................... OFF
When adequate flight situationPL affected side…………………………………………………… FIEEC affected side................................................................. OFF If successful
ONE EEC FAULT procedure (2.09) ..............................APPLY If unsuccessful- or - If TQ = 0% and NP<77%
PL affected side..................................................................... FICL affected side......................................................... FUEL SOSINGLE ENG OPERATION procedure (2.04) ..............APPLY
If "- - -" indication on torque digital counter (only for PW127 -PW127F - PW127M)
AVOID SUDDEN PL MOVEMENTS
FIRE LOOP FAULT
LOOP affected ................................................................................ OFF
2.07
72
FOLLOWING FAILURES POWER PLANT
APR 08 001
ABNORMAL PROP BRK (if applicable)
If on ground
If unexpected propeller rotation – or – If local UNLK and CCAS PROP BRK alert CL 2 .............................................................................. FUEL SO MAINTENANCE ACTION REQUIRED
If CCAS PROP BRK alert only If GUST LOCK ON CL 2 ......................................................................... FUEL SO If DC and AC GPU are not available ENG 1.....................................................................START CL 1..........................................................................AUTO When READY light illuminates PROP BRK................................................................. OFF UNLK LIGHT .............................CHECK EXTINGUISHED PROP BRK PWR SPLY C/B .....................................PULL If GUST LOCK OFF GUST LOCK...................................................................... ON According to operational situation PROP BRK................................................................. OFF ALL PROP BRK LIGHTS ..........CHECK EXTINGUISHED
If in flight CONTINUE NORMAL OPERATION ENG 2 PARAMETERS .....................................................MONITOR After landing CL 2 .............................................................................. FUEL SO MAINTENANCE ACTION REQUIRED
2.08
72
FOLLOWING FAILURES POWER PLANT
APR 08 500
ENG RESTART IN FLIGHT
FUEL SUPPLY...........................................................................CHECK CL ........................................................................................... FUEL SO PL........................................................................................................ FI CAUTION: After ATPCS sequence, PWR MGT rotary selector must
be set to MCT position before engine restart, in order to cancel propeller feathering.
ENG START ROTARY SELECTOR................................ START A & B EEC PB............. RESET if necessary or DESELECT if FAULT persists START PB ........................................................................................ ON
At 10 % NH CL ...............................................................................................FTR RELIGHT ..........................................................................MONITOR CL ............................................................................................AUTO PL......................................................ADJUST TO OTHER ENGINE ENG START ROTARY SELECTOR....................................AS RQD SYSTEMS AFFECTED.................................................... RESTORE
ENG STALL
PL affected side .................................................................................. FI ENG PARAMETERS .................................................................CHECK
If abnormal engine parameters CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY
If normal engine parameters DE-/ANTI-ICING ENG ................................................................. ON PL affected side ...............................................SLOWLY ADVANCE If stall recurs Reduce thrust and operate below the stall threshold If stall does not recur Continue engine operation
Mod : 3973 or 4371 or 4457
2.0972
FOLLOWING FAILURESPOWER PLANT
SEP 10 500
ONE EEC FAULT
RR
ATPCS ............................................................................................ OFF
CAUTION: DO NOT DESELECT EEC FLASHING
When adequate flight situationPL affected side ............................... RETARD IN GREEN SECTOREEC affected side ..................................................................RESET
If successfulATPCS.................................................................................... ONPL affected side........................................... RESTORE POWER
If unsuccessfulEEC affected side................................................................. OFFPL affected side .......................................... RESTORE POWER......................................... HANDLING THROTTLE WITH CARE
In the following cases: icing conditions, engine(s) flame out,emergency descent, severe turbulence, heavy rainMAN IGN ........................................................................... ON
In final approachCL 1 + 2 ..............................................................100% OVRD
After landingTAXI WITH THE AFFECTED ENGINE FEATHEREDNote: ACW BTC must be check closed in order to avoid the lossof ACW bus on ground
BOTH EEC FAULT
ATPCS ............................................................................................ OFF
CAUTION: DO NOT DESELECT EEC FLASHING
When adequate flight situationPL 1 + 2 ........................................... RETARD IN GREEN SECTOREEC 1 + 2 ................................................................. OFF THEN ON
If EEC 1+2 recoveredATPCS.................................................................................... ONPL 1 + 2 ....................................................... RESTORE POWER
If only one EEC recoveredONE EEC FAULT procedure (2.09) .................................APPLY
If no EEC recoveredEEC 1 + 2 ............................................................................. OFFPL 1 + 2 ....................................................... RESTORE POWER....................................... HANDLING THROTTLES WITH CARETQ IND ENG 1 + 2.......................................................MONITORLDG DIST ....................................................... MULTIPLY BY 1.5Note: Refer to Part 4 to determine landing distance
In the following cases: icing conditions, engine(s) flame out,emergency descent, severe turbulence, heavy rainMAN IGN ........................................................................... ON
In final approachCL 1 + 2 ..............................................................100% OVRD
After landingBRAKE HANDLE........................................... EMER AS RQDCAUTION: Reverse power is reduced.Both main HYD pumps will be lost at low speed.TAXI ON BOTH ENGINES,HANDLE THROTTLES WITH CARE
Mod : 3973 or 4371 or 4457
2.10
72
FOLLOWING FAILURES POWER PLANT
APR 08 050
ENG FLAME OUT
PL affected side .................................................................................. FI
If NH drops below 30 % (no immediate relight) CL affected side.............................................. FTR THEN FUEL SO If damage suspected FIRE HANDLE affected side ...............................................PULL SINGLE ENG OPERATION procedure (2.04)..................APPLY If no damage suspected ENG RESTART IN FLIGHT procedure (2.08)..................APPLY If unsuccessful SINGLE ENG OPERATION procedure (2.04) ............APPLY
IDLE GATE FAIL
In flight IDLE GATE LEVER .................................................................PUSH
At touch down IDLE GATE LEVER ..................................................................PULL
Mod : 4111
2.10A
72
FOLLOWING FAILURES POWER PLANT
SEP 10 500
R
R
UNCOMMANDED 100% NP ON ONE OR
TWO PROPELLERS
RR
CL 1 + 2 .............................................................................100% OVRD
PEC SGL CH
DO NOT RESET PEC IN FLIGHT - NO SPECIAL CREW ACTION ANTICIPATE A PEC FAULT AT LANDING MAINTENANCE IS REQUIRED
PEC FAULT
� If in short final approach (below 400 ft RA) GO AROUND procedure .......................................................APPLY
� Above 400 ft or when adequate CL affected side............................................................100% OVRD PEC affected side ..................................................................RESET � If successful CL affected side..................................................................AUTO � If unsuccessful PEC affected side................................................................. OFF Avoid sudden PL movements � Before landing CL NON AFFECTED..........................................100% OVRD Reverse is not available on affected side. TAXI ON BOTH ENGINES Note: ACW BTC may be check closed in order to avoid the loss of ACW bus on ground
Mod : 3973 or 4371 or 4457
2.11
72
FOLLOWING FAILURES POWER PLANT
SEP 10 030
LO PITCH IN FLIGHT
PL affected side .................................................................................. FI CL affected side ................................................... FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04) ............................APPLY
ENG OVER LIMIT
PL affected side .............. RETARD TO RESTORE NORMAL VALUES
Note: BLEED VALVE may be selected OFF in order to reduce ITT
� If TQ, NH, and/or ITT still over limit and if conditions permit PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY
PROP OVER LIMIT
R R R R R R
PL affected side .......................... RETARD TO SET NP BELOW 101% PEC affected side .............................................................OFF then ON PL affected side .......................................................................AS RQD Note: If conditions do not permit engine shut down, 110% is allowed to
complete the flight. An engine removal has to be done for maintenance action on arrival.
� If NP decreases below 101% CONTINUE NORMAL FLIGHT � If NP remains above 101% and conditions permit PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY
Mod : 4371 Eng : PW124
2.12
72
FOLLOWING FAILURES POWER PLANT
OCT 08 050
ENG OIL TEMP BELOW 45°C
If icing conditions are expected or present
ENG POWER ...............................................If possible, INCREASE
ENG OIL TEMP HIGH
OIL TEMP between 115°C and 125°C
OIL TEMP AND PRESS ...................................................MONITOR Note: If OIL temperature rise follows PL reduction, advancing PL
may reduce OIL temperature. Note: If OIL temperature rise occurs in steady state conditions, a
power reduction should permit a reduction in OIL temperature.
OIL TEMP between 115°C and 125°C for more than 20 minutes PL affected side ...........RETARD TO SET minimum possible power
CAUTION: Flight plan must be rescheduled to minimize engine operating time in these abnormal conditions.
OIL TEMP above 125°C PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY
ENG OIL LO PR
R
PL affected side .................................................................................. FI
If both OIL LO PR on CAP and local alert are activated CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY
If local alert only is activated CL affected side.............................................. FTR THEN FUEL SO Once engine is shut off CL affected side..........................................................................FTR If CCAS is activated after 30 seconds CL affected side............................................................ FUEL SO ENG RESTART IN FLIGHT procedure (2.08)..................APPLY If not CL affected side ............................................................ FUEL SO SINGLE ENG OPERATION procedure (2.04)..................APPLY
If OIL LO PR alert on CAP only is activated DISREGARD INFORM MAINTENANCE
If single engine operation required NP of feathered engine.....................................................MONITOR If NP of feathered engine above 10% IAS ...................................... LIMIT NOT TO EXCEED NP 101% APPROACH SPEED .................................INCREASE BY 10 KT
Mod : 4111 Eng : PW124
2.13
72
FOLLOWING FAILURES FUEL
APR 08 001
FUEL ABNORMAL TEMP
If too high (>50°C)
Note: Avoid rapid throttle movement OIL TEMP AND OTHER ENGINES PARAMETERS .......MONITOR
If too low (<0°C) Note: Use anti-icing additive for next refueling if repair can't be done
FUEL CLOG
If both lights are illuminated
ENGINES PARAMETERS................................................MONITOR If abnormal engines parameters
LAND ASAP Note: Fuel contamination may be suspected
MAINTENANCE ACTION REQUIRED
If only one light is illuminated ENGINE PARAMETERS affected side.............................MONITOR
FEED LO PR
PUMP affected side ........................................................ CONFIRM ON ENGINE affected side...........MONITOR FOR POSSIBLE RUN DOWN
If engine runs down or if fuel quantity decreases significantly PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO PUMP affected side ................................................................... OFF FIRE HANDLE affected side ....................................................PULL SINGLE ENG OPERATION procedure (2.04).......................APPLY CAUTION: Do not open X FEED valve
2.14
72
FOLLOWING FAILURES FUEL
APR 08 001
FUEL LEAK ALERT CONDITION
A fuel leak may be detected by either: - sum of fuel on board (FOB), read in steady flight at cruise level, and
fuel used (FU), FOB+FU significantly less than fuel at departure, or - total fuel quantity decreasing (fuel spray from engine or wing tip), or - fuel imbalance, or - a tank emptying too fast (leak from engine or a hole in a tank), or - excessive fuel flow (leak from engine), or - fuel smell in the cabin
FUEL LO LVL
AVOID EXCESSIVE AIRCRAFT ATTITUDES If both LO LVL lights ON
LAND ASAP If LO LVL light on one side only
FUEL LEAK procedure (2.14)................................................APPLY
FUEL LEAK
When a leak is confirmed
LAND ASAP Leak from engine (excessive fuel flow or feed spray from engine) PL affected side........................................................................ FI CL affected side......................................... FTR THEN FUEL SO PUMP affected side.............................................................. OFF FIRE HANDLE affected side ...............................................PULL SINGLE ENG OPERATION procedure (2.04)..................APPLY If excessive fuel flow was identified before engine shutdown FUEL X FEED valve can be opened In all other cases X FEED valve must remain closed Leak not located FUEL X FEED............................................. MAINTAIN CLOSED
Note: the X FEED must remain closed to prevent the leak affecting both sides.
Before landing ATC................................................................................. NOTIFY
2.15
72
FOLLOWING FAILURES ELEC
OCT 08 001
DC BUS 1 OFF
DC GEN 1 ....................................................................................... OFF PF....................................................................................................CM2 MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN DC SVCE/UTLY BUS PB................................................MAINTAIN ON AFFECTED EQUIPMENT .............................................................. OFF DC BUS 1 LOST EQUIPMENT LIST.........................................CHECK
At touch down IDLE GATE LEVER ..................................................................PULL
DC BUS 1 LOST EQUIPMENT LIST
R R
DUCT/COMPT TEMP IND Recirculation Fan #1 AFCS Computer (in flight) Spoilers IND Stick Pusher PWR and CTL CM1 Stick Shaker CAPT and STBY Static Ports LH Side Window Anti-Icing LH Windshield HTG IND Weather Radar / Radio Altimeter
GPWS / G/S IND CM1 EHSI, DME #1 BLEED HP Valve #1 and LEAK IND BLEED X FEED Valve and IND AUTO PRESS Syncrophaser (if applicable) AUTO IDLE GATE Fuel Tank TEMP IND CM1 FF/FU IND CM1 Fuel TEMP and CLOG IND CM1 Oil PRESS and TEMP IND
R
AC BUS 1 OFF
Note: Wait for 10 seconds in order to confirm the failure. DC BTC......................................................................... ISOL THEN ON
If unsuccessful AC BUS 1 LOST EQUIPMENT LIST....................................CHECK
AC BUS 1 LOST EQUIPMENT LIST
R TRIMS IND
BLEED LEAK DET Weather Radar
For more information on BUS EQUIPMENT LISTS see FCOM 1.06.60
2.15A
72
FOLLOWING FAILURES ELEC
OCT 08 100
DC BUS 2 OFF
DC GEN 2 ....................................................................................... OFF PF....................................................................................................CM1 ADC SW.........................................................................SET TO ADC 1 VHF 1 / ATC 1...........................................................................SELECT AFFECTED EQUIPMENT .............................................................. OFF DC BUS 2 EQUIPMENT LIST ...................................................CHECK
Before descent PAX INSTRUCTIONS.......................................................... USE PA
After touch down TAXI ON BOTH ENGINES
DC BUS 2 LOST EQUIPMENT LIST
R
R
Recirculation Fan #2 AFCS ADU VHF and ATC #2 CM2 Stick Shaker DC AUX HYD Pump CM2 Static Ports, Wiper, Probes IND RH Side Window Anti-Icing RH Windshield HTG IND CM2 Clock
LIGHTS: TAXI / TO / WINGS PAX SIGNS CM2 ADC, EADI, EHSI and SGU ADF, DME and VOR/ILS #2 CM1 RMI BLEED HP Valve #2 DOORS: ALERTS IDLE GATE FAIL IND CM2 FF/FU IND CM2 Fuel TEMP and CLOG IND CM2 Oil PRESS and TEMP IND
R R
AC BUS 2 OFF
Note: Wait for 10 seconds in order to confirm the failure. DC BTC......................................................................... ISOL THEN ON
If unsuccessful PF ..............................................................................................CM1 AC BUS 2 EQUIPMENT LIST ..............................................CHECK
AC BUS 2 LOST EQUIPMENT LIST
R CM2 ASI/VSI/ALTI ADF, ADC OUTPUT #2
GPWS CM1 RMI R
For more information on BUS EQUIPMENT LISTS see FCOM 1.06.60
Mod : 4116
2.16
72
FOLLOWING FAILURES ELEC
OCT 08 001
ACW BUS 1 OFF / ACW BUS 2 OFF
R
ACW GEN affected side ................................................................. OFF LEAVE AND AVOID ICING CONDITIONS AS LONG AS ICING CONDITIONS EXIST ICE ACCRETION ..................................... VISUALLY MONITOR
If ACW BUS 1 OFF PF ..............................................................................................CM2 CM1 AIRSPEED INDICATOR ..........................................MONITOR
If ACW BUS 2 OFF PF ..............................................................................................CM1 CM2 AIRSPEED INDICATOR ..........................................MONITOR AFFECTED EQUIPMENT .............................................................. OFF HYD X FEED .................................................................................... ON ACW BUS 1 or 2 LOST EQUIPMENT LIST ..............................CHECK
If any IAS discrepancy occurs DADC DATA INVALID (ADU message) procedure (2.30) ....APPLY
After touch down TAXI ON BOTH ENGINES
ACW BUS 1 LOST EQUIPMENT LIST
R R
BLUE PUMP PWR CAPT PITOT / ALPHA / TAT ANTI-ICING PROP 1 ANTI-ICING HORNS (LH ELEV, RUD)
LH WINDSHIELD HTG LEFT LDG LIGHT PWR LEFT and REAR STROBES
R
ACW BUS 2 LOST EQUIPMENT LIST
R
GREEN PUMP PWR F/O PITOT / ALPHA / TAT ICE DET ANTI-ICING PROP 2
ANTI-ICING HORNS (RH ELEV, AIL) RH WINDSHIELD HTG TAXI and T/O LIGHTS PWR RIGHT LDG LIGHT PWR RIGHT STROBE
R R
2.16A
72
FOLLOWING FAILURES ELEC
OCT 08 001
ACW TOTAL LOSS
ACW GEN 1 + 2.............................................................................. OFF HYD X FEED .....................................................................CHECK OFF LEAVE AND AVOID ICING CONDITIONS AS LONG AS ICING CONDITIONS EXIST ICE ACCRETION........................................... VISUALLY MONITOR CM1 and CM2 AIRSPEED INDICATORS........................MONITOR ACW TOTAL LOSS EQUIPMENT LIST ....................................CHECK AFFECTED EQUIPMENT .............................................................. OFF MAIN HYD PUMPS......................................................................... OFF LDG GEAR EXTENSION/RETRACTION..................................... LOST NORMAL BRAKE ......................................................................... LOST LDG DIST .................................................................MULTIPLY BY 1.5 Note: Refer to Part 4 to determine LDG DIST
Before landing LDG GEAR LEVER ............................................................... DOWN BLUE PRESSURE................................................................CHECK FLAPS..................................................................................AS RQD LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY
After touch down REVERSE............................................................................AS RQD BRAKE HANDLE..................................................... EMER AS RQD TAXI ON BOTH ENGINES
ACW TOTAL LOST EQUIPMENT LIST
R
BLUE and GREEN PUMP PWR CAPT and F/O PITOT / ALPHA / TAT ICE DET ANTI-ICING PROP 1 + 2
ANTI-ICING HORNS LH and RH WINDSHIELD HTG TAXI and T/O LIGHTS PWR LEFT and RIGHT LDG LIGHTS PWR LEFT, RIGHT and REAR STROBES
R R
For more information on BUS EQUIPMENT LISTS see FCOM 1.06.60
2.1772
FOLLOWING FAILURESELEC
OCT 08 001
DC ESS BUS OFF
DC ESS BUS EQUIPMENT LIST ..............................................CHECK
If Cockpit Securized Door installedCOCKPIT DOOR MANUAL LOCK BOLT(S).....................................
.......................................................... MOVE TO CLOSE POSITION
Note: Cockpit Door Control Panel FAULT LIGHT is inoperative.
Note: When the door is locked with the manual bolt(s), theemergency access to the cockpit is unavailable. It isrecommended that at least two crewmembers remain in thecockpit during that time.
DC ESS BUS LOST EQUIPMENT LIST
RR
See QRH pages 2.42 (all configuration)and 2.42A (for cargo configuration only)
DC EMER BUS OFF
RR
LEAVE AND AVOID ICING CONDITIONSDESCEND TOWARD ........................................................FL100 / MEASTBY PITCH TRIM.......................................................... USE AS RQDADC SW (ADC FAULT lights lost) .................................SET TO ADC 2HYD X FEED .................................................................................... ON If ice accretion builds up on airframe
DE-ICING MODE SEL FAULT procedure (2.28)...................APPLYANTI-ICING PROP FAULT procedure (2.29) ........................APPLYANTI-ICING HORNS FAULT procedure (2.29) .....................APPLYCM1 and STBY IAS ............................................COMPARE to CM2Note: Use CM2 instruments in case of disagreement.
Before landingANTI-SKID ................................................................................. OFFN/W STEERING ........................................................................ OFFANTI-SKID FAULT procedure (2.25).....................................APPLY
DC EMER BUS OFF LOST EQUIPMENT LIST
RSee QRH pages 2.42 (all configuration)and 2.42A (for cargo configuration only)
For more information on BUS EQUIPMENT LISTS see FCOM 1.06.60
2.18
72
FOLLOWING FAILURES ELEC
OCT 08 500
DC GEN FAULT
DC GEN affected side..................................................................... OFF If OAT exceeds ISA + 25
FL........................................................................................200 MAX TAXI ON BOTH ENGINES
INV FAULT
NO SPECIFIC ACTION IN FLIGHT
ACW GEN FAULT
ACW GEN affected side ................................................................. OFF LEAVE AND AVOID ICING CONDITIONS TAXI ON BOTH ENGINES
DC SVCE/UTLY BUS SHED
DC SVCE/UTLY BUS PB..........................................................AS RQD
DC SVCE/UTLY BUS SHED LOST EQUIPMENT LIST
R See FCOM 1.06.60 pages 12 to 14
BAT CHG FAULT
CHG associated.............................................................................. OFF
DUAL BAT CHG LOSS
MFC MODULES, one at a time ....................................... OFF / RESET If RESET unsuccessful
LAND ASAP Note: minimize use of VHF 1 if conditions permit.
BAT DISCHARGE IN FLIGHT
ENG START ROTARY SELECTOR............................................... OFF
If battery(ies) still discharging LAND ASAP
Mod : 3246 + 4111
2.18A
72
FOLLOWING FAILURES ELEC
APR 08 500
STBY BUS AND BAT ONLY LOST EQUIPMENT LISTS
Mod : 4116
2.18B
72
FOLLOWING FAILURES ELEC
APR 08 500
STBY BUS AND BAT ONLY LOST EQUIPMENT LISTS
Mod : 4116
2.19
72
FOLLOWING FAILURES HYDRAULIC
OCT 08 001
HYD LO LVL
If blue system affected BLUE PUMP .............................................................................. OFF AUX PUMP ....................................................... OFF (CONFIRMED) REDUCED FLAPS LANDING procedure (2.21)....................APPLY After touch down USE NORMAL BRAKE FOR STEERING TAXI ON BOTH ENGINES
If green system affected GREEN PUMP........................................................................... OFF LDG DIST ............................................................ MULTIPLY BY 1.5 Note: Refer to Part 4 to determine landing distance LDG GRAVITY EXTENSION procedure (2.24) .....................APPLY After touch down TAXI ON BOTH ENGINES REVERSE.......................................................................AS RQD BRK HANDLE..................................................... EMER AS RQD
HYD SYS LOST EQUIPMENT LIST
BLUE GREEN
FLAPS / SPOILERS / N/W STEERING PROP BRK (if applicable) EMER AND PARKING BRK (on accu only)
LDG GEAR EXT / RET NORM BRK
BOTH MAIN HYD PUMPS LOSS
MAIN BLUE AND GREEN PUMPS ................................................ OFF X FEED ..............................................................................CHECK OFF LDG DIST .................................................................MULTIPLY BY 1.5 Note: Refer to Part 4 to determine landing distance
Before landing LDG GEAR LEVER ............................................................... DOWN BLUE PRESSURE................................................................CHECK FLAPS 15 ............................................................................AS RQD LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY FLAPS 30 ............................................................................AS RQD
After touch down TAXI ON BOTH ENGINES REVERSE............................................................................AS RQD BRK HANDLE.......................................................... EMER AS RQD
BOTH MAIN HYD PUMPS LOST EQUIPMENT LIST
R R
BLUE
recovered when LDG GEAR lever is DOWN
GREEN
R R R
FLAPS / SPOILERS / N/W STEERING PROP BRK (if applicable) EMER AND PARKING BRK (on accu only)
LDG GEAR EXT / RET NORM BRK
2.20
72
FOLLOWING FAILURES HYDRAULIC
OCT 08 050
BOTH HYD SYS LOSS
R
RRR
MAIN AND AUX PUMPS ................................................................ OFF
� Before approach GPWS......... GPWS OVRD or FLAP OVRD (depending on version) LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY APP/LDG SPEED........................VmHB 0 + 5 KT + WIND EFFECT LDG DIST ........................MULTIPLY LDG DIST FLAPS 30 BY 2.6 Note: Refer to Part 4 to determine VmHB and LDG DIST
CAUTION: Tail strike may occur if pitch attitude exceeds 8° during the flare depending upon vertical speed at touch down.
� After touch down REVERSE............................................................................AS RQD BRK HANDLE.......................................................... EMER AS RQD TAXI ON BOTH ENGINES
BOTH HYD SYS LOST EQUIPMENT LIST
R BLUE GREEN
R R R
FLAPS / SPOILERS / N/W STEERING PROP BRK (if applicable) EMER AND PARKING BRK (on accu only)
LDG GEAR EXT / RET NORM BRK
HYD LO PR / HYD OVHT
PUMP affected side ........................................................................ OFF X FEED ............................................................................................. ON
Mod : 4371 Eng : PW124
2.21
72
FOLLOWING FAILURES FLIGHT CONTROL
APR 08 050
FLAPS UNLK
If before V1
TAKE OFF ............................................................................ ABORT If after V1
VR, V2.............................................................INCREASE BY 10 KT If alarm occurs during approach
GO AROUND procedure .......................................................APPLY VGA ................................................................INCREASE BY 10 KT
When possible FLAPS..............................................................................................0 REDUCED FLAPS LANDING procedure (2.21)....................APPLY
FLAPS JAM / UNCOUPLED / ASYM
FLAPS CONTROL LEVER ..........NEAR FLAPS PRESENT POSITION
When applicable REDUCED FLAPS LANDING procedure (2.21)....................APPLY
REDUCED FLAPS LANDING
GPWS .............. GPWS OVRD or FLAP OVRD (depending on version) STEEP SLOPE APPROACH (≥4.5°) ............................... PROHIBITED
FLAPS LDG DIST FLAPS 30
MULTIPLY BY APP/LDG SPEED
0 1.9 VmHB 0 + WIND EFFECT + 5 KT
15 1.8 VmHB 15 + WIND EFFECT
Note: Refer to Part 4 to determine VmHB and LDG DIST CAUTION: Tail strike may occur if pitch attitude exceeds 8° during the
flare depending upon vertical speed at touch down.
STICK PUSHER / SHAKER FAULT
STICK PUSHER / SHAKER ........................................................... OFF TCAS (if installed) ................................................................... TA ONLY VmHB / VmLB FOR ALL CONFIGURATION ......INCREASE BY 10 KT LDG DIST ...............................................................MULTIPLY BY 1.13 Note: Refer to Part 4 to determine VmHB / VmLB and LDG DIST
Mod : 4371 Eng : PW124
2.22
72
FOLLOWING FAILURES FLIGHT CONTROL
APR 08 001
PITCH TRIM ASYM (LOCAL LIGHT)
AP DISCONNECTION...................................... CONFIRM MANUALLY PITCH TRIM INOPERATIVE procedure (2.22) ..........................APPLY
PITCH TRIM INOPERATIVE
EXISTING CONFIGURATION AND SPEED.......................................... .................................................... MAINTAIN AS LONG AS POSSIBLE
For approach STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED FLAPS................ EXTEND AT VFE FOR EACH CONFIGURATION LDG SPEED ...................................................INCREASE BY 10 KT LDG DIST .......................................................... MULTIPLY BY 1.13 Note: Refer to Part 4 to determine VmHB / VmLB and LDG DIST
RUDDER RELEASABLE CENTERING UNIT FAIL
If YD is available
YD ...................................................................................... ENGAGE If YD is not available
KEEP THE FEET ON THE PEDALS
PITCH DISCONNECT
BOTH CONTROL COLUMNS ........................................ CHECK FREE IAS .......................................................................................180 kt MAX LOAD FACTOR ............................................................................... 2 g MAX BANK ANGLE............................ 30° MAX UNTIL FLAPS EXTENSION
AVOID ICING CONDITIONS For approach
STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED LAND AT AIRPORT WITH MINIMUM CROSSWIND LDG SPEED ...................................................INCREASE BY 10 KT LDG DIST .......................................................... MULTIPLY BY 1.13 PL 1 + 2 ..................................... REDUCE SMOOTHLY TO FLARE Note: Refer to Part 4 to determine LDG DATA
When on ground and ELEV CLUTCH GUARDED PB installed PITCH RECONNECTION ON GROUND procedure (2.22A) ............ ...............................................................................................APPLY
2.22A
72
FOLLOWING FAILURES FLIGHT CONTROL
APR 08 001
PITCH RECONNECTION ON GROUND
(if applicable)
GUST LOCK ........................................................................... ENGAGE BOTH COLUMNS...................................................... CHECK LOCKED ELEV CLUTCH GUARDED PB .........................DEPRESS AND HOLD
When PITCH DISCONNECT flashes red on CAP ELEV CLUTCH GUARDED PB ........................................RELEASE PITCH DISCONNECT ON CAP ...............CHECK EXTINGUISHED BOTH COLUMNS.............................................. CHECK COUPLED
TLU FAULT
If ADC 1 + 2 are lost
If IAS above 185 kt TLU ...................................................................................HI SPD If IAS below 185 kt TLU ................................................................................. LO SPD DISREGARD TLU FAULT ALERT
If at least one ADC operates If IAS above 185 kt TLU ...................................................................................HI SPD If TLU FAULT alarm persists SPEED ............................................................... 180 KT MAX TLU............................................................................ LO SPD If IAS below 185 kt SPEED..................................................................... 180 KT MAX TLU................................................................................. LO SPD DISREGARD TLU FAULT ALERT If TLU green light is not lit VAPP ....................................................INCREASE BY 10 KT LDG DIST ................................................ MULTIPLY BY 1.13 LAND AT AIRPORT WITH MINIMUM CROSSWIND Note: Maximum demonstrated crosswind (dry runway) with TLU HI SPD
mode : 15 kt.
2.23
72
FOLLOWING FAILURES FLIGHT CONTROL
APR 08 001
ELEVATOR JAM
CONTROL COLUMNS ...................................................... UNCOUPLE
AVOID ICING CONDITIONS IAS ..................................................................................... 180 KT MAX
If one elevator is stuck to full down position IAS ................................................................................ 154 KT MAX
If left elevator is jammed MINIMUM MANEUVER OPERATING SPEEDS..........INCREASE BY 10 KT
If elevator jamming occurs at take off IAS ................................................................................ 161 KT MAX PITCH DISCONNECT procedure (2.22).....................................APPLY
AILERON JAM / SPOILER JAM
BANK ANGLE LIMIT................................................................ 25° MAX BLUE AND AUX HYD PUMPS ....................................................... OFF LAND AT AIRPORT WITH MINIMUM CROSSWIND
For approach STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED BLUE AND AUX HYD PUMPS.................................................... ON CAUTION: Do not extend FLAPS in turn
When in landing configuration BLUE AND AUX HYD PUMPS.................................................. OFF
Immediately after touch down BLUE AND AUX HYD PUMPS.................................................... ON
RUDDER JAM
STEEP SLOPE APPROACH (≥4.5°) ............................... PROHIBITED LANDING............................................................................... FLAPS 30 USE DIFFERENTIAL POWER SO AS TO MINIMIZE SIDESLIP LAND AT AIRPORT WITH MINIMUM CROSSWIND
At touch down NOSE DOWN BEFORE REDUCTION BELOW FI
2.24
72
FOLLOWING FAILURES LANDING GEAR
APR 08 001
LDG GEAR GRAVITY EXTENSION
LDG GEAR LEVER..................................................................... DOWN EMER EXTENSION HANDLE .........PULL ABOVE PEDESTAL LEVEL .....................AND MAINTAIN UP TO GREEN LIGHTS ILLUMINATED
CAUTION: Do not twist the handle when operating TCAS (if installed) ................................................................... TA ONLY If unsuccessful
LANDING WITH ABNORMAL LDG GEAR procedure (2.24)............APPLY
LANDING WITH ABNORMAL LDG GEAR
Preparation CABIN CREW (PA).............................................................. NOTIFY ATC / TRANSPONDER...................................... NOTIFY / AS RQD SEAT BELTS / NO SMOKING .................................................... ON GPWS........................................................................................ OFF CABIN AND COCKPIT .................................................... PREPARE LOOSE AND SURVIVAL EQUIPMENT ............ CHECK SECURED BELTS AND SHOULDER HARNESS .................. CHECK LOCKED FUEL WEIGHT .......................................... IF POSSIBLE, REDUCE If abnormal nose LDG GEAR CG LOCATION..............................................IF POSSIBLE, AFT If abnormal main LDG GEAR FUEL UNBALANCE .........................IF POSSIBLE, ESTABLISH Note: Reduced fuel on side with failed LDG GEAR.
Approach LDG GEAR LEVER ............................................. CONFIRM DOWN LDG GEAR EMER EXT HANDLE .....................CONFIRM PULLED ENG START ROTARY SELECTOR..............OFF / START ABORT CABIN REPORT........................................... CONFIRM OBTAINED
Before landing BLEEDS 1 + 2............................................................................ OFF BRACE FOR IMPACT ..........................................................ORDER
At touch down PL 1 + 2 .........................................................................................GI CL 1 + 2 .......................................................... FTR THEN FUEL SO
After touch down FIRE HANDLES 1 + 2 ..............................................................PULL
When aircraft stopped PARKING BRAKE ......................................................................SET CABIN CREW (PA).............................................................. NOTIFY FUEL PUMPS 1 + 2................................................................... OFF AGENTS 1 + 2 ....................................................................... DISCH EVACUATION ....................................................................INITIATE
Before leaving aircraft BAT ............................................................................................ OFF
2.2572
FOLLOWING FAILURESLANDING GEAR
SEP 10 001
LDG GEAR UNSAFE INDICATION
If LDG GEAR selected DOWN If GREEN LIGHT OFF on one panel only
UNSAFE INDICATION ........................................... DISREGARD If GREEN LIGHT OFF on both panels
LDG GEAR GRAVITY EXTENSION procedure (2.24) ....APPLY
If LDG GEAR selected UP If RED LIGHT ON on one panel only
UNSAFE INDICATION ........................................... DISREGARD If RED or GREEN LIGHT ON on both panels
LEAVE AND AVOID ICING CONDITIONSIAS ........................................................................... 160 KT MAXLDG GEAR ....................................................................... DOWNTCAS (if installed)......................................................... TA ONLY
LDG GEAR RETRACTION IMPOSSIBLE
LEAVE AND AVOID ICING CONDITIONSLDG GEAR LEVER..................................................................... DOWNIAS ..................................................................................... 185 KT MAXCCAS .............................................................................................. RCLTCAS (if installed) ................................................................... TA ONLYIDLE GATE ............................................................................MONITOR
ANTI-SKID FAULT
R ANTI SKID ...................................................................................... OFFLDG DIST ................................................................. MULTIPLY BY 1.4Note: Refer to Part 4 to determine LDG DIST
At touch downREVERSE............................................................................AS RQDNORMAL BRAKE .................................................USE WITH CAREBRAKE HANDLE ..................................................... EMER AS RQD
BRK TEMP HOT
If BRK TEMP HOT occurs before take offTAKE OFF .............................................................................DELAY
If BRK TEMP HOT occurs in flightLEAVE LDG GEAR DOWN FOR 1 MINUTE AFTER TAKE OFFFOR COOLING EXCEPT IN CASE OF EMERGENCY
2.26
72
FOLLOWING FAILURES AIR
APR 08 001
BLEED VALVE FAULT
PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES
BLEED OVHT
PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES
BLEED LEAK
PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES CAUTION: System must not be restored in flight. Note: If a bleed leak occurs on ground during taxi, go back to parking.
X VALVE OPEN
CAUTION: Do not supply both packs from one single bleed.
PACK VALVE FAULT
PACK VALVE affected side ............................................................ OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES
BOTH PACK VALVES FAULT
MAX FL ..................................................................................100 / MEA When ΔP < 1 PSI
OVBD VALVE ............................................................... FULL OPEN MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN MAN RATE KNOB................................................. MAX INCREASE
RECIRC FAN FAULT
RECIRC FAN affected side ............................................................ OFF
2.26A
72
FOLLOWING FAILURES AIR
OCT 08 001
DUCT OVHT
TEMP SEL affected side.................................................................MAN COMPT TEMP SELECTOR affected side....................................COLD CAUTION: Monitor DUCT TEMP and make sure it remains positive to
avoid possible pack turbine damage due to freezing. If alert persists
PACK VALVE affected side....................................................... OFF MAX FL.............................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES
EXCESS CAB ALT
R
CABIN PRESS IND....................................................................CHECK
If rapid decompression EMERGENCY DESCENT procedure (1.07A) .......................APPLY
If Z cabin > 10000 ft confirmed MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN MAN RATE KNOB.........................................................DECREASE
If unsuccessful CREW OXYGEN MASKS............................................................ ON CREW COMMUNICATIONS .........................................ESTABLISH OXYGEN PAX SUPPLY......................................................AS RQD OXYGEN PRESSURE..........................................................CHECK DESCENT.................................................................AS RQD / MEA
AUTO PRESS FAULT
MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN MAN RATE KNOB ...............................AS RQD TO SET CABIN RATE
FL 140 170 200 250
TARGET CAB ALT (ft) 0 2000 4000 6750
Note: Minimum TARGET CAB ALT is landing elevation
EXCESS CAB ΔP
MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN MAN RATE KNOB ...................................................... MAX INCREASE
If unsuccessful DESCENT TO A COMPATIBLE FL....................................INITIATE
2.27
72
FOLLOWING FAILURES AIR
APR 08 001
AVIONICS VENT EXHAUST MODE FAULT
EXHAUST MODE ........................................................................ OVBD
OVBD VALVE FAULT
CAUTION: Do not select OVBD valve FULL OPEN if ΔP > 1 PSI.
If engine 1 running, in flight or on ground OVBD VALVE ............................................................. FULL CLOSE
If engine 1 not running, on ground OVBD VALVE ............................................................... FULL OPEN
2.28
72
FOLLOWING FAILURES DE/ANTI ICE
APR 08 070
AFR AIR BLEED FAULT
LEAVE AND AVOID ICING CONDITIONS AFR AIR BLEED............................................................................. OFF
If DE-ICING ENG FAULT light illuminates after 10 s DE-ICING ENG affected side .................................................... OFF AFR AIR BLEED.......................................................................... ON AFR AIR BLEED light ....................................CHECK EXTINGUISH
If DE-ICING ENG FAULT light does not illuminate on any side DE-ICING AIR FRAME FAULT procedure (2.28)..................APPLY
DE-ICING AIR FRAME FAULT
DE-ICING AIR FRAME ................................................................... OFF LEAVE AND AVOID ICING CONDITIONS MINIMUM ICING SPEEDS ................................... INCREASE BY 10 kt
If in icing conditions LDG DIST .......................................................... MULTIPLY BY 1.13 Note: Refer to Part 4 to determine SPEEDS and LDG DIST
If ice accretion STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED
DE-ICING MODE SEL FAULT
OVRD........................................................................................SELECT MONITOR DE-ICING
In case of engine flame out OVRD................................................................................RELEASE
Mod : 1368 + (3973 or 4371)
2.29
72
FOLLOWING FAILURES DE/ANTI ICE
OCT 08 500
ICE DETECT FAULT
ICE ACCRETION................................................ VISUALLY MONITOR
DE-/ANTI-ICING ENG FAULT
LEAVE AND AVOID ICING CONDITIONS ENGINE PARAMETERS affected side..................................MONITOR
ANTI-ICING PROP FAULT
LEAVE AND AVOID ICING CONDITIONS ANTI-ICING PROP affected side.................................................... OFF
If propeller unbalance due to ice becomes excessive CL 1 + 2 ......................... MOVE TO 100% OVRD FOR 5 MINUTES
ANTI-ICING HORNS FAULT
LEAVE AND AVOID ICING CONDITIONS
If in icing conditions, every 5 minutes FLIGHT CONTROLS.............CHECK FREEDOM OF MOVEMENT
SIDE WINDOW / WINDWHIELD HTG FAULT
SIDE WINDOW / WINDSHIELD HTG affected side....................... OFF
PROBES HTG FAULT
R
If One PROBE HTG ALPHA illuminated
STICK PUSHER / SHAKER .............................................MONITOR If Two PROBE HTG ALPHA illuminated
STICK PUSHER / SHAKER ...................................................... OFF STICK PUSHER / SHAKER procedure (2.21).......................APPLY
If PROBE HTG other than ALPHA illuminated ADC non affected side................................................... SELECTED Associated INDICATION ..................................................MONITOR
Mod : 3973 or 4371 or 4457
2.30
72
FOLLOWING FAILURES AUTO PILOT
OCT 08 500
AILERON MISTRIM (ADU message)
– or – EXCESSIVE LATERAL TRIM REQUIRED
– or – ABNORMAL FLIGHT CHARACTERISTICS
FLIGHT CONTROLS ...............................................HOLDING FIRMLY AP ...................................................................................DISCONNECT
Note: FLY MANUALLY PRIOR TO ADJUSTING THE LATERAL TRIMS Note: The autopilot may be reengaged following adjustment of the lateral
trims
PITCH MISTRIM (ADU message)
FLIGHT CONTROLS ...............................................HOLDING FIRMLY AP ...................................................................................DISCONNECT Note: FLY MANUALLY UNTIL RESUMING NORMAL CONDITIONS
PITCH TRIM FAIL (ADU message)
FLIGHT CONTROLS ...............................................HOLDING FIRMLY AP ...................................................................................DISCONNECT Note: FLY MANUALLY UNTIL RESUMING NORMAL CONDITIONS
DADC DATA INVALID (ADU Message)
INSTRUMENTS............................................................CROSSCHECK FAULTY ADC......................................................................... IDENTIFY ADC SW............................................................... SELECT VALID ADC
If ADC 1 is wrong C/B ADC 1 ................................................................................PULL
If ADC 2 is wrong C/B ADC 2 ................................................................................PULL ADC FAULT procedure (2.32) ...................................................APPLY
Mod : 3168
2.30A
72
FOLLOWING FAILURES AND ABNORMAL
MPC APR 08 100
APPLICABLE TO AIRCRAFT FITTED WITH MODIFICATION 5567 or 8392 or 8442
APM FAULT
APM ..................................................................................................OFF
For troubleshooting see FCOM 2.02.21.
DEGRADED PERF
Mainly appears in level flight after CRUISE SPEED LOW or in climb, to inform the crew that an abnormal drag increase induces a speed decrease or a loss of rate of climb
The most probable reason is an abnormal ice accretion
AIRFRAME DE-ICING ON.........................................................CHECK IAS > RED BUG + 10 KT.......................................................MONITOR AP (if engaged) ................HOLD FIRMLY CONTROL WHEEL and DISENGAGE
If SEVERE ICING conditions confirmed – or – If impossibility to maintain IAS > RED BUG + 10 KT in level flight – or – If abnormal aircraft handling feeling
SEVERE ICING procedure (1.09) .........................................APPLY
If not
SCHEDULED FLIGHT....................................................CONTINUE ICING CONDITIONS and SPEED....................................MONITOR
INCREASE SPEED
Appears after DEGRADED PERF to inform the crew that the drag is abnormally high and IAS is lower than RED BUG + 10 KT
If abnormal conditions confirmed
IMMEDIATELY PUSH THE STICK TO INCREASE SPEED TO RECOVER MINIMUM IAS = RED BUG + 10 KT
SEVERE ICING procedure (1.09) .........................................APPLY
2.31
72
FOLLOWING FAILURES AVIONICS
APR 08 001
AUDIO SEL FAULT
AUDIO SEL affected side ............................................................. ALTN
AHRS A / ERECT FAIL
ATT / HDG PB affected side................................................. DEPRESS
When possible AIRCRAFT.................................... STABILIZE SPEED AND LEVEL AHRS affected side, PUSH TO ERECT PB ......................................
.................................................DEPRESS FOR 15 SECONDS
EFIS COMP
BOTH EADI, STBY HORIZON ..................................... CROSSCHECK WRONG INSTRUMENT ........................................................ IDENTIFY ATT / HDG PB affected side................................................. DEPRESS
If AHRS 1 is wrong C/B AHRS 1 NORM SPLY........................................................PULL C/B AHRS 1 AUX SPLY ...........................................................PULL
If AHRS 2 is wrong C/B AHRS 2 NORM SPLY........................................................PULL C/B AHRS 2 AUX SPLY FLT....................................................PULL
If LOC / GS / ILS caution appears on EFIS NAV SOURCES....................................................................CHECK VOR / ILS PB affected side .............................. DEPRESS AS RQD
ADC SW FAULT
ADC SW........................................................ SET TO OPPOSITE ADC
2.32
72
FOLLOWING FAILURES AVIONICS
APR 08 050
ADU FAILURE
IAS / VS MODE.......................................................................USE TCS Note: ALT SEL mode is lost
If amber "AP MSG" appears on EADI – or – If in composite mode FLIGHT CONTROLS................................................ HOLD FIRMLY AP ..............................................................................DISCONNECT
ADC FAULT
VALID ADC ...............................................................................SELECT PF..............................................................................NON affected side AP COUPLING .........................................................NON affected side ATC.................................................................NON affected equipment
If ADC 1 is lost LANDING ELEVATION ...................... PRESSURE ALTITUDE SET GPWS........................................................................................ OFF
If ADC 1 + 2 are lost STBY INST ................................................................................ USE MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN ENGINE PARAMETERS ..................................................MONITOR TCAS (if installed).................................................................... STBY GPWS........................................................................................ OFF TLU ................................................................................MAN MODE TLU FAULT procedure (2.22A) .............................................APPLY
AHRS FAIL
ATT / HDG PB affected side................................................. DEPRESS Periodically compare remaining AHRS outputs to STBY INST
SGU FAIL
EFIS SG PB affected side .................................................... DEPRESS
CRT FAIL
CRT affected................................................................................... OFF
Mod : 5205
2.32A
72
FOLLOWING FAILURES MISCELLANEOUS
APR 08 100
COCKPIT DOOR CONTROL PANEL FAULT (if installed)
COCKPIT DOOR MANUAL LOCK BOLT(S).......................................... ............................................................... MOVE TO CLOSE POSITION Note: when the door is locked with the manual bolt(s), the emergency
access to the cockpit is unavailable. It is recommended that at least two crewmembers remain in the cockpit during that time.
2.3372
FOLLOWING FAILURESMISCELLANEOUS
SEP 10 001
LOSS OF RADIO ALTIMETER INFORMATION
GPWS ............................................................................................. OFFTCAS (if installed) ......................................................................... STBY
CAUTION: LDG GEAR NOT DOWN undue warning may begenerated when reducing PL; this alarm may becancelled by using EMER AUDIO CANCEL.
R SMK DET FANS FAULT
FAN............................................................................................... ALTN
DOORS UNLK IN FLIGHT
If any door except FWD COMPTSIGNS.......................................................................................... ONASSOCIATED DOOR.........................................VISUALLY CHECK
If unlocked or check not feasibleLANDING ELEVATION .....................................................9000 ftMAX FL........................................................................100 / MEA
If FWD COMPTNO ACTION
COCKPIT WINDOW CRACKED
WINDOW HEAT affected................................................................ OFFLANDING ELEVATION................................................................9000 ftMAX FL ..................................................................................100 / MEA
OXYGEN LO PR
OXY MAIN SUPPLY ...................................................... OFF THEN ON
If OXYGEN LO PR light remains illuminatedMAIN SUPPLY........................................................................... OFFOXYGEN PORTABLE UNIT.......... INSTALL IN COCKPIT AS RQD
2.34
72
FOLLOWING FAILURES MFC
OCT 08 001
MFC 1A FAULT
R R
MODULE 1A .................................................................... OFF / RESET MFC 1A MODULE LOST EQUIPMENT LIST............................CHECK
R MFC 1A MODULE LOST EQUIPMENT LIST
MECHANIC CALL IND DC BUS 1 OFF WARNING AC BUS 1 SPLY INV 1 FAULT LIGHT
LDG GEAR PRIMARY UNLK IND BLEED HP VALVE 1 FWD COMPT DOOR UNLK IND EMER HATCH UNLK IND RIGHT AFT DOOR UNLK IND, if
applicable
MFC 1B FAULT
R R
MODULE 1B .................................................................... OFF / RESET MFC 1B MODULE LOST EQUIPMENT LIST............................CHECK
If failure during take off PACK 1 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN Prior take off PACK 2 ................................................................................. OFF After take off PACKS.................................................................................... ON OVBD VALVE........................................................ FULL CLOSE LDG GEAR ......LEAVE DOWN FOR COOLING FOR 1 MINUTE ..........AFTER TAKE OFF EXCEPT IN CASE OF EMERGENCY
After landing PACK 1 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN
CAUTION : Before opening any door, PACKS 1 and 2 must be selected OFF and cockpit communication hatch must be open.
R MFC 1B MODULE LOST EQUIPMENT LIST
GROUND FAN 1 OUTFLOW VALVE OPENING AFTER
LANDING OVBD VALVE AUTO
FUNCTIONING CVR ERASE
DC STBY BUS UNDV DETECT INV 1 FAULT LIGHT GREEN PUMP LO PR IND BRAKE OVERTEMP ALERTS LH / RH BLEED VALVE 1 FAULT IND
2.35
72
FOLLOWING FAILURES MFC
OCT 08 001
MFC 2A FAULT
R R
MODULE 2A .................................................................... OFF / RESET AVIONICS VENT EXHAUST MODE ........................................... OVBD MFC 2A MODULE LOST EQUIPMENT LIST............................CHECK
If failure during taxi out OVBD VALVE ............................................................... FULL OPEN After take off IDLE GATE......................................................................CHECK OVBD VALVE.....................................................................AUTO
At touch down IDLE GATE .......................................................................MONITOR
After landing OVBD VALVE ............................................................... FULL OPEN
R MFC 2A MODULE LOST EQUIPMENT LIST
AIR X VALVE OVBD VALVE AUTO FUNCTIONING EXTRACT FAN HOSTESS CALL IND CREW CALL IND DC BUS 2 OFF WARNING AC BUS 2 SPLY INV 2 FAULT LIGHT
RH SIDE WINDOW ANTI-ICING LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN
ARROWS BLEED HP VALVE 2 LEFT DOORS UNLK IND IDLE GATE AMBER WARNING
MFC 2B FAULT
R R
MODULE 2B .................................................................... OFF / RESET MFC 2B MODULE LOST EQUIPMENT LIST............................CHECK
Failure during take off PACK 2 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN Prior take off PACK 1 ................................................................................. OFF After take off PACK 1 + 2............................................................................. ON OVBD VALVE........................................................ FULL CLOSE LDG GEAR ......LEAVE DOWN FOR COOLING FOR 1 MINUTE ..........AFTER TAKE OFF EXCEPT IN CASE OF EMERGENCY
After landing PACK 2 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN
CAUTION: Before opening any door, PACKS 1 and 2 must be selected OFF and cockpit communication hatch must be open.
R MFC 2B MODULE LOST EQUIPMENT LIST
GROUND FAN 2 OUTFLOW VALVE OPENING AFTER
LANDING OVBD VALVE AUTO FUNCTIONING INV 2 FAULT LIGHT RH SIDE WINDOW ANTI-ICING and
associated FAULT IND
LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN
ARROWS RH BRAKE OVERTEMP ALERTS BLEED VALVE 2 FAULT IND
2.36
72
FOLLOWING FAILURES MFC
OCT 08 001
MFC 1A+1B FAULT
R R
MODULES 1A+1B ........................................................... OFF / RESET PROP 1 ANTI-ICING ...................................................................... OFF PROP ANTI-ICING FAULT procedure (2.29) .............................APPLY DE-ICING MODE SEL .................................................. OVRD AS RQD PACK 1 ........................................................................................... OFF BLEED 1 ......................................................................................... OFF BLEED VALVE FAULT procedure (2.26) ...................................APPLY RADAR ........................................................................................... OFF GPWS ............................................................................................. OFF MFC 1A+1B MODULES LOST EQUIPMENT LIST...................CHECK
Before landing ATPCS....................................................................................... OFF
After landing OVBD VALVE ............................................................... FULL OPEN
CAUTION : Before opening any door, PACKS 1 and 2 must be selected OFF and cockpit communication hatch must be open.
R MFC 1A+1B MODULES LOST EQUIPMENT LIST
PACK 1 / PACK 1 FAULT IND GROUND FAN 1 OUTFLOW VALVE OPENING AFTER
LANDING OVBD VALVE AUTOFUNCTIONING MECHANIC CALL IND CVR ERASE DC STBY BUS UNDV DETECT DC BUS 1 OFF WARNING AC BUS 1 SPLY INV 1 FAULT LIGHT LEFT PFTS STICK PUSHER TRIPLE TRIM IND GREEN PUMP LO PR INDICATION ANTI-ICING PROP 1 and associated
FAULT IND
DE-ICING AIRFRAME (BOOTS A) DE-ICING AIRFRAME (BOOTS B) LH SIDE WINDOW ANTI-ICING and
associated FAULT IND PRIMARY UNLK IND PRIMARY GREEN ARROWS BRAKE OVERTEMP ALERTS LH / RH BLEED HP VALVE 1 BLEED VALVE 1 and associated
FAULT IND FWD COMPT DOOR UNLK IND EMER HATCH UNLK IND RIGHT AFT DOOR UNLK IND, if
applicable ENG 1 UPTRIM ENG 1 AUTO FEATHER LEFT AUTO CL
2.3772
FOLLOWING FAILURESMFC
OCT 08 001
MFC 1A+2A FAULT
R
R
R
MODULES 1A+2A ........................................................... OFF / RESETTLU .....................................................................................MAN MODEAVIONICS VENT EXHAUST MODE ........................................... OVBDRADAR ........................................................................................... OFFGPWS ............................................................................................. OFFMFC 1A+2A MODULES EQUIPMENT LIST .............................CHECKNote : Airframe FAULT amber alert is lost.Note : When airframe de-icing is used, monitor boots inflation.Note : As AP OFF alert is lost, use of AP below 1000 ft AGL is prohibited.Note : VOR 2, ADF 2, CRS 2 information are lost. ADC 2 outputs are not
available.
Before landingLDG GEAR LEVER ............................................................... DOWNEMER EXTENSION HANDLE..................................................PULL
CAUTION : LDG GEAR cannot be retracted.
At touch downIDLE GATE .......................................................................MONITOR
After landingOVBD VALVE ................................................................FULL OPEN
R MFC 1A+2A MODULES LOST EQUIPMENT LIST
AIR X VALVEOVBD VALVE AUTOFUNCTIONINGEXTRACT FANAP OFF WARNING LIGHTALTITUDE ALERT LIGHTGUIDANCE LIGHTMECHANIC CALL INDHOSTESS CALL INDCREW CALL INDRECORDERS (START/STOP)DC BUS 1 + 2 OFF WARNINGAC BUS 1 + 2 SPLYINV 1 + 2 FAULT LIGHTEMER BAT CHG CTLFLAPS UNLK WARNINGSTICK PUSHER / SHAKER FAULTReleasable Centering Unit AUTO
DISCONNECT after YAW TRIMaction or YD engagement
TLU FAULT LIGHT
TRIPLE TRIM INDAIL LOCK LIGHT (if installed)DE-ICING AIRFRAME FAULTRH SIDE WINDOW ANTI-ICINGCCAS WARNING ALERT (FLAP
UNLK)LDG GEAR CONTROLLDG GEAR PRIMARY UNLK INDLDG GEAR Secondary UNLK INDLDG GEAR Secondary GREEN
ARROWSLIGHT TESTBLEED HP VALVE 1 + 2LEFT DOORS UNLK INDFWD COMPT DOOR UNLK INDEMER HATCH UNLK INDRIGHT AFT DOOR UNLK IND, if
applicableRIGHT FWD DOOR UNLK INDIDLE GATE and associated AMBER
WARNING
2.3872
FOLLOWING FAILURESMFC
OCT 08 001
MFC 1A+2B FAULT
R
R
R
MODULES 1A+2B ........................................................... OFF / RESETMAIN BLUE HYD PUMP................................................................. OFFHYD X FEED .................................................................................... ONDE-ICING MODE SEL .................................................. OVRD AS RQDMFC 1A+2B MODULES EQUIPMENT LIST .............................CHECKNote : AP does not disconnect after STBY PITCH TRIM activation.
Before landingNote : Flaps control is lost.REDUCED FLAPS LANDING procedure (2.21)....................APPLYLDG GEAR LEVER ............................................................... DOWNEMER EXTENSION HANDLE..................................................PULL
CAUTION : LDG GEAR cannot be retracted.
After landingPACK 2 ...................................................................................... OFFOVBD VALVE ................................................................FULL OPEN
CAUTION : Before opening any door, PACKS 1 and 2 must be selectedOFF and cockpit communication hatch must be open.
R MFC 1A+2B MODULES LOST EQUIPMENT LIST
GROUND FAN 2OUTFLOW VALVE OPENING AFTER
LANDINGOVBD VALVE AUTOFUNCTIONINGMECHANIC CALL INDDC BUS 1 OFF WARNINGAC BUS 1 SPLYINV 1 + 2 FAULT LIGHTFLAPS CONTROLBLUE HYD PUMP CTLDE-/ANTI-ICING ENG 1DE-/ANTI-ICING ENG 2 FAULT
RH SIDE WINDOW ANTI-ICING andassociated FAULT IND
LDG GEAR CONTROLLDG GEAR PRIMARY UNLK INDLDG GEAR Secondary UNLK INDLDG GEAR Secondary GREEN
ARROWSBRAKE OVERTEMP ALERT RHBLEED HP VALVE 1BLEED VALVE 2 FAULT INDFWD COMPT DOOR UNLK INDEMER HATCH UNLK INDRIGHT AFT DOOR UNLK IND, if
applicable
2.3972
FOLLOWING FAILURESMFC
OCT 08 001
MFC 1B+2A FAULT
R
RR
MODULES 1B+2A ........................................................... OFF / RESETDE-ICING MODE SEL .................................................. OVRD AS RQDAVIONICS VENT EXHAUST MODE ........................................... OVBDMFC 1B+2A MODULES EQUIPMENT LIST .............................CHECKNote : VOR 2, ADF 2, CRS 2 information are lost. CM2 IAS is not
available.
Before landingNote : Flaps control is lost.REDUCED FLAPS LANDING procedure (2.21)....................APPLYLDG GEAR LEVER ............................................................... DOWNEMER EXTENSION HANDLE..................................................PULL
CAUTION : LDG GEAR cannot be retracted.
At touch downIDLE GATE .......................................................................MONITOR
After landingPACK 1 ...................................................................................... OFFOVBD VALVE ................................................................FULL OPEN
CAUTION : Before opening any door, PACKS 1 and 2 must be selectedOFF and cockpit communication hatch must be open.
R MFC 1B+2A MODULES LOST EQUIPMENT LIST
GROUND FAN 1AIR X VALVEOUTFLOW VALVE OPENING AFTER
LANDINGOVBD VALVE AUTOFUNCTIONINGEXTRACT FANHOSTESS CALL INDCREW CALL INDCVR ERASEDC STBY BUS UNDV DETECTDC BUS 2 OFF WARNINGAC BUS 2 SPLYINV 1 FAULT LIGHTINV 2 FAULT LIGHT
FLAPS CONTROLGREEN PUMP LO PR INDICATIONDE-/ANTI-ICING ENG 1 FAULTDE-/ANTI-ICING ENG 2RH SIDE WINDOW ANTI-ICINGLDG GEAR CONTROLLDG GEAR Secondary UNLK INDLDG GEAR Secondary GREEN
ARROWSBRAKE OVERTEMP ALERTS LH / RHBLEED HP VALVE 2BLEED VALVE 1 FAULT INDLEFT DOORS UNLK INDIDLE GATE AMBER WARNING
2.40
72
FOLLOWING FAILURES MFC
OCT 08 001
MFC 2A+2B FAULT
R R
MODULES 2A+2B ........................................................... OFF / RESET AVIONICS VENT EXHAUST MODE ........................................... OVBD ANTI-ICING PROP 2 ...................................................................... OFF ANTI-ICING PROP FAULT procedure (2.29) .............................APPLY DE-ICING MODE SEL .................................................. OVRD AS RQD PACK 2 ........................................................................................... OFF BLEED 2 ......................................................................................... OFF BLEED VALVE FAULT procedure (2.26) ...................................APPLY MFC 2A+2B MODULES EQUIPMENT LIST .............................CHECK
Before landing ATPCS....................................................................................... OFF
At touch down IDLE GATE .......................................................................MONITOR
After landing OVBD VALVE ............................................................... FULL OPEN
CAUTION : Before opening any door, PACKS 1 and 2 must be selected OFF and cockpit communication hatch must be open.
R MFC 2A+2B MODULES LOST EQUIPMENT LIST
PACK 2 PACK 2 FAULT IND GROUND FAN 2 AIR X VALVE OUTFLOW VALVE OPENING AFTER
LANDING OVBD VALVE AUTOFUNCTIONING EXTRACT FAN HOSTESS CALL IND CREW CALL IND DC BUS 2 OFF WARNING AC BUS 2 SPLY INV 2 FAULT LIGHT STICK PUSHER ANTI-ICING PROP 2 ANTI-ICING PROP 2 FAULT DE-ICING AIRFRAME (BOOTS B)
RH SIDE WINDOW ANTI-ICING and associated FAULT IND
LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN
ARROWS BRAKE OVERTEMP ALERT RH BLEED HP VALVE 2 BLEED VALVE 2 BLEED VALVE 2 FAULT IND LEFT DOORS UNLK IND ENG 2 UPTRIM ENG 2 AUTO FEATHER PROP BRAKE BRAKING if applicable PROP BRAKE RELEASING if
applicable IDLE GATE AMBER WARNING RIGHT AUTO CL
2.41
72
FOLLOWING FAILURES MFC
OCT 08 001
MFC 1B+2B FAULT
R R
MODULES 1B+2B ........................................................... OFF / RESET OVERHEAD PANEL..............................................................MONITOR MFC 1B+2B MODULES EQUIPMENT LIST .............................CHECK
Before landing NOSE WHEEL STEERING ....................................................... OFF ANTI-SKID ................................................................................. OFF ANTI-SKID FAULT procedure (2.25).....................................APPLY LDG GEAR LEVER ............................................................... DOWN EMER EXTENSION HANDLE..................................................PULL
CAUTION : LDG GEAR cannot be retracted.
At touch down IDLE GATE ...............................................................................PULL DIFFERENTIAL BRAKING........................................................ USE
After landing PACK 1 + 2 ................................................................................ OFF ANTI-ICING HORNS ................................................................. OFF PROBES HTG ........................................................................... OFF OVBD VALVE ............................................................... FULL OPEN Note : ATPCS ARM light is not available. Autofeather light is lost. Note : External power cannot be used.
CAUTION : Before opening any door, PACKS 1 and 2 must be selected OFF and cockpit communication hatch must be open.
R MFC 1B+2B MODULES LOST EQUIPMENT LIST
GROUND FAN 1 GROUND FAN 2 AIR X VALVE OUTFLOW VALVE OPENING AFTER
LANDING OVBD VALVE AUTOFUNCTIONING CVR ERASE DC STBY BUS UNDV DETECT INV 1 FAULT LIGHT INV 2 FAULT LIGHT MAIN BAT CHG CTL BAT DISCHARGE IN FLIGHT FLAPS ASYMMETRY DETECTION STICK PUSHER INHIBITION STICK SHAKER STALL WARNING PITCH TRIM WHOOLER PITCH TRIM ASYMWARNING AIL LOCK LIGHT if applicable GREEN PUMP LO PR INDICATION RH SIDE WINDOW ANTI-ICING and
associated FAULT IND INHIBITION OF HORNS ANTI-ICING
ON GROUND
CCAS MASTER WARNING CCAS MASTER CAUTION CCAS AURAL ALERTS CCAS AMBER ALERTS ON CAP CCAS WARNING ALERTS (CONFIG,
PROP BRK, ENG OIL) LDG GEAR CONTROL LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN
ARROWS BRAKE OVERTEMP ALERTS LH / RH LDG GEAR LEVER LOCKED DOWN
ON GROUND NOSE WHEEL STEERING ANTI-SKID "LANDING GEAR NOT DOWN"
WARNING BLEED VALVE 1 FAULT IND BLEED VALVE 2 FAULT IND ARM LIGHT IND PROP BRAKE RED UNLK LT if
applicable LEFT and RIGHT AUTO CL
2.42
72
FOLLOWING FAILURES ELEC
APR 08 100
DC EMER BUS LOST EQUIPMENT LIST
DC ESS BUS LOST EQUIPMENT LIST
AIR CONDITIONING OVBD and Underfloor Valves CTL OVBD and Underfloor Valves IND AIR COOLING high flow IND PRESS IND / EXCESS ALT IND Pneumatic Outflow Valves FWD COMPT Ventilation Valve (*) COMMUNICATIONS VHF / RCAU CM2 Cockpit Amplifier ELECTRICAL POWER AC BUS OFF 1 + 2 IND ACW BUS OFF 1 + 2 IND INV 1 FAULT IND DC BUS OFF 1 + 2 IND DC STBY BUS IND (UNDV/OVRD) EMER BAT CHG IND FIRE PROTECTION FIRE HANDLE IND ENG 1 + 2 FIRE DETECTION ENG 1 + 2 FLIGHT CONTROLS PITCH TRIM NORMAL COMMAND RUDDER TRIM AILERON TRIM HYDRAULIC POWER BLUE PUMP CTL and IND GREEN PUMP IND ICE AND RAIN PROTECTION AAS CTL, IND and ALERTS WING, EMPENNAGE BOOTS A ENG 1 BOOTS A and B PROP 1 + 2 ANTI-ICING CTL PROP 1 + 2 ANTI-ICING IND HORNS ANTI-ICING IND and CTL INDICATING / RECORDING CM1 CLOCK FDAU on ground LANDING GEAR ANTI-SKID Outboard NOSE WHEEL STEERING WOW 1 CTL LIGHTS CM1 PANELS PYLON STBY COMPASS LAVATORY (EMER) NAVIGATION ATC 1 PROPELLERS A/F AUX PUMPS CTL TQ IND 1 + 2 ENGINES CL FIRE IND 1 + 2 (*): if applicable
AIR CONDITIONING PACK and RECIRC FAN 1 + 2 IND PACK 1 + 2 Valve EXTRACT FAN CTL Landing Elevation IND Cockpit and Cabin Automatic and Manual TEMP CTL and IND AUTO PILOT AP OFF IND and DISC by Quick Disconnect COMMUNICATIONS CM1+2 Flight Interphones CM1+2 Audio Control Panels CM1 Cockpit Amplifier CVR / Passenger Address Mechanical CALL Cockpit and Cabin Crew CALL ELECTRICAL POWER DC SVCE/UTLY BUS 1 + 2 CTL MAIN BAT CHG IND INV 2 FAULT IND FIRE PROTECTION Avionics / Toilets SMK DET FWD and AFT COMPT SMK DET AFT COMPT and FWD COMPT /Toilets DET FANS CTL and IND FWD COMPT Fire Extinguishing CTL, IND and TEST (*) AUX AFT COMPT (*) See 2.42A for Cargo Operations FLIGHT CONTROLS Clutch Reengagement System (*) AILERON Locking CTL FUEL FQI 1 + 2 X FEED Valve Starting Pumps 1 + 2 Motive Flow Valves 1 + 2 HYDRAULIC GREEN PUMP CTL ICE AND RAIN PROTECTION DE-ICING ISOL Valves Side Windows ANTI-ICING IND CAPT/STBY/TAT PROBES IND CM1 Wiper INDICATING / RECORDING FDAU in flight LIGHTS Landing CTL NAVIGATION TAS TEMP IND OXYGEN PRESS IND Pilots and Pax Valves CTL Pax Masks DROP CTL PNEUMATIC BLEED Valves PWR and IND 1 + 2 PROPELLERS NP IND 1 + 2 PROP BRK PWR, CTL and IND ENGINES IGNITION and STARTING 1 + 2 NH/NL, ITT IND 1 + 2
Mod : 4116
NO
RM
AL
PR
OC
ED
UR
ES
3.0172
NORMAL PROCEDURESSEP 10 001
3 - NORMAL PROCEDURESAll steps have to be performed before the first flight of the day orfollowing a crew change or maintenance action. In other cases,start at FINAL COCKPIT PREPARATION.
PROCEDURE LISTED INCLUDE THE USE OF A GPUREFER TO PAGE 3.01A FOR HOTEL MODE.
EXTERIOR INSPECTION
CM1 CM2
Exterior walk around performed
PRELIMINARY COCKPIT PREPARATION
CM1 CM2CARGO DOOR CTL panel cover (ifinstalled)............................. CLOSEDEMER EQPT........................ CHECKGEAR PINS ...................ON BOARDC/Bs ..................................... CHECKBAT ..............................................ONMFC ..................................... CHECKPARKING BRK ............................ONPL 1 + 2 ...................CHECK AT G.I.GUST LOCK ......................ENGAGECL 1 + 2..............................FUEL SOFLAPS LEVER..................... CHECKEEC 1 + 2.....................................ONLDG GEAR.............................DOWNWIPERS .....................................OFFDC EXT PWR P/B........................ON
OVERHEAD PANEL ..............SCANANY WHITE LIGHT....EXTINGUISH
ANN LIGHT..............................TESTENG 1 FIRE.............................TESTPROP BRK (if installed) ..........ON / LOCKEDCVR .........................................TESTSIGNS PANEL..................... CHECKEMER EXIT LIGHT................... ARMEMER LOCK XMTR ...............AUTOCOMPT SMK (if installed)........TESTEXHAUST MODE .................RESETOVBD VALVE .........................AUTOOXYGEN PRESS ................ CHECKENG 2 FIRE.............................TEST
R
3.01A
72
NORMAL PROCEDURES APR 08 001
3 - NORMAL PROCEDURES
All steps have to be performed before the first flight of the day or following a crew change or maintenance action. In other cases, start at FINAL COCKPIT PREPARATION.
HOTEL MODE
EXTERIOR INSPECTION
CM1 CM2
Exterior walk around performed
PRELIMINARY COCKPIT PREPARATION
CM1 CM2
CARGO DOOR CTL panel cover (if installed)............................. CLOSED EMER EQPT........................ CHECK GEAR PINS ...................ON BOARD C/Bs ..................................... CHECK BAT ..............................................ON MFC ..................................... CHECK PARKING BRK ............................ON PL 1 + 2 ............................... CHECK GUST LOCK ..................... ENGAGE CL 1 + 2 ............................ FUEL SO FLAPS LEVER..................... CHECK EEC 1 + 2 ....................................ON LDG GEAR ............................DOWN WIPERS.....................................OFF ENG 2 FIRE.............................TEST PROP BRK (if installed)..........ON / LOCKED ATPCS.....................................TEST OVERHEAD PANEL ..............SCAN ANY WHITE LIGHT....EXTINGUISH ENG 2 START IN HOTEL MODE ANN LIGHT..............................TEST ENG 1 FIRE.............................TEST CVR .........................................TEST SIGNS PANEL..................... CHECK EMER EXIT LIGHT...................ARM EMER LOC XMTR..................AUTO AIR BLEED PANEL: ENG 1 BLEED FAULT and, X VALVE OPEN....................... ........... CHECK ILLUMINATED COMPT SMK (if installed)........TEST EXHAUST MODE .................RESET OVBD VALVE .........................AUTO OXYGEN PRESS ................ CHECK
3.02
72
NORMAL PROCEDURES APR 08 500
PRELIMINARY COCKPIT PREPARATION (CONT'D)
CM1 CM2
LEFT LATERAL CONSOLE N/W STEERING.......................... ON OXYGEN MASK (once a day) . CHECK MKR .........................................TEST GPWS ....................................NORM
LEFT INSTRUMENT PANEL NO FLAGS........................... CHECK CLOCK............................. SET TIME RMI / EHSI.......... CROSSCHECK HEADING ADC SW ..............SET TO ADEQUATE ADC
PEDESTAL FDEP (if applicable)............. CHECK TRIMS.................................. CHECK ATPCS (except ENG 2 in Hotel mode).......................................TEST TCAS (if installed)....... STBY / TEST VHF / NAV ...................................ON XPDR.......................................STBY IDLE GATE .......................... CHECK EMER AUDIO CANCEL ...... CHECK AIL LOCK LIGHT (if installed)................. CHECK EXTINGUISHED EFIS .............................................ON RADAR.....................................STBY
CENTRAL PANEL PWR MGT....................................TO PEC 1 + 2 ....................................ON HYD PRESS ........................ CHECK CAB PRESS MODE SEL.......NORM
RIGHT LATERAL CONSOLE OXYGEN MASK (once a day). CHECK
RIGHT INSTRUMENT PANEL NO FLAGS........................... CHECK CLOCK............................. SET TIME RMI / EHSI..........CROSSCHECK HEADING
Mod : 3973 or 4371 or 4457
3.02A
72
NORMAL PROCEDURES APR 08 200
COCKPIT DOOR DAILY CHECK (if applicable)
COCKPIT DOOR LOCKING SYSTEM SW .................................................ON In the cargo compartment, on the DOOR CALL panel: EMER PB................................................................................................ON CHECK OPEN LIGHT flashes In the cockpit: CHECK BUZZER CHECK OPEN LIGHT flashes If correct In the cockpit: TOGGLE SW ON COCKPIT DOOR CTL panel ...........................DENY CHECK BUZZER stops CHECK OPEN LIGHT extinguishes In the cargo compartment, on the DOOR CALL panel: CHECK OPEN LIGHT extinguishes and DENIED LIGHT illuminates If correct TOGGLE SW...........................................................................OPEN COCKPIT DOOR LOCKING SYSTEM SW................................OFF COCKPIT DOOR CTL panel FAULT LIGHT........................ CHECK FUNCTIONAL CHECK OF THE MANUAL LOCK BOLT(S)
3.03
72
NORMAL PROCEDURES APR 08 500
R FINAL COCKPIT PREPARATION
CM1 CM2
PARKING BRK ............ON / PRESS CHECK ALTIMETERS.............................SET COM / NAV / GPS......................SET FUEL QTY............................ CHECK MEMO PANEL ..................... CHECKPWR MGT....................................TO
ALTIMETERS.............................SET LANDING ELEVATION..............SET COM / NAV / GPS......................SET ENG F/U................................RESET
BEFORE PROPELLER ROTATION
CM1 CM2
TAIL PROP.................... ON BOARDDOORS ..............................CLOSED TO BUGS / APM * ............SET AND CHECK SEAT BELTS............................... ON BEACON ..................................... ON
TO BUGS / APM *.............SET AND CHECK TRIMS........................................SET CDLS * .........................................ON
BEFORE TAXI
CM1 CM2
PROP BRK.................................OFFCOCKPIT COM HATCH ................. CLOSED
CL 1 + 2 ..................................AUTO ANTI-ICING......................... AS RQD ANTI-SKID ...............................TEST FLAPS........................................SET
TAXI
CM1 CM2
TAXI & TO LIGHTS..................... ONBRAKES............................... CHECK RUDDER CAM...................CENTER TAKE OFF BRIEFING...COMPLETE
BRAKES............................... CHECK AFCS..........................................SET TO CONFIG .............................TEST TAKE OFF BRIEFING .. COMPLETE
* : if applicable
Mod : 3973 or 4371 or 4457
3.04
72
NORMAL PROCEDURES APR 08 050
R BEFORE TAKE OFF
CM1 CM2
FLIGHT CONTROLS ........... CHECK CCAS ...................................TO INHI EXT LIGHTS ............................... ON FD BAR (When lined up) ........... CENTERED
BLEED VALVES ................. AS RQD AIR FLOW..............................NORM GUST LOCK .................... RELEASE FLIGHT CONTROLS ........... CHECK XPDR / TCAS * ............. ALT / AUTO FD BAR (When lined up)............CENTERED
AFTER TAKE OFF
PF PNF
ALTIMETERS...... SET AND CHECK
LDG GEAR ..................................UP FLAPS............................................. 0 PWR MGT / NP.......... CLB / CHECK BLEED VALVES ..........................ON TAXI AND TO LIGHTS ..............OFF ALTIMETERS.......SET AND CHECK
ICING CONDITIONS
SEE 3.05
DESCENT
PF PNF
CCAS .........................................RCL LDG BUGS.......... SET AND CHECK ARRIVAL BRIEFING.....COMPLETE
LDG BUGS...........SET AND CHECK LDG ELEVATION.......................SET ARRIVAL BRIEFING..... COMPLETE
* : if applicable
Mod : 4111
3.05
72
NORMAL PROCEDURES APR 08 100
ENTERING ICING CONDITIONS
ANTI-ICING (PROP - HORNS - SIDE WINDOWS) .....................................ON
PROP MODE SEL.................................................................According to SAT NP .........................................................................................CONFIRM ≥ 86% PWR MGT ROTARY SELECTOR, if in cruise ......................CONFIRM CRZ 1
MINIMUM MANEUVER/OPERATING ICING SPEEDS..................BUGGED AND OBSERVED ICE ACCRETION .............................................................................MONITOR
AT FIRST VISUAL INDICATION OF
ICE ACCRETION AND AS LONG AS ICING CONDITIONS EXIST
ANTI-ICING (PROP - HORNS - SIDE WINDOWS) ...................CONFIRM ON ENG 1 + 2 DE-ICING ...................................................................................ON AIRFRAME DE-ICING .................................................................................ON ENG AND AIRFRAME MODE SEL.......................................According to SAT
MINIMUM MANEUVER/OPERATING ICING SPEEDS..................BUGGED AND OBSERVED BE ALERT TO SEVERE ICING DETECTION In case of severe icing, refer to 1.09
If significant vibrations occur BOTH CL ........................................100 OVRD for not less than 5 minutes
LEAVING ICING CONDITIONS
DE-ICING AND ANTI-ICING MAY BE SWITCHED OFF
WHEN THE AIRCRAFT IS VISUALLY VERIFIED CLEAR OF ICE
ICING AOA CAPTION MAY BE CANCELLED AND NORMAL SPEEDS MAY BE USED
Mod : 3973 or 4371
3.05A
72
NORMAL PROCEDURES MPC
APR 08 100
R
APPLICABLE TO AIRCRAFT FITTED WITH MODIFICATION 5567 or 8392 or 8442
APM TEST
DAILY CHECK MUST BE PERFORMED
APM PTT PB..................................PUSH and MAINTAIN for test duration
- CRUISE SPEED LOW lights on 13 VU (both sides) illuminate - over 1 second later, DEGRADED PERF lights on 13 VU (both sides) illuminate, with
CAUTION light and SC, with CRUISE SPEED LOW lights still illuminated - over 1 second later, INCREASE SPEED lights on 13 VU (both sides) illuminate flashing,
with CAUTION light and SC, with CRUISE SPEED LOW and DEGRADED PERF lights still illuminated
- over 1 second later, FAULT light on the 5VU illuminates, with CAUTION light, SC and ANTI-ICING (on CAP), with CRUISE SPEED LOW, DEGRADED PERF and INCREASE SPEED lights still illuminated
- end of test, the crew stop action on APM PTT TEST pushbutton, all lights shall extinguish.
CRUISE SPEED LOW
Appears in cruise only, to inform the crew that an abnormal drag increase induces a speed decrease of more than 10 KT compared with the expected speed
ICING CONDITIONS and SPEED .........................................MONITOR
3.06
72
NORMAL PROCEDURES APR 08 001
R APPROACH
PF PNF
ALTIMETERS...... SET AND CHECK
SEAT BELTS ...............................ON ALTIMETERS ......SET AND CHECK CABIN ALTITUDE................ CHECK
BEFORE LANDING
PF PNF
LDG GEAR........................ 3 GREEN FLAPS.................................. CHECK PWR MGT....................................TO TLU ......................................LO SPD ICING AOA LIGHT............... CHECK EXT LIGHTS ................................ON
AFTER LANDING
CM1 CM2
XPDR / TCAS * / RADAR ........STBY FLIGHT CONTROLS ......... LOCKED FLAPS............................................0° TRIMS...................................RESET LAND LIGHTS / STROBES .......OFF ANTI-/DE-ICING.........................OFF ENG START ROT SEL ..............OFF
After at least one minute CL 1 ..............FTR THEN FUEL SO
PARKING
CM1 CM2
PARKING BRK............................ ONTAXI & TO LIGHTS....................OFFCL 2............................................FTR PROP BRK (if installed) .............. ONBEACON ....................................OFFSEAT BELTS..............................OFF TAIL PROP................ ON POSITION
When leaving the aircraft OXYGEN MAIN SUPPLY........OFF ICE AND RAIN PROTECTION ............OFF EXT LIGHTS............................OFF EMER EXIT LIGHT...........DISARM EFIS / RADAR / COM / NAV................OFF CL 2 .................................FUEL SO FUEL PUMPS 1 + 2.................OFF CDLS *.....................................OFF BAT..........................................OFF
* : if applicable
OP
S D
ATA
4.0172
OPS DATASEP 04 001
4 – OPS DATA
COMMENTS :
- T/O SPEEDS COMPUTATIONValid for non limiting runways only
- LANDING SPEEDS COMPUTATIONThe approach speeds have been computed with 1.23 VS1G oflanding configuration or VMCL, whichever is higher
- GROSS CEILING COMPUTATION
For operational reasons, gross ceilings have been established withCG position : 25%
Eng : PW124/PW127
4.1172
OPS DATASEP 04 001
TAKE OFF TORQUE COMPUTED FOR VC = 50. KT
SAT (oC) PROPELLER SPEED 100 %
PRESSURE ALTITUDE (FT)AIRCOND.
OFF
1250$/
AIRCOND.
ON
HIGHAIR
COND.ON
-1000. 0. 1000. 2000. 3000. 4000. 5000. 6000. 7000. 8000. 8500.
- 40.- 10.- 8.- 6.- 4.
- 63.- 27.- 24.- 22.- 19.
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.089.0
90.090.089.288.287.2
- 2. 0. 2. 4. 6.
- 17.- 14.- 12.- 10.- 7.
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.089.688.587.4
88.087.085.984.983.8
86.285.184.183.182.1
8.10.12.14.16.
- 5.- 2. 0. 3. 5.
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.088.9
90.088.987.886.585.2
86.385.384.283.081.7
82.881.780.779.578.4
81.180.079.077.976.7
18.20.22.24.26.
8. 10. 13. 15. 18.
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.089.888.0
90.089.587.886.184.5
87.485.884.282.681.0
83.982.380.879.377.7
80.478.977.576.074.5
77.175.774.372.971.4
75.574.172.771.369.9
28.30.32.34.36.
20. 23. 25. 28. 30.
90.090.090.090.090.0
90.090.090.090.090.0
90.090.090.088.386.6
89.988.286.584.883.1
86.384.783.081.479.8
82.881.279.778.176.5
79.577.976.474.973.4
76.274.873.371.970.4
73.171.770.368.967.5
70.168.767.466.164.7
68.667.366.064.763.4
38.40.42.44.46.
33. 36. 38. 41. 43.
90.090.088.286.384.4
88.386.584.782.981.1
84.883.181.379.677.9
81.479.778.176.474.7
78.176.574.973.371.7
75.073.471.970.468.8
71.970.469.067.5
69.067.666.2
66.164.8
63.4 62.1
48.50.52.54.55.
46. 48. 51. 53. 54.
82.680.778.876.976.0
79.377.575.773.973.0
76.174.472.7
73.171.4
70.1
The part in bolt is the flat rated zone ; engine mechanical limit.
The part below is the area where the thermodynamical limit is reached first.
Note : Applicable for 0 < Vc < 60 kt
Eng : PW124
4.1272
OPS DATASEP 04 001
RESERVE TAKE OFF TORQUE COMPUTED FOR Vc = 50 KT
SAT (oC) PROPELLER SPEED 100 %
PRESSURE ALTITUDE (FT)AIRCOND.
OFF
1250$/
AIRCOND.
ON
HIGHAIR
COND.ON
-1000. 0. 1000. 2000. 3000. 4000. 5000. 6000. 7000. 8000. 8500.
- 40.- 10.- 8.- 6.- 4.
- 63.- 27.- 24.- 22.- 19.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.98.9
100.100.99.198.096.9
- 2. 0. 2. 4. 6.
- 17.- 14.- 12.- 10.- 7.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.99.698.497.2
97.896.695.594.393.1
95.794.693.592.391.2
8.10.12.14.16.
- 5.- 2. 0. 3. 5.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.98.7
100.98.897.596.194.7
95.994.793.592.290.8
92.090.889.788.487.1
90.188.987.886.585.3
18.20.22.24.26.
8. 10. 13. 15. 18.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.99.797.8
100.99.497.695.793.8
97.295.493.691.890.0
93.291.589.888.186.3
89.487.786.184.482.8
85.784.182.581.079.4
83.982.380.879.377.7
28.30.32.34.36.
20. 23. 25. 28. 30.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.98.296.2
99.998.096.194.292.3
95.994.192.390.488.6
92.090.388.586.885.0
88.386.684.983.381.6
84.783.181.579.878.2
81.279.778.176.675.0
77.876.474.973.471.9
76.274.873.371.970.4
38.40.42.44.46.
33. 36. 38. 41. 43.
100.100.98.095.993.8
98.196.194.192.190.1
94.292.390.488.486.5
90.588.686.784.983.0
86.885.083.381.579.7
83.381.679.978.276.5
79.978.376.675.0
76.675.173.5
73.572.0
70.5 69.0
48.50.52.54.55.
46. 48. 51. 53. 54.
91.789.687.685.584.5
88.186.184.182.181.1
84.682.780.8
81.279.4
77.9
The part in bolt is the flat rated zone ; engine mechanical limit.
The part below is the area where the thermodynamical limit is reached first.
Note : Applicable for 0 < Vc < 60 kt
Eng : PW124
4.1372
OPS DATASEP 04 001
GO AROUND TORQUE APPLICABLE FOR 0 ≤ Vc ≤ 125 kt
TAT (oC) PROPELLER SPEED 100. %
PRESSURE ALTITUDE (FT)AIRCOND.
OFF
1250$/
AIRCOND.
ON
HIGHAIR
COND.ON
-100.0. 0. 100.0. 2000. 3000. 4000. 5000. 6000. 7000. 8000. 8500.
- 40.- 10.- 8.- 6.- 4.
- 63.- 27.- 24.- 22.- 19.
- 71.- 35.- 32.- 30.- 27.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.99.2
100.100.99.398.297.1
- 2. 0. 2. 4. 6.
- 17.- 14.- 12.- 10.- 7.
- 25.- 22.- 19.- 17.- 14.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.99.898.697.4
98.096.995.794.693.4
96.094.893.792.691.4
8.10.12.14.16.
- 5.- 2. 0. 3. 5.
- 12.- 9.- 7.- 4.- 1.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.99.0
100.99.097.896.495.0
96.295.093.892.591.1
92.291.189.988.787.4
90.389.288.086.885.5
18.20.22.24.26.
8. 10. 13. 15. 18.
2. 4. 7. 10. 13.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.100.98.2
100.99.897.996.194.2
97.595.794.092.290.4
93.591.890.188.486.7
89.788.186.484.883.2
86.084.582.981.379.7
84.282.781.279.678.1
28.30.32.34.36.
20. 23. 25. 28. 30.
16. 18. 21. 24. 27.
100.100.100.100.100.
100.100.100.100.100.
100.100.100.98.596.5
100.98.496.594.692.7
96.394.492.890.889.0
92.490.688.987.185.4
88.687.085.383.681.9
85.083.481.880.278.6
81.580.078.576.975.4
78.276.775.273.872.3
76.675.173.772.270.8
38.40.42.44.46.
33. 36. 38. 41. 43.
30. 32. 35. 38. 41.
100.100.98.396.394.2
98.596.594.592.590.5
94.692.690.788.886.9
90.889.087.185.383.4
87.285.483.681.880.1
83.781.980.278.576.8
80.378.677.075.473.7
77.075.473.972.3
73.872.370.8
70.869.4
69.367.9
48.50.52.54.56.
46. 48. 51. 53. 55.
43. 46. 49. 52. 54.
92.190.087.985.983.8
88.586.584.582.580.5
84.983.081.179.2
81.679.777.9
78.376.5
75.1
The part in bolt is the flat rated zone ; engine mechanical limit.
The part below is the area where the thermodynamical limit is reached first.
Note : Add 0.8% for each 10 kt above 125 kt without exceeding 100% torque
Eng : PW124
4.3172
OPS DATASEP 04 010
13 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
100105
100105
FINAL TAKE OFF 108(Flaps 0)
107(Flaps 15)
DRIFT DOWN 107(Flaps 15)
MINI EN ROUTEVmLB 108
(Flaps 0) 132(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 87 92
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80100.2 102.3
438 413252 245275 267
101.1 102.3443 416252 244278 269
101.2 102.3446 418251 243279 270
99.1 102.3442 421248 242279 272
93.4 102.3426 423242 241274 273
88.3 96.9412 408236 235270 269
83.4 91.6396 392230 229266 264
100101.2 102.3
431 403251 243282 273
101.2 102.3434 406250 242284 274
100.5 102.3434 408249 241285 276
95.2 102.3418 411243 239281 277
89.8 98.2402 400236 235276 274
84.8 92.9388 386230 230271 270
80.1 87.9375 372225 224267 266
120101.2 102.3
427 397249 240288 278
100.1 102.3425 399247 239289 280
95.6 102.3409 402242 238286 281
91.1 99.3395 393237 235282 280
86.2 94.0380 378231 229278 276
81.3 88.9366 364225 224273 272
76.8 84.1354 351219 218269 267
14098.0 102.3412 396243 238290 284
94.5 102.3398 397240 236289 285
90.8 98.5385 384235 232287 283
86.5 94.2371 370230 228283 280
82.4 89.8359 357225 223279 277
77.9 85.0346 343219 218274 273
73.5 80.3334 331214 213270 269
16091.8 99.8385 386235 233289 287
88.9 96.5373 374232 229288 285
85.5 93.0361 361228 225286 283
82.0 89.1349 348224 221284 280
78.2 85.2337 336219 217280 277
74.4 81.1326 324213 212276 274
70.3 76.8314 312208 207271 270
18085.8 93.2359 360227 225288 286
83.1 90.4348 349224 222287 284
80.4 87.3338 338220 218286 282
77.3 84.1327 327217 214284 280
74.0 80.5316 315212 210280 277
70.6 77.0306 305207 205277 274
67.1 73.1296 294202 201272 270
20079.9 86.9333 336219 217287 285
77.5 84.2324 325216 214286 283
75.0 81.7314 316213 210284 282
72.6 78.8306 306209 207283 280
69.7 75.8296 296205 203280 277
66.7 72.5287 286200 198276 274
63.5 69.3278 276195 194272 270
22074.1 80.7310 313211 209285 283
72.0 78.3302 303208 206284 282
69.9 76.0293 294204 202283 280
67.6 73.6285 286201 199281 278
65.3 70.9277 277197 195279 276
62.7 68.2268 268193 191275 273
59.9 65.2260 259188 186271 269
24068.7 74.7290 292202 201283 281
66.7 72.6282 284199 198282 280
64.8 70.4274 275196 194280 278
62.8 68.3266 267193 191279 276
60.8 66.1259 260189 187277 274
58.5 63.6252 251185 183273 270
56.2 61.1244 244181 179270 266
25066.1 71.8281 283198 197282 280
64.2 69.8272 275195 193280 279
62.3 67.8265 267192 190279 277
60.4 65.7258 258188 186277 274
58.5 63.6251 251185 183275 272
56.5 61.4244 244181 179272 269
54.3 59.0237 236177 174269 265
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 Eng : PW124
4.3272
OPS DATASEP 04 010
14 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
100105
100105
FINAL TAKE OFF 112(Flaps 0)
111(Flaps 15)
DRIFT DOWN 111(Flaps 15)
MINI EN ROUTEVmLB 112
(Flaps 0) 137(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 90 96
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80100.5 102.3
439 413252 244275 267
101.2 102.3444 416252 243278 268
101.2 102.3447 418251 243279 270
99.1 102.3442 421248 242278 271
93.4 102.3426 423241 241273 273
88.3 96.9412 408236 235269 268
83.4 91.6396 392230 229265 264
100101.2 102.3
431 404251 243282 273
101.2 102.3434 406250 242284 274
100.4 102.3434 408248 240285 275
95.2 102.3418 411242 239280 277
89.8 98.1403 400236 235275 274
84.7 92.9389 386230 229271 270
80.1 87.8375 372225 223267 265
120101.2 102.3
427 397249 240288 278
100.1 102.3425 400247 239289 279
95.6 102.3409 402242 238285 281
91.0 99.2395 393236 234282 279
86.1 94.0380 378230 229277 275
81.2 88.8367 364224 223272 271
76.7 84.1354 351219 218268 267
14098.0 102.3412 396243 237290 283
94.4 102.3398 398239 236288 285
90.7 98.5385 384235 232286 282
86.5 94.2371 370230 227283 280
82.4 89.8359 357225 223279 276
77.8 85.0346 343219 217274 272
73.4 80.3334 331213 212269 268
16091.7 99.8384 386235 233289 286
88.8 96.4373 373231 229288 284
85.5 92.9361 361228 225286 282
82.0 89.1349 348223 221283 280
78.2 85.2337 336218 216279 277
74.4 81.0326 324213 211275 273
70.3 76.7314 312207 206271 269
18085.7 93.1358 360227 225288 285
83.0 90.3348 349223 221287 284
80.3 87.2338 338220 217285 282
77.2 84.0327 327216 213283 279
74.0 80.4316 315211 209280 277
70.5 76.9306 305206 205276 273
67.0 73.0296 294201 200271 269
20079.8 86.8333 336218 217286 284
77.4 84.1324 325215 213285 282
74.9 81.6314 315212 210284 281
72.5 78.7306 305209 206282 278
69.6 75.7296 295204 202279 276
66.6 72.4286 285199 197275 273
63.4 69.2278 276194 193271 269
22074.0 80.5310 312210 208284 282
71.9 78.2301 303207 205283 281
69.7 75.8293 294204 202282 279
67.5 73.5285 286200 198280 277
65.2 70.8277 276196 194277 274
62.5 68.0268 268192 190274 271
59.8 65.0260 259187 185270 267
24068.5 74.5289 292201 200281 280
66.6 72.4281 283198 197280 278
64.7 70.3274 275195 193279 276
62.7 68.1266 267192 190277 274
60.6 65.9259 259188 186275 271
58.4 63.4252 251184 181271 268
56.1 60.9244 244179 177268 264
25066.0 71.6281 282197 196280 279
64.0 69.6272 274194 192279 277
62.2 67.6265 266191 189277 275
60.3 65.5258 258187 185275 272
58.3 63.4250 251183 181273 269
56.4 61.1244 244180 177270 266
54.1 58.8237 236175 172266 262
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 Eng : PW124
4.3372
OPS DATASEP 04 010
15 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
100105
100105
FINAL TAKE OFF 116(Flaps 0)
115(Flaps 15)
DRIFT DOWN 115(Flaps 15)
MINI EN ROUTEVmLB 116
(Flaps 0) 142(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 94 99
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80100.8 102.3
440 414252 244275 267
101.2 102.3444 416252 243277 268
101.2 102.3447 419251 242279 270
99.1 102.3442 421248 241278 271
93.4 102.3426 423241 240273 272
88.3 96.8412 408235 234269 268
83.3 91.5396 391230 229265 263
100101.2 102.3
432 404251 242282 273
101.2 102.3434 406250 241283 274
100.4 102.3434 409248 240284 275
95.2 102.3418 411242 239280 276
89.7 98.1403 400236 234275 274
84.7 92.8389 386230 229271 269
80.0 87.8375 372224 223266 265
120101.2 102.3
427 397248 240287 278
100.0 102.3425 400247 239288 279
95.5 102.3409 402241 237285 280
91.0 99.2395 393236 234281 279
86.1 93.9380 378230 228277 275
81.2 88.8367 364224 223272 271
76.7 84.0354 351218 217268 266
14097.9 102.3412 396243 237290 283
94.4 102.3398 398239 236288 284
90.7 98.4385 384235 232286 282
86.4 94.1371 370229 227282 279
82.3 89.7359 357224 222278 276
77.8 84.9346 343218 217273 272
73.4 80.2334 331213 211269 267
16091.7 99.7384 386235 232289 286
88.7 96.4373 373231 228287 284
85.4 92.8361 361227 224285 282
81.9 89.0349 347223 220282 279
78.1 85.1337 336217 215278 276
74.3 81.0326 324212 211274 272
70.2 76.6315 312207 205270 268
18085.6 93.0358 360226 224287 285
82.9 90.2348 349223 220286 283
80.3 87.1338 338219 217284 281
77.1 83.9327 327215 213282 278
73.9 80.3316 315211 208278 275
70.4 76.8306 305205 204274 272
66.9 72.9296 294200 199270 268
20079.7 86.6333 335218 216285 283
77.3 84.0323 325214 212284 281
74.8 81.4314 315211 209283 280
72.4 78.5305 305208 205281 277
69.5 75.6296 295203 201278 275
66.5 72.3286 285198 196273 271
63.3 69.0278 276193 191270 267
22073.9 80.4309 312209 208283 281
71.8 78.0301 303206 204282 279
69.6 75.7293 293203 200280 277
67.4 73.3284 285199 197279 275
65.0 70.6277 276195 193276 272
62.4 67.9268 267190 188272 269
59.7 64.9260 259186 183268 264
24068.4 74.3289 291200 199280 278
66.4 72.2281 283197 195279 277
64.5 70.1273 274194 192277 274
62.5 67.9266 266190 188275 272
60.4 65.7259 259186 184272 269
58.2 63.2252 251182 179269 265
55.9 60.7244 244178 174265 261
25065.8 71.4280 282196 194279 277
63.8 69.4271 274192 191277 275
62.0 67.4264 266189 187275 273
60.1 65.2257 257186 183273 269
58.1 63.1250 251182 179270 266
56.2 60.9244 243178 174267 262
53.9 58.5237 236173 170263 258
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 Eng : PW124
4.3472
OPS DATASEP 04 010
16 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
100105
100105
FINAL TAKE OFF 120(Flaps 0)
120(Flaps 15)
DRIFT DOWN 120(Flaps 15)
MINI EN ROUTEVmLB 120
(Flaps 0) 146(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 97 103
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80101.1 102.3
441 414252 244275 266
101.2 102.3444 416251 243277 268
101.2 102.3447 419250 242278 269
99.0 102.3442 421247 241278 271
93.4 102.3426 423241 240273 272
88.3 96.8412 408235 234269 267
83.3 91.5396 391229 228264 263
100101.2 102.3
432 404250 242281 272
101.2 102.3434 406249 241283 273
100.4 102.3434 409248 240284 275
95.1 102.3418 411242 238279 276
89.7 98.1403 400235 234274 273
84.7 92.8389 386229 228270 269
80.0 87.7375 372224 222266 264
120101.2 102.3
427 398248 239287 277
100.0 102.3424 400246 238288 279
95.5 102.3409 402241 237285 280
90.9 99.1395 393236 233281 278
86.1 93.9380 378229 228276 274
81.2 88.7367 364223 222271 270
76.6 84.0354 351218 216267 265
14097.9 102.3412 396242 237289 282
94.3 102.3398 398238 235287 284
90.6 98.4385 384234 231285 281
86.4 94.0371 370229 226281 278
82.2 89.6359 357223 221277 275
77.7 84.8346 344217 216272 271
73.3 80.1334 331212 210268 266
16091.6 99.6384 386234 232288 285
88.7 96.3372 373231 228287 283
85.3 92.7361 361227 224284 281
81.8 88.9349 347222 219281 278
78.0 85.0337 336217 215277 275
74.2 80.9326 324211 210273 271
70.1 76.5315 312206 204269 267
18085.5 92.9358 360226 223286 284
82.8 90.1347 348222 220285 282
80.2 87.0337 337219 216283 280
77.0 83.7327 326214 212281 277
73.8 80.2316 315210 207277 274
70.3 76.7306 305204 203273 271
66.9 72.8296 294199 197269 266
20079.5 86.5332 335217 215284 282
77.1 83.8323 324214 211283 280
74.7 81.3314 315210 208281 278
72.2 78.4305 305207 204279 276
69.3 75.4296 295202 200276 273
66.3 72.1286 285197 195272 269
63.2 68.9278 276192 190268 265
22073.7 80.2309 312208 206282 280
71.6 77.9301 302205 203280 278
69.5 75.5292 293201 199279 276
67.2 73.1284 285198 195277 273
64.8 70.4276 276193 191273 270
62.2 67.7268 267189 186270 266
59.5 64.7260 259184 181266 261
24068.2 74.1289 291199 197278 276
66.2 72.0280 282196 194277 274
64.3 69.8273 274192 190275 272
62.3 67.6265 266189 186273 269
60.2 65.4258 259185 182270 266
58.0 62.9251 251180 177267 261
55.7 60.4244 243176 172262 256
25065.6 71.1280 281194 193276 275
63.6 69.1271 273191 189275 272
61.7 67.1264 265187 185273 270
59.9 64.9257 257184 181271 266
57.9 62.8250 250180 176268 262
55.9 60.5243 243176 171264 258
53.7 58.2236 236171 166260 253
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 Eng : PW124
4.3572
OPS DATASEP 04 010
17 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
100105
104108
FINAL TAKE OFF 124(Flaps 0)
124(Flaps 15)
DRIFT DOWN 124(Flaps 15)
MINI EN ROUTEVmLB 124
(Flaps 0) 151(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 100 107
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80101.2 102.3
442 414252 243275 266
101.2 102.3444 416251 242277 267
101.2 102.3447 419250 242278 269
99.0 102.3442 421247 241277 270
93.3 102.3426 424240 240272 271
88.2 96.8412 409235 233268 267
83.3 91.5396 391229 227264 262
100101.2 102.3
432 404250 242281 272
101.2 102.3434 406249 240283 273
100.3 102.3434 409247 239283 274
95.1 102.3418 411241 238279 275
89.7 98.0403 400235 233274 272
84.6 92.7389 386229 228269 268
80.0 87.7375 371223 221265 263
120101.2 102.3
427 398248 239287 277
99.9 102.3424 400246 238287 278
95.4 102.3409 402241 237284 279
90.9 99.1395 393235 233280 277
86.0 93.8380 378229 227275 273
81.1 88.7367 364223 221270 269
76.6 83.9354 351217 215266 264
14097.8 102.3411 396242 236289 282
94.2 102.3398 398238 235287 283
90.5 98.3385 384234 230284 281
86.3 94.0371 370228 226280 277
82.1 89.5359 357223 221276 274
77.7 84.8346 344217 215271 270
73.3 80.1334 331211 209267 265
16091.5 99.5384 386233 231287 284
88.6 96.2372 373230 227286 282
85.2 92.6361 361226 223284 280
81.7 88.8349 347221 218280 277
77.9 84.9337 336216 214276 274
74.2 80.8326 324210 209272 270
70.1 76.4315 313205 203267 265
18085.4 92.8358 360225 223285 283
82.7 89.9347 348221 219284 281
80.0 86.8337 337218 215282 279
76.9 83.6327 326213 211279 276
73.6 80.1316 315208 206276 273
70.2 76.5306 305203 201271 269
66.8 72.7296 294198 196267 264
20079.4 86.3332 335216 214283 281
77.0 83.7323 324213 210282 279
74.6 81.1313 314209 207280 277
72.1 78.2305 305205 203278 274
69.2 75.3295 295200 198274 271
66.2 72.0286 285196 193270 267
63.1 68.7278 276191 188266 262
22073.6 80.0308 311207 205280 278
71.5 77.6300 302203 201279 276
69.3 75.2292 293200 198277 274
67.0 72.9284 285196 194274 271
64.7 70.2276 276192 189271 267
62.1 67.4268 267187 184267 263
59.3 64.4260 259182 179263 258
24068.0 73.8288 290197 196276 274
66.0 71.7280 282194 192275 272
64.1 69.5272 273190 188273 269
62.0 67.3265 265187 183270 265
60.0 65.1258 258183 179267 262
57.8 62.6251 250178 174263 257
55.5 60.1244 243173 168259 251
25065.3 70.8279 280192 191274 272
63.3 68.7270 272189 187272 269
61.5 66.7263 264185 182270 266
59.6 64.5256 256182 178267 262
57.6 62.4249 249178 173264 258
55.7 60.1243 242173 168260 252
53.4 57.7236 235168 162255 246
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 Eng : PW124
4.3772
OPS DATASEP 04 010
19 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
107111
111115
FINAL TAKE OFF 132(Flaps 0)
131(Flaps 15)
DRIFT DOWN 131(Flaps 15)
MINI EN ROUTEVmLB 132
(Flaps 0) 160(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 106 114
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80101.2 102.3
442 414251 242274 265
101.2 102.3445 417250 241276 266
101.2 102.3447 419249 240277 267
98.9 102.3442 422246 239276 269
93.2 102.2426 424239 238271 270
88.1 96.6412 409234 232267 265
83.2 91.3396 391227 226262 260
100101.2 102.3
432 404249 241280 271
101.2 102.3435 407248 239282 272
100.2 102.3434 409246 238282 273
95.0 102.3418 412240 237277 274
89.6 97.9403 400233 232272 271
84.5 92.6389 386227 226268 266
79.9 87.5375 371221 220263 261
120101.2 102.3
428 398247 238286 275
99.8 102.3424 401245 237286 277
95.2 102.3408 403239 235282 278
90.7 98.9395 393233 231278 276
85.8 93.6380 378227 226273 271
81.0 88.5367 364221 219269 267
76.5 83.7354 351215 213264 261
14097.6 102.3411 397241 235287 280
94.1 102.1398 398237 234285 282
90.3 98.0385 383232 229282 279
86.1 93.7371 370226 224278 275
81.9 89.3359 357221 219274 272
77.5 84.5346 344215 213269 267
73.1 79.8334 332209 207264 261
16091.2 99.2383 385232 229285 282
88.3 95.9372 372228 225284 280
85.0 92.3360 360224 221281 278
81.5 88.5349 347219 216278 274
77.6 84.6337 336213 211273 271
73.9 80.5326 324208 206269 266
69.9 76.1315 313202 200264 261
18085.1 92.4357 359223 221283 280
82.4 89.6346 347219 217281 278
79.7 86.5336 337216 212279 276
76.5 83.2326 326211 208276 273
73.4 79.7316 315206 203272 269
69.9 76.1306 305201 198268 264
66.5 72.3297 295195 192263 259
20079.0 85.9331 334214 211280 277
76.6 83.2322 323210 207278 275
74.2 80.6313 314206 204276 273
71.7 77.8304 304202 199273 270
68.8 74.7295 294197 194270 265
65.9 71.5286 285192 188265 260
62.7 68.2278 276187 182260 255
22073.1 79.4307 310204 202276 274
71.0 77.1299 301200 198274 271
68.8 74.6291 291197 193272 268
66.5 72.2283 283192 189269 264
64.2 69.5275 275188 183266 259
61.6 66.7267 267183 178261 254
58.9 63.7260 258177 171256 247
24067.4 73.1286 288193 191271 268
65.4 70.9278 280190 186269 264
63.5 68.7271 271186 182266 260
61.4 66.4263 263182 176263 255
59.3 64.1257 257177 171259 250
57.2 61.6250 249172 165254 244
54.8 59.2243 242166 159248 238
25064.7 69.9277 278188 185268 264
62.7 67.8268 270184 180265 260
60.8 65.7261 262180 175262 255
58.9 63.4254 254175 169259 249
56.8 61.3248 247170 163254 244
54.9 59.2242 241165 159249 239
52.7 56.8235 234159 152242 231
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 Eng : PW124
4.3872
OPS DATASEP 04 040
20 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
111114
115118
FINAL TAKE OFF 135(Flaps 0)
135(Flaps 15)
DRIFT DOWN 135(Flaps 15)
MINI EN ROUTEVmLB 135
(Flaps 0) 164(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 110 117
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80101.2 102.3
442 415250 242273 264
101.2 102.3445 417249 241275 265
101.2 102.3448 420249 240277 267
98.8 102.3442 422245 239275 268
93.2 102.1427 424239 238270 269
88.1 96.6412 409233 231266 264
83.1 91.2396 391227 225261 259
100101.2 102.3
433 405249 240280 270
101.2 102.3435 407248 239281 271
100.1 102.3434 410246 237281 272
94.9 102.3418 412239 236277 273
89.5 97.8403 400233 231272 270
84.4 92.5389 386227 225267 265
79.8 87.4375 371221 218262 260
120101.2 102.3
428 399246 237285 275
99.7 102.3424 401244 236285 276
95.1 102.3408 403238 235282 277
90.6 98.8395 393233 230277 275
85.8 93.5381 378226 225272 270
80.9 88.4367 364220 218267 265
76.4 83.6354 351214 212262 260
14097.5 102.3411 397240 234286 280
93.9 102.0397 398236 233284 280
90.2 97.9385 383231 228281 278
86.0 93.6371 370225 223277 274
81.8 89.2359 357219 217272 270
77.4 84.4346 344214 211268 265
73.0 79.7334 331208 205262 259
16091.1 99.0383 385231 228284 281
88.2 95.7371 372227 224283 279
84.8 92.1360 360223 220280 276
81.3 88.4348 347217 215276 273
77.5 84.4337 336212 210272 269
73.8 80.3326 324207 204267 264
69.7 76.0315 313201 197262 258
18084.9 92.2356 358222 219282 279
82.2 89.3346 347218 215280 276
79.5 86.3336 336214 211277 274
76.3 83.0326 325209 206274 270
73.2 79.5315 314204 201270 266
69.8 75.9306 305199 195266 261
66.4 72.1297 294193 189260 255
20078.8 85.6331 333212 210278 275
76.4 82.9322 323208 206276 273
73.9 80.3312 313204 201274 270
71.4 77.4304 304200 197271 266
68.6 74.4295 294195 191267 262
65.7 71.2286 285190 185263 256
62.5 67.8278 276184 179257 249
22072.8 79.1306 309202 200274 271
70.7 76.7298 300198 195272 267
68.5 74.2290 290194 190269 264
66.2 71.8282 283190 186266 260
63.9 69.0275 274185 180262 254
61.3 66.2267 266180 173257 248
58.6 63.3260 258174 167251 241
24067.1 72.5286 287191 188268 263
65.0 70.3277 278187 183265 259
63.1 68.0270 270183 177262 254
61.0 65.7262 262178 171258 248
58.9 63.5256 256173 166253 243
56.8 61.2250 248167 160248 237
54.3 58.6242 241161 152240 228
25064.4 69.3276 276185 181264 258
62.2 67.1267 268181 175261 253
60.3 64.9260 260176 169257 247
58.4 62.8253 253171 164252 242
56.3 60.7247 247165 158247 236
54.3 58.4241 240160 151241 227
51.9234150229
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 + 2735 Eng : PW124
4.3972
OPS DATASEP 04 040
21 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
114117
118121
FINAL TAKE OFF 138(Flaps 0)
138(Flaps 15)
DRIFT DOWN 138(Flaps 15)
MINI EN ROUTEVmLB 138
(Flaps 0) 168(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 113 120
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80101.2 102.3
443 415250 241273 263
101.2 102.3445 418249 240274 265
101.2 102.3448 420248 239276 266
98.8 102.3442 422244 238274 267
93.1 102.0427 424238 237270 268
88.0 96.5412 409232 230265 263
83.0 91.1395 391226 224260 258
100101.2 102.3
433 405248 239279 269
101.2 102.3435 408247 238280 270
100.0 102.3434 410245 237281 271
94.8 102.3418 412238 235276 272
89.4 97.7403 400232 230271 269
84.4 92.4389 386226 224266 263
79.7 87.3375 371219 217261 258
120101.2 102.3
428 399246 236285 274
99.6 102.3424 401243 235284 275
95.0 102.3408 403237 234280 276
90.5 98.7394 393232 229276 274
85.7 93.4381 378225 223271 269
80.8 88.3367 365219 217266 263
76.3 83.5354 351213 210261 258
14097.3 102.3410 398239 233286 279
93.8 101.8397 397235 232283 279
90.0 97.8384 383230 227280 276
85.8 93.4370 370224 222275 272
81.7 89.1359 357218 216271 268
77.3 84.3346 344212 210266 263
72.9 79.6334 331206 203261 257
16090.9 98.8383 384230 227283 280
88.0 95.5371 372226 223281 277
84.6 91.9360 360221 218278 274
81.2 88.2348 347216 213274 271
77.4 84.2337 336211 208270 266
73.7 80.2326 324205 202265 261
69.6 75.8315 312199 195260 255
18084.7 92.0356 358221 218280 277
82.0 89.1345 346217 214278 274
79.2 86.0336 336212 209275 271
76.2 82.7325 325207 204272 268
73.0 79.2315 314202 199268 263
69.6 75.6306 305197 193263 258
66.2 71.8297 294191 186258 251
20078.5 85.3330 332210 208276 273
76.2 82.6321 322207 204274 270
73.6 79.9311 312202 199271 267
71.2 77.1303 303198 194268 262
68.3 74.0294 294193 188264 257
65.4 70.7286 285187 181259 251
62.2 67.4277 275181 174252 244
22072.5 78.6305 308200 197271 267
70.4 76.2298 299196 192269 263
68.2 73.7289 289192 187266 259
65.9 71.2281 282187 181262 254
63.6 68.5275 274182 175258 247
60.9 65.8267 265176 169252 241
58.2 62.9259 257169 162244 234
24066.7 71.9284 285188 183264 257
64.6 69.6276 277184 178260 252
62.6 67.3269 268179 171257 246
60.5 65.1261 261174 166252 241
58.3 62.8255 254168 160246 234
56.2 60.2249 247161 151239 224
53.4241149223
25063.9 68.5275 274182 176259 251
61.7 66.3266 266176 169255 244
59.7 64.3259 259171 164250 240
57.8 62.0252 251166 157245 232
55.6 59.5245 245158 147236 219
53.1239146221
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 + 2735 Eng : PW124
4.4072
OPS DATASEP 04 040
21.5 tSpeeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
115118
120123
FINAL TAKE OFF 140(Flaps 0)
140(Flaps 15)
DRIFT DOWN 140(Flaps 15)
MINI EN ROUTEVmLB 140
(Flaps 0) 170(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 114 121
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80101.2 102.3
443 415250 241273 263
101.2 102.3445 418249 240274 264
101.2 102.3448 420248 239275 266
98.7 102.3442 423244 238274 267
93.1 102.0427 424238 236269 268
88.0 96.4412 409232 230265 262
83.0 91.1395 391225 223260 257
100101.2 102.3
433 405248 239278 268
101.2 102.3435 408247 238280 270
99.9 102.3434 410244 236280 271
94.7 102.3418 413238 235275 272
89.4 97.6403 400231 230270 268
84.3 92.3389 386225 223265 263
79.7 87.3375 371219 216260 257
120101.2 102.3
428 399245 236284 273
99.5 102.3424 401243 235284 274
95.0 102.3408 404237 233280 276
90.4 98.6394 393231 229275 273
85.6 93.4381 378225 223270 268
80.8 88.2367 365218 216265 263
76.2 83.4354 351212 209260 257
14097.3 102.3410 398239 233285 278
93.7 101.7397 397235 231283 279
89.9 97.7384 383229 226279 275
85.7 93.3370 370223 221274 272
81.6 89.0359 357218 215270 267
77.3 84.2346 344212 209265 262
72.8 79.5334 331205 202260 255
16090.8 98.7382 384230 227282 279
87.9 95.4371 372226 222281 276
84.5 91.8359 359221 218277 273
81.1 88.0348 347215 212273 270
77.3 84.1337 335210 207269 265
73.6 80.0326 325204 201264 260
69.5 75.7315 312198 194258 253
18084.6 91.8356 357220 217279 276
81.9 88.9345 346216 213277 273
79.1 85.9335 336211 208274 270
76.0 82.6325 325206 203270 266
72.9 79.1315 314201 197267 261
69.5 75.4306 305196 191262 256
66.1 71.7297 294189 184256 248
20078.4 85.1330 332210 207275 272
76.0 82.4321 321206 202273 268
73.5 79.7311 312201 198270 265
71.1 76.9303 303197 192267 260
68.2 73.8294 294192 186262 255
65.3 70.5286 284186 179257 248
62.1 67.3277 274179 172250 241
22072.3 78.4305 307199 195269 265
70.2 75.9297 298195 190267 261
68.0 73.4289 289190 185264 256
65.7 70.9281 281186 179260 250
63.4 68.2274 273180 172255 244
60.7 65.5266 265174 166248 238
58.0 62.5259 256167 158241 228
24066.5 71.5284 284186 181261 254
64.3 69.2275 276182 175258 248
62.3 67.0268 268177 169253 243
60.2 64.7261 260171 163248 236
58.0 62.3254 253165 155241 227
55.6248155230
25063.6 68.0274 273180 172256 246
61.4 65.9265 265174 167251 241
59.4 63.7258 258169 160246 234
57.3 61.3251 250161 151238 223
54.9244151225
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 + 2735 Eng : PW124
4.4172
OPS DATASEP 04 040
22 tNever exceed certified weight limitations
Speeds Normal Icing
NON LIMITING RWYTAKE-OFFFLAPS 15
V1 = VRV2
117120
121124
FINAL TAKE OFF 142(Flaps 0)
142(Flaps 15)
DRIFT DOWN 142(Flaps 15)
MINI EN ROUTEVmLB 142
(Flaps 0) 172(Flaps 0)
FINALAPPROACH
VmHB(Flaps 30) 115 122
MAX CRUISE 2 ENGINES∆ ISA
FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20
80101.2 102.3
443 415249 240272 262
101.2 102.3445 418248 239274 264
101.2 102.3448 420247 238275 265
98.7 102.3442 423244 237274 266
93.1 101.9427 424237 236269 267
87.9 96.4412 408231 229264 262
83.0 91.0395 391225 222259 256
100101.2 102.3
433 405247 238278 268
101.2 102.3436 408246 237280 269
99.9 102.3434 410244 236279 270
94.7 102.3418 413237 235274 271
89.3 97.6403 401231 229270 267
84.3 92.2389 386225 222264 262
79.6 87.2375 371218 216259 256
120101.2 102.3
428 399245 235284 273
99.4 102.3424 402242 234283 274
94.9 102.3408 404236 233279 275
90.3 98.5394 393230 228275 272
85.6 93.3381 378224 222270 267
80.7 88.1367 365218 215265 262
76.2 83.3354 351211 208259 256
14097.2 102.3410 398238 232284 277
93.6 101.6397 397234 230282 278
89.8 97.6384 383229 226278 275
85.7 93.2370 369222 220274 271
81.6 88.9359 357217 214269 266
77.2 84.1346 344211 208264 260
72.8 79.4334 331204 201258 254
16090.7 98.6382 384229 226282 278
87.8 95.3371 372225 222280 276
84.4 91.7359 359220 217276 272
81.0 87.9348 347214 211272 268
77.2 84.0337 335209 206268 264
73.5 79.9326 325203 200263 258
69.4 75.5315 312197 192257 251
18084.5 91.7355 357219 216278 275
81.7 88.8345 346215 212276 272
79.0 85.7335 335210 207273 269
75.9 82.4325 325205 202269 264
72.8 78.9315 314200 196265 259
69.4 75.3306 304195 189260 253
65.9 71.5296 293188 182254 245
20078.2 84.9329 331208 206274 270
75.9 82.2320 321205 201271 266
73.4 79.5311 312200 196268 263
70.9 76.6303 303196 190265 258
68.0 73.5294 293190 184260 252
65.1 70.3286 283184 177254 244
61.9 67.1277 274177 170247 238
22072.1 78.1305 306197 193268 262
70.0 75.6297 297193 188265 258
67.8 73.0289 288189 182262 252
65.5 70.5281 281184 176257 246
63.1 67.9274 272178 170252 241
60.5 65.1266 264171 163245 233
57.7 61.9258 255162 151234 219
24066.2 71.1283 283184 178259 250
64.0 68.8275 275179 172255 244
62.0 66.6267 267174 166250 239
59.9 64.2260 259168 158244 230
57.5 61.0253 250159 142234 209
25063.3 67.7273 272177 170253 242
61.0 65.4264 264171 163247 236
58.9 63.1257 256164 154240 226
56.6250155229
TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS
127�7+(502�/,0,7('
Mod : 1368 + 2735 Eng : PW124
4.6172
OPS DATASEP 04 001
For weight in KG, use white boxes.For weight in LB, use shaded boxes.
SINGLE ENGINE GROSS CEILING (FT)
NORMAL CONDITIONS (FLAPS 0)
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:(,*+7[������OE
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Eng : PW124
R
4.6272
OPS DATASEP 05 040
For weight in KG, use white boxes.For weight in LB, use shaded boxes.
SINGLE ENGINE GROSS CEILING (FT)
ICING CONDITIONS (FLAPS 15)
WEIGHTx 1000 kg ISA - 10 ISA ISA + 10 ISA + 15 ISA + 20 WEIGHT
x 1000 lb
13.0 25000 25000 24800 24500 23500 23200 22800 22500 22200 21900 29
14.0 24100 24000 22700 22500 21300 21200 20700 20500 19800 19700 31
15.0 22000 22100 20600 20700 19200 19300 18500 18500 17600 17600 33
16.0 20000 20200 18600 18800 17200 17400 16300 16600 15600 15800 35
17.0 18100 18500 16700 17100 15200 15700 14400 14800 15100 15100 37
18.0 16400 16900 15000 15500 13400 13900 12700 13200 - 15100 39
19.0 14800 15400 13400 14000 11700 12400 12600 12600 - - 41
20.0 13300 14000 11900 12600 10000 10900 12600 12600 - - 43
21.0 11800 12700 10300 11200 10000 10000 - - - - 45
21.5 11100 11300 9500 9700 10000 10000 - - - - 47
22.0 10300 10300 8600 8600 10000 10000 - - - - 48.5
Note : When bolt-underligned figures, icing conditions do not exist.
R
Mod : 1368 + 2735 Eng : PW124
4.6372
OPS DATASEP 04 001
REDUCED FLAPSLANDING CONFIGURATION
VAPP (kt)NOTE : For a go around flaps 15 configuration increase speed up to VmLB0
before selecting flaps 0
FLAPS 0VmHB0 + 5 kt
FLAPS 15VmHB15
.*
WEIGHT(x 1000kg) Normal Icing Normal Icing
13 118 141 96 11214 122 145 99 11715 126 151 103 12216 130 156 106 12617 134 161 109 13018 138 165 113 13419 142 170 116 13720 146 174 119 14121 149 178 123 145
21.350 149 178 125 147
FLAPS 0VmHB0 + 5 kt
FLAPS 15VmHB15
/E
WEIGHT(x 1000Lb) Normal Icing Normal Icing
29 119 142 96 11331 122 146 99 11733 126 151 103 12235 130 156 106 12537 133 160 109 12939 137 164 112 13341 141 168 115 13743 144 173 118 14045 147 176 121 14347 150 179 124 146
Eng : PW127EEng : PW124
4.6472
OPS DATASEP 04 001
1.1 VMCA IAS * OAT °C
ZP (ft)-30 -20 -10 0 + 10 + 20 +30 + 40 + 50
0 105 105 104 103 102 102 101 99 95
2000 104 103 102 102 101 100 99 96 92
4000 103 102 101 100 100 98 96 92 89
6000 101 100 100 99 97 95 92 89 86
8500 99 98 97 95 93 91 88 85 82
* Conservative values calculated for the maximum landing weight.
Eng : PW124
R
4.65
72
OPS DATA SEP 10 600
PW127F / PW127M ACTUAL LANDING DISTANCE (M) - SEA LEVEL
NORMAL CONDITIONS - FLAPS 30 WEIGHT (1000 KG) 13 14 15 16 17 18 19 20 21 22 22.5 23
DRY 570 570 570 570 570 590 610 630 650 670 680 700
WET 690 690 690 690 700 730 760 780 810 840 850 860
WATER OR
SLUSH <1/2 in
640 680 710 750 780 820 860 900 940 980 1000 1020
COMPACT SNOW 690 720 760 790 830 860 900 930 970 1000 1020 1030 R
UN
WA
Y C
ON
DIT
ION
CO
NT
AM
INA
TE
D B
Y
ICE 1010 1070 1120 1170 1230 1280 1340 1390 1450 1500 1530 1560
ICING CONDITIONS – FLAPS 30
WEIGHT (1000 KG) 13 14 15 16 17 18 19 20 21 22 22.5 23
DRY 610 610 620 620 620 640 670 690 710 740 750 770
WET 760 760 760 760 770 800 830 860 890 920 940 950
WATER OR
SLUSH <1/2 in
700 740 780 820 860 900 950 990 1040 1080 1100 1130
COMPACT SNOW 760 800 840 880 920 960 1000 1040 1080 1120 1140 1160 R
UN
WA
Y C
ON
DIT
ION
CO
NT
AM
INA
TE
D B
Y
ICE 1140 1200 1260 1320 1390 1450 1520 1580 1640 1710 1740 1770
CORRECTION ON LANDING DISTANCES
-Wind : • dry or wet runway add 10% per 5 kt tailwind. subtract 2% per 5 kt headwind. • contaminated runway add 16% per 5 kt tailwind. subtract 2% per 5 kt headwind. -Airport elevation : • dry or wet runway add 3% per 1000 ft above sea level. • contaminated runway add 5% per 1000 ft above sea level.
-Effect of reverse : landing distances are decreased by : • 2% on dry runway. • 4% on wet runway. • 8% on runway contaminated by water or slush. • 10% on runway contaminated by compact snow. • 30 % on runway contaminated by ice.
CAUTION: On contaminated runway, performances without reverser only are to be used for flight preparation.
NOTE: Landing on damp runway.
A runway is damp when it is not perfectly dry, but when the water which is on it does not give it a shiny appearance. For damp runway, we consider no performance limitation.
Mod : 5561 Model : 212A
R
5.01
72
CHECK LIST L.T.R.
List of Temporary Revisions MAY 11 089
NO
TR EDITION DATE DESTROYED INSERTION
DATE REASON
01 MAR 07 AT REV 27 DATED SEP 07 TR 11 ENV
02 12DEC07 AT REV 28 DATED APR 08 MOD 5561
03 JUN 08 AT REV 29 DATED OCT 08 TR 13 ENV
04 31MAY10 AT REV 33 DATED SEP 10 Cockpit door
05 MAY 11 TR 16 ENV
5.05
72
CHECK LIST
L.N.R. List of Normal Revisions SEP 10 001
REV EDITION DATE
INSERTION DATE REMARKS
00 OCT 89
01 DEC 89
02 MAR 90
03 NOV 90
04 MAY 91
05 NOV 91
06 MAY 92
07 NOV 92 TOTAL EDITION
08 MAY 93 TOTAL EDITION
09 NOV 93 TOTAL EDITION
10 JUN 94
11 DEC 94
12 JUN 95
13 DEC 95
14 JUN 96
15 DEC 96
16 JUN 97
17 DEC 97
18 JUL 98
19 JUL 99
20 JUL 00
21 JUL 01
22 SEP 02
23 SEP 03
24 SEP 04 TOTAL WORD EDITION
25 SEP 05
26 SEP 06
27 SEP 07
28 APR 08
29 OCT 08
30 OCT 09
31 SEP 10
5.06
72
CHECK LIST
R.N.R. Reason of Normal Revisions SEP 10 001
REV EDITION DATE REASON FOR ISSUE CHAP
INVOLVED
31 SEP 10 EMERGENCY PROCEDURES AIR COND SMOKE: amber engine “caution”. RECOVERY AFTER STALL or ABNORMAL ROLL CONTROL: procedure reviewed. PROCEDURES FOLLOWING FAILURES Contents page updated. ENG NAC OVHT: wording improvement. ABNORMAL ENG PARAMETERS IN FLIGHT: procedure reviewed. ONE EEC FAULT: wording correction “UNCOMMANDED 100%NP ON ONE OR TWO PROPELLERS”: content and title changed (instead of “ONE PROPELLER REMAINING….POWER SELECTION”). PROP OVER LIMIT: procedure reviewed. DC GEN FAULT: correction of a missing item. ANTI SKID FAULT: anti skid set to OFF item added. SMK DET FANS FAULT: content and title changed to generalize. PRELIMINARY COCKPIT PREPARATION : PL 1+2: check at ground idle. Speeds adjusted and 23T performances completion.
1.05A 1.10
2.01, 2.03 2.06
2.09 2.10A
2.11 2.18 (_550variant)
2.25
2.33
3.01 & 6.01
4.63 & 4.65
QRH QUICK REFERENCE HANDBOOK 5-07 page 1-089
ATR72
S.N.N.P.Shipping Note Normal Pages
SEP 10
Action P CH SE Page Seq Date Validation Criteria
Turn NO
" ADD " = Add "DESTROY" = Destroy " …….." = Revised
"SEE VAL" = See Validation
DESTROY TR 004
...... 1 05A 001 SEP 10
...... 1 09 001 SEP 04 PW1241 10 001 SEP 10
...... 1 09 100 APR 08 PW127-127F-127M1 10 001 SEP 10
...... 2 01 001 SEP 102 02 001 OCT 09
...... 2 03 001 SEP 102 04 500 OCT 09 MOD 3973 or 4371 or 4457
...... 2 05 001 OCT 082 06 001 SEP 10
...... 2 09 500 SEP 10 MOD 3973 or 4371 or 44572 10 050 OCT 09 MOD 4111
...... 2 10A 500 SEP 10 MOD 3973 or 4371 or 4457
...... 2 11 030 SEP 10 PW124 MOD 43712 12 050 OCT 08 PW124 MOD 4111
...... 2 11 500 SEP 10 PW127F-127M2 12 500 OCT 08 PW127F-127M
...... 2 25 001 SEP 102 26 001 APR 08
...... 2 33 001 SEP 102 34 001 OCT 08
...... 3 01 001 SEP 10
5.02
72
CHECK LIST
R.T.R. Reason of Temporary Revisions SEP 10 001
ENV
TR EDITION DATE REASON AFFECTED PAGES
01 OCT 98 Single engine gross ceiling 4.61 - 4.62
02 FEB 99 DUAL DC GEN LOSS 1.06
03 MAR 99 SEVERE ICING : improvement of
detection and procedure 1.09 - 3.04
04 NOV 99 Spring tab MOD 4373 or 8167 ENG FLAME OUT AT TO
2.03 - 2.20 - 2.21
05 NOV 00 Introduction of FAA AD Missing page for 212A
Various
3.05 - 3.06 - 3.07 4.64 2.37
06 FEB 02 Introduction of modification 5313 EGPWS
1.07 - 1.08
07 FEB 03 Introduction of modifications 5377+5434
CDLS Models 102-202-212-212A 1 - 2 - 3 - 6
08 OCT 03 Introduction of modifications 5377+5434 CDLS Models 101-201-211
1 - 2 - 3 - 6
09 FEB 05
Correction of content 2.02 Introduction of BOTH ELEVATORS RECONNECTION ON GROUND
Correction of Cockpit Door Daily Check Single Eng Gross Ceiling Flaps 15 for
Icing Conditions
2.02 2.22A
3.02A 4.62
10 APR 06 FUEL LO LVL Procedure Updating
Introduction of Mod 5561 : Messier--Bugatti Wheels and Brakes
2.13 4.65
11 MAR 07 DITCHING and FORCED LANDING
Procedure Updating MISSING PAGE 2.14
1.08 – 1.08A 2.14
12 MAY 07 MPC : indicating/recording system, install MPC with QAR Thales
2.29A
13 JUN 08
Contents page correction (deletion of EEC SELECT IN FLIGHT and ATPCS
FAIL) ENG OIL LO PR : (Only for Aircraft with
Man Ignition), Procedure updating
2.01
2.12 (sequences 050, 150
and 500 only)
14 JUL 08 PW127M impact including BOOST
function Part 4
15 AUG 08 ENG BOOST FAULT procedure
introduction 2.01 – 2.12A
QRH QUICK REFERENCE HANDBOOK 5-03 page 1-089
ATR 72
S.N.T.P. Shipping Note Temporary Pages MAY 11
Please find below the list of the temporary pages created, suppressed or revised
Temporary revision N° 05 (MAY 11).
Action P CH SE Page Seq Date Label Modification expression
End NO
"F"=Facing "ADD"=Add "DESTROY" = Destroy "A" = After "……" = Revised "SEE VAL" = See Validation
ADD 1 ** ** 010 050 MAY 11 MOD (3973 or 4371 or 4457) ADD 1 ** ** 010 500 MAY 11 ADD 1 ** ** 011 050 MAY 11 MOD (3973 or 4371 or 4457) ADD 1 ** ** 011 500 MAY 11 ..... 5 01 ** 001 089 MAY 11 NO ..... 5 02 ** 001 001 MAY 11 ..... 5 04 ** 001 089 MAY 11 NO
QRH QUICK REFERENCE HANDBOOK 5-04 page 1-089
ATR 72
L.E.T.P. List of EffectiveTemporary Pages MAY 11
You must hold in your manual the following temporary pages Issue P CH SE Page Seq Date Label Modification expression Validity expression
End NO
TR05 1 ** ** 010 050 MAY 11 MOD (3973 or 4371 or 4457) NO0001-0003 TR05 1 ** ** 010 500 MAY 11 NO0051-0059 TR05 1 ** ** 011 050 MAY 11 MOD (3973 or 4371 or 4457) NO0001-0003 TR05 1 ** ** 011 500 MAY 11 NO0051-0059 TR05 5 01 ** 001 089 MAY 11 NO ALL TR16 5 02 ** 001 001 MAY 11 ALL TR05 5 04 ** 001 089 MAY 11 NO ALL
NO
RM
AL
CH
EC
KLI
ST
6.01
72
NORMAL PROCEDURES APR 08 100
* : if applicable
R
Mod : 3973 or 4371 or 4457
FINAL COCKPIT PREPARATION PARKING BRK ............... ON / PRESS CHECKALTIMETERS .............................................SETLANDING ELEVATION ..............................SETCOM / NAV / GPS ......................................SET FUEL QTY ............................................ CHECKENG F/U ................................................RESETMEMO PANEL...................................... CHECKPWR MGT ....................................................TO
DESCENT
CCAS..........................................................RCL LDG BUGS ...........................SET AND CHECK LDG ELEVATION ..................................CHECK ARRIVAL BREIFING ..................... COMPLETE
BEFORE PROPELLER ROTATION
TAIL PROP.................................... ON BOARDDOORS ..............................................CLOSEDT/O BUGS / APM* ............... SET AND CHECKTRIMS ........................................................SET CDLS*.......................................................... ONSEAT BELTS............................................... ONBEACON ..................................................... ON
BEFORE TAXI
PROP BRK *.............................................. OFFCOCKPIT COM HATCH.....................CLOSEDCL 1 + 2 ...................................................AUTOANTI-ICING .........................................AS RQD ANTI-SKID............................................... TESTFLAPS ........................................................SET
TAXI
TAXI & T.O LIGHTS .................................... ONBRAKES ............................................... CHECKAFCS ..........................................................SETRUDDER CAM ...................................CENTER TO CONFIG............................................. TESTTAKE OFF BRIEFING ...................COMPLETE
BEFORE TAKE OFF
BLEED VALVES..................................AS RQDAIR FLOW ..............................................NORMGUST LOCK..................................... RELEASEFLIGHT CONTROLS............................ CHECK CCAS................................................... TO INHIXPDR / TCAS*............................... ALT / AUTOEXT LIGHTS................................................ ONFD BAR (When lined up) ....................CENTER
AFTER TAKE OFF
LDG GEAR ...................................................UPFLAPS ........................................................... 0°PWR MGT / NP .......................... CLB / CHECKBLEED VALVES.......................................... ON TAXI & T.O LIGHTS .................................. OFFALTIMETERS ...................... SET AND CHECK
APPROACH
SEAT BELTS................................................ON ALTIMETERS ....................... SET AND CHECK CABIN ALTITUDE .................................CHECK
BEFORE LANDING
LDG GEAR .........................................3 GREEN FLAPS ...................................................CHECK PWR MGT .................................................... TO TLU....................................................... LO SPD ICING AOA LIGHT ................................CHECK EXT LIGHTS.................................................ON
AFTER LANDING
XPDR / TCAS* / RADAR..........................STBY FLIGHT CONTROLS...........................LOCKED FLAPS ............................................................0° TRIMS ........................................................ SET LAND LIGHTS / STROBES........................ OFF ANTI-/DE-ICING ......................................... OFF ENG START ROT SEL............................... OFF
After at least one minute CL 1............................ FTR THEN FUEL SO
PARKING
PARKING BRK ............................................ ON TAXI & T.O LIGHTS ...................................OFF CL 2 ...........................................................FTR PROP BRK *................................................ ON BEACON ....................................................OFF SEAT BELTS..............................................OFF TAIL PROP................................ ON POSITION
When leaving aircraft OXYGEN MAIN SUPPLY.....................OFF ICE AND RAIN PROTECTION ............OFF EXT LIGHTS ........................................OFF EMER EXIT LIGHT .......................DISARM EFIS / RADAR / COM / NAV................OFF CL 2............................................. FUEL SO FUEL PUMPS 1 + 2 .............................OFF CDLS* ..................................................OFF
BAT ......................................................OFF
IN CASE OF ICING CONDITIONS REFER TO 3.05 IN CASE OF SEVERE ICING REFER TO 1.09
ON GROUND EMER EVACUATION AIRCRAFT / PARKING BRAKE ............................................................ STOP / ENGAGE ATC (VHF 1)......................................................................................................... NOTIFY CL 1 + 2........................................................................................... FTR THEN FUEL SO MIN CAB LIGHT........................................................................................................... ON CABIN CREW (PA) .............................................................................................. NOTIFY FIRE HANDLES 1 + 2 ...............................................................................................PULL AGENTS...............................................................................................................AS RQD ENG START ROTARY SELECTOR .............................................. OFF / START ABORT FUEL PUMPS 1 + 2 ................................................................................................... OFF EVACUATION ..................................................................................................... INITIATE
Before leaving aircraft, BAT................................................................................. OFF