Download pdf - Checklist - Piper Arrow PA28 Full

PIPER ARROW PA28 CHECKLIST

1 Aircraft Documentsa) Certificate of Registrationb) Certificate of Airworthinessc) Certificate of Radio Installationd) Aircraft Radio Licencee) Certificate of Insurancef) Certificate of Maintenance

2 Aircraft Technical Log

3 CAAFU Aircraft Approval

4 Flying Training Manual

5 Aerad Plates / Charts

6 Pilot licence, medical & logbook

7 170A

8 Two pairs of headsets

9 Stopwatch

10 Fuel Strainer

DOCUMENTS / EQUIPMENT FOR CAAFU TESTS

19 March 2004 Page 1

PRE-FLIGHT CHECKSNote: Before entering aircraft, check surface clear of hoar frost, snow, iceand mud.COCKPIT PREPARATION1 Aircraft documents Check2 Parking brake ON3 Remove control lock Stow4 Fire extinguisher Check5 First Aid kit Check6 Magneto / Starter Switch / Radio OFF7 Pitot & Static System Drains Operate8 Fear Selector Down9 Emergency Gear over-ride ON

10 Battery Master Switch ON11 Vacuum alternator & oil lights Check ON12 Fuel Selector ON - check contents13 Anti-collision lights Check14 Landing light Check15 Pitot heater - stall warning Check16 Nav lights, panel & cabin lighting As required17 Battery master switch OFF

18 Flaps Check movement, leave down

STARBOARD WING1 Flap Check2 Aileron Check3 Wing tip, anti-collision & nav lights Check4 Wing surfaces Check5 Fuel tank contents, vents & drains Check6 Landing gear Check 2.5" extension7 Brake block & disc Check8 Fresh air inlet Clear


FRONT FUSELAGE1 Windscreen & O.A.T. probe Check2 Engine Check3 Oil contents Check4 Engine cowling Check5 Propeller & spinner Check6 Air intakes & alternator belt Check7 Landing light Check8 Exhaust pipe Check9 Landing gear Check 2.75" extension

10 Engine oil Check quantity11 Engine hydraulic quantity Check12 Engine cowls Check13 Fuel drain CheckPORT WING1 Landing gear Check 2.5" extension2 Brake block and disc Check3 Fuel tank contents, vents & drains Check4 Wing surfaces Check5 Stall warning trigger Check6 Pitot head Check7 Wingtip, anti-collision & nav lights Check8 Aileron Check9 Flap & static vent Check

REAR FUSELAGE AND TAIL1 Fuselage skin Check2 Fin surfaces Check3 Stabilator & anti-servo tabs Check4 Rudder & nav light Check5 Anti-collision light Check6 Stabilator & anti-servo tabs Check7 Radio aerials & static vent Check8 Fuselage skin & windows Check9 Baggage door Check

10 Cabin door Check11 Flaps UP


BEFORE STARTING CHECKS - PAX BRIEF1 Safety brief Completed1a Mobile phones OFF - not on standby2 External check Completed3 Entrance door Close4 Parking brake ON5 Seat & seat belts Check6 Ailerons, stabilator & trimmers Check7 Flap operation Check8 Battery master / Alternator switch ON

Avionics master switches ON9 Comm 2 ATIS - set QNH / QFE10 Comm 2 Tower - start clearance, ATIS - QNH11 Comm 2 Approach12 Comm 2 OFF13 Circuit breakers Check14 Fuel pump ON - check pressure15 Anti-collision light fin ONSTARTING ENGINE1 Throttle - half open, Mixture Prime then idle-cut-off2 Throttle Set ½” open 3 Propeller area Clear4 Magneto / Starter switch ON / Start5 Mixture Full rich6 Starter warning light Out7 Oil pressure Check8 Throttle 1400 rpm9 Fuel pressure Check10 Alternator Check11 Suction Check12 Fuel pump OFF - check pressure remains13 Magneto Dead cut check


AFTER STARTING ENGINE

1 Engine T’s & P’s Check2 Avionics master ON3 Comm 2, Nav 2 ON4 Audio panel Select Comm 15 Flight instruments Serviceable6 Gyro compass instruments On/Checked/Synchronised

7 ILSSelectDisplay Ident

Freq Nav 1 & Nav 2No flags, functional displayNav 1, Nav 2

DME

SelectDisplay Ident

Nav 1 or Nav 2Range checksNav 1 or Nav 2

VORSelectDisplay Ident

Freq Nav 1 and Nav 2If no flags, function checkNav 1, Nav 2

ADF

SelectDisplay Ident

Freq ADFCheck sensible headingFunctional checkADF

TRANSPONDER Select Standby

MARKERS Select Audio, test lights

7 G.P.S. Select Program8 Altimeters Check QNH / QFE

9 Comm 19 Comm 1 Taxi clearance


TAXYING - TAXY CHECKS1 Brakes Check P1 & P22 Rudder pedals Check full movement3 Flight instruments Check for correct indication4 Compass & radio compass Check for correct indication

POWER CHECKS1 Parking brake ON2 Temperatures & pressures Within limits3 Fuel Change tanks4 Fuel pump ON5 Throttle 2000 RPM6 Aircraft not moving Check7 Alternate air Check8 Propeller Exercise (twice) 200 RPM

drop minimum9 Magnetos Max drop 175, difference 50

10 Vacuum 4.8 - 5.1 inches HG11 Oil temperature Check12 Oil pressure Check13 Throttle Slow running 500 - 700 RPM

19 March 2004 Page 5A

PRE-TAKE OFF1 Trimmers Set2 Propeller Full forwards3 Mixture Full rich4 Throttle friction As required5 Alternative air Closed6 Fuel cock L / R tank contents sufficient7 Fuel pump ON8 Flaps As required (check visually)9 Instruments Check QNH - Compass Synch

10 Engine T’s & P’s Checked11 Suction 4.8 - 5.1 inches HG12 Cabin heater defroster As required13 Anti-collision lights ON14 Harnesses & seatbacks Tight & erect15 Door Closed & locked16 Controls Full & free movement17 Request clearance Copy & read back18 Radio & Nav aids Set19 Transponder Set20 Departure clearance Call ready for departure

AFTER LINE UP CLEARANCE1 Landing lights ON2 Pitot heat ON3 Transponder Set on ALT4 Compass Check against runway5 In line aids Check6 Ice & cross wind Check

AFTER TAKE OFF CHECKS1 Brakes Gear Up On/Off2 Gear Up3 Flaps Up4 Landing lights OFF5 T’s & P’s Check6 Radio Nav aids Set & Idented7 Fuel pump Off @ 1000'


CRUISE CHECK

F Fuel Sufficient contents / MixtureR Radios / Navaids Select - Ident - DisplayI Icing CheckE Engine Temperature / PressureD D.I. Compass In synchA Altimeters m 1 1013.2

m 2 QNH or RPS as requiredA Alternative air OFF

CLIMB & DESCENT CHECKS (Every 1000')

A Altimeters Check 1013 set & QNH (m 2) T Throttle 27" (Climb)T T’s & P’s CheckI Icing Check temperatureS Speed Climb speed

PRE-DESCENT CHECKS

W Weather & approach brief CompleteA Altimeters Check destination QNHI Icing Check temperature

M M.S.A. Check M.S.A.

ALTIMETER SETTING PROCEDURES

Pre-flight & taxy QNH on bothBefore take off QNH/QNH

Climb At transition of when cleared 1013on No.1 QNH on No.2

En-route 1013 on No.1 RQNH on No.2Initial approach QNH on bothFinal approach / Go-around QNH / QNH


AIRFIELD APPROACH CHECK

S Speed 115 ktI Idents CheckedC Compass / DI CheckedA Alternative Air OffI Icing Check

PRE-LANDING CHECKS

1 B Brakes OFF2 U Undercarriage Delay to final approach3 M Mixture controls Fully rich4 P Propellor Max RPM5 F Fuel pump Contents, fuel pump ON6 F Flaps Set 108 kt max7 I Instruments T’s & P’s, Altimeter set8 Alternate air OFF9 Door Closed & locked

10 Harnesses / seat backs Tight & erect11 Landing light ON

1000' CHECK

1 Greens Checked2 Blue Max3 Red Max4 Flags Away5 TOES OFF BRAKES


GO AROUND CHECKS

1 Throttle Fully forward2 Gear Positive rate of climb - UP3 Climb Power Set4 Flaps Positive rate of climb - UP5 Fuel pump OFF above 1000'

AFTER LANDING

1 Flaps UP2 Fuel pump OFF3 Pitot heat OFF4 Cabin heater As required5 Radio - Comm 2 Tower6 Avionics master OFF7 Trimmers Neutral8 Electrics non-essential - OFF

SHUT DOWN CHECKS

1 Parking brake ON2 Throttle Set for 1200 RPM3 Ignition switches Check for dead cut4 Radio Comm 2 & Nav 2 - OFF5 Electrical switches OFF6 Mixture controls Idle cut off7 Ignition switches OFF8 Master switch OFF9 Control lock Fitted


H.A.S.E.L.L. Checks

H Height Sufficient to recover by 3000' AGLA Airframe Flaps, as required, brakes - OFFS Security Straps tight, hatches secure, no

loose articlesE Engine Fuel pump - ON

Fuel contents - sufficientMixture - richTemperatures & pressures

L Location Clear of: Airways & AirfieldsBuilt up areasCloud & CASDanger areas

L Lookout Clearing turns to look out for otheraircraft


ENGINE FAILURE AT HEIGHT

1 Fuel selector Check / change tanks2 Fuel pump ON3 Alternative air Open4 Mixture Rich5 Magnetos Both - ON6 Temperatures / pressures Check

ALTERNATOR FAILURE

1 Electrical load Reduce2 Field / Output circuit breaker Check / restart3 Ammeter / warning light Check

IF OUTPUT RESTORED - CONTINUE WITH ITEM 6

IF NO OUTPUT

4 Alternator switch OFF for 2 secs then ON5 Ammeter / warning light Check

IF OUTPUT RESTORED

6 Electrical load As required

IF NO OUTPUT

7 Elecrical load Minimum safe


ENGINE FIRE DRILL (AIR)TRIM FOR 79 KNOTS

1 Fuel selector OFF2 Fuel pump OFF3 Throttle Closed4 Mixture Idle cut off5 Magnetos OFF6 Heater & de-mister OFF

DISTRESS CALL (IF TIME PERMITS) THEN FORCED LAND

DO NOT ATTEMPT RESTART

7 Battery master / alternator OFF8 Door top latch Unlatched9 Seat belt / shoulder straps Secure

10 Seat backs Erect11 Gear Down12 Flaps As required13 Brace For landing14 Landing established Slow to 72 kt

CABIN FIRE DRILL (AIR)

1 Source of fire Check2 All electrics Check / OFF3 Cabin heat OFF4 Heater vents Open5 Fire extinguisher Operate

LAND AS SOON AS POSSIBLE


ENGINE FIRE DRILL (GROUND)1 Mixture Idle cut off

2 ThrottleOpen / continue crankingengine to blow throughthen;

3 Throttle Closed4 Mixture Idle cut off5 Fuel selector OFF6 Fuel pump OFF7 Magnetos OFF8 Brakes OFF9 Battery master OFF

EVACUATE AIRCRAFT AS SOON AS

PROPELLER OVER SPEED1 Throttle Reduce2 Oil pressure Check

3 Propellor controlFull DECREASE RPMThen set if any controlavailable

4 Air speed Reduce

5 Throttle As required to stay below2700 RPM

EMERGENCY LANDING GEAR1 Circuit breakers Check IN

2 Panel lights Check OFFCheck / change bulbs

3 Airspeed Reduce to 87 kt4 Landing gear Select down

5 Backup gear extender Raise to OVERRIDEENGAGED

If gear does not lock down move GEAR EXTENDER LEVER downand hold it in the emergency DOWN position


GEAR UP EMERGENCY LANDING

1 Flaps As required2 Throttle Close3 Mixture Idle cut off4 Ignition switch Off5 Master switch OFF6 Fuel selector OFF7 Seat belt and harness Tight8 Brace position Adopt and brace

ENGINE POWER LOSS DURINGTAKE OFFNote: If sufficient runway, land ahead selecting full flapIf it is necessary to clear obstructions:Gear selector UP

Emergency gear lever Locked in OVERRIDEENGAGED position

Note: If sufficient altitude has been gained to attempt a re-start,maintain safe airspeed.

1 Fuel selector Switch tanks2 Electric fuel pump Check ON3 Mixture Check full rich4 Alternate air OPEN5 Emergency gear lever As required

Note: If power is not regained proceed with power off landing.

NOTE: Lock Emergency Gear Lever in OVERRIDE ENGAGEDPOSITION before airspeed drops to 105 IAS to prevent the landinggear from free-falling.


RECOMMENDED SPEEDS AND POWER SETTINGSRPM IAS (kt) FLA

Rotate normal Max 65-75* 0o

Rotate / Short field obstacle Max 51-60* 0o /Rotate / Short field no obstacle Max 50 0o /Climb normal V.Y. Max 87 0o

Climb best angle V.X. Max 77 0o

Climb en-route 2500 /27" 105 0o

Climb with flap 2500 /27" 65 A/RCruise 2300 /24" 120 0o

Descent normal 2300 /15" 130 0o

Descent cruise 1700 95 0o

Glide Descent /Engine failure 1200 79 0o

Circuit A/R 100 0o

Bad weather circuit A/R 85 25o

FLAP VA VAT FLAPPowered approach 75 kt 1.3VSO 70 40o

Glide approach 79 kt 70 kt 40o

Flapless approach 85 kt 77 kt 0o

Max crosswind component 17 ktVNE (never exceed) 190 ktVNO (normal operating) 149 ktVRA ( 121 ktVFE (flap extended) 108 ktFlight over water 110 ktMaximum all up-weight 2750Utility category 2020Maximum gear extension SPD 130 ktMaximum gear retraction SPD 109 ktVLE (landing gear extended) 130 ktFuel consumption at cruise 10.4 U.S. Gals/HrPower off full flap stall 53 kt IASClean 58 kt IAS* Depends on weight


FUEL REQUIREMENTS G-BPZM & G-TOLL

TOTAL USEABLE FUEL

72 US gallons 60 IMP gallons 432 pounds 272 litres

Start-Taxi-Take off 1 gallon

Climb 14.4 U.S. gph

Cruise 10.4 U.S. gph

Descent 1.5 U.S. gallon

Hold NDB, ILS 11 U.S. gph

TOTAL BURN

Hold - 45 minutes 9.5 U.S. gph

Diversion 12 U.S. gps

gps = gallons per hour


W

I

N

D

S

P

E

E

D

K

N

0

T

S

ANGLE BETWEEN WIND DIRECTION AND RUNWAYHEADING

FOR CROSSWIND COMPONENT

10o 20o 30o 40o 50o 60o 70o

5 1 2 2 3 4 4 4

10 2 3 5 6 7 8 9

15 3 5 7 9 11 13 14

20 3 7 10 13 15 17 18

25 4 8 12 16 19 22 23

30 5 10 15 19 23 26 28

35 6 12 17 22 26 30 32

40 7 14 20 25 30 35 37

45 8 15 22 29 34 39 42

50 9 17 25 32 38 43 47

55 10 19 27 35 42 48 52

60 10 20 30 38 46 52 55

65 11 22 32 42 50 56 61

70 12 24 35 45 54 60 65

75 13 26 37 48 57 64 70

80 14 27 40 51 60 69 75

85 15 29 43 55 64 73 80

90 16 31 45 58 68 77 84

95 16 33 48 61 72 82 89

100 17 34 50 64 75 86 93

10o 20o 30o 40o 50o 60o 70o

FOR HEADWIND COMPONENT - ANGLE BETWEEN WIND DIRECTION AND RUNWAY HEADING

DRIFT ANGLESWind Speed 5kt 10kt 15kt 20kt 25kt 30kt

KCAS 100 115 135 100 115 135 100 115 135 100 115 135 100 115 135 100 115 135

WIND ANGLE OFF NOSE5o 0 0 0 1 0 0 1 1 0 1 1 1 1 1 1 1 1 1

10o 0 0 0 1 1 1 1 1 1 2 2 1 2 2 2 2 2 2

15o 1 1 1 1 1 1 2 2 1 3 2 2 3 2 2 4 3 3

20o 1 1 1 2 2 1 3 2 2 4 3 3 4 3 3 5 4 4

25o 1 1 1 2 2 2 3 3 2 4 4 3 5 4 4 6 5 4

30o 1 1 1 3 2 2 4 3 3 5 4 4 6 4 4 7 6 5

35o 2 1 1 3 3 2 5 4 3 6 5 4 7 5 5 8 7 6

40o 2 2 1 4 3 2 5 4 4 7 6 5 8 6 6 9 8 7

45o 2 2 1 4 3 3 5 5 4 7 6 5 8 6 6 10 9 8

50o 2 2 1 4 4 3 6 5 4 8 7 6 9 7 7 11 10 8

55o 2 2 2 4 4 3 7 6 5 8 7 6 10 8 8 12 10 9

60o 3 2 2 5 4 3 7 7 5 9 8 6 11 8 8 13 11 9

65o 3 2 2 5 4 4 7 7 5 9 8 7 11 8 8 14 12 10

70o 3 2 2 5 4 4 8 7 5 10 9 7 12 9 9 14 13 11

75o 3 2 2 5 4 4 8 7 6 10 9 7 13 9 9 15 13 11

80o 3 2 2 5 5 4 8 7 6 11 9 8 13 10 10 16 14 11

85o 3 3 2 5 5 4 8 7 6 11 10 8 13 10 10 16 14 11

90o 3 3 2 6 5 4 8 7 6 11 10 8 14 10 10 17 15 12

© David Bruford V.2 - 2 April 2006