HAWKER 4000 FAA APPROVED AIRPLANE FLIGHT · PDF fileFAA Approved Airplane Flight Manual AS-1 P/N 401-590001-0078 TABLE OF CONTENTS ... • An SPDA 1 communication problem is indicated

Section 3B - Advisory/Status Procedures

FAA Approved Airplane Flight Manual

AS-1 P/N 401-590001-0078

TABLE OF CONTENTSSUBJECT PAGE

SECTION 3BADVISORY/STATUS PROCEDURES

ADVISORY / STATUS PROCEDURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS-3CREW ALERTING SYSTEM (CAS) MSGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS-3COMPUTER RESET. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS-3

ADVISORY / STATUS PROCEDURES ALPHABETICAL CAS INDEX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS-4

Original Issue: Aug 8, 2011


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AS-2

P/N 401-590001-0078Section 3B - Advisory/Status ProceduresOriginal Issue: Aug 8, 2011



AS-3 P/N 401-590001-0078

ADVISORY / STATUS PROCEDURESThe procedures contained in this section have been developed and recommended by the manufacturer for use in the operationof this airplane. These procedures are for guidance only in identifying the meaning and operating impact of ADVISORY orSTATUS Crew Alerting System (CAS) Messages (MSGs).

NOTEIn these procedures, it is assumed that the positions of the Pilot and Copilot are as follows:

Pilot - occupying the left crew seat.Copilot - occupying the right crew seat.

CREW ALERTING SYSTEM (CAS) MSGSThroughout the procedural sections of the Airplane Flight Manual, CAS MSGs are organized by color as shown below:

COMPUTER RESETCAS MSGs may be reset on the ground by the following procedure:

1. Allow adequate time for the system to complete its power up BIT (Built In Test).2. If CAS MSG(s) remains posted, shutdown the airplane and remove all electrical power.3. Repower the airplane. Refer to SECTION 4 - NORMAL PROCEDURES.4. If CAS MSG(s) recur, refer to the appropriate Crew Action and/or Dispatch column in this Section to determine dispatch

capability.

EMERGENCY

ABNORMAL

ADVISORY

STATUS



Section 3B - Advisory/Status ProceduresAS-4 P/N 401-590001-0078

ADVISORY / STATUS PROCEDURES ALPHABETICAL CAS INDEX

NOTE• Advisory / Status CAS MSGs that post new, are highlighted (inverse video) for 5 seconds.

• CAS MSGs with designations for Left, Right, Left and Right, are abbreviated to L, R, L-R, respectively.The abbreviations are not used in the alphabetical ordering of this index.

• Dispatch column addresses No Go (dispatch not permitted) or MEL (dispatch permitted, after applyingMEL procedures) or N/A (Not Applicable for dispatch).

CAS MSG Description Crew Action Dispatch

AC External Power On Ground Only CAS MSG.AC EXT power connected and ON.

Crew Awareness N/A

Aileron Trim Fail Active when ECMM2 detects failure within the aileron trim system or the trim actuator does not respond to commands or after selecting AILERON TRIM POWER to OFF.

NOTE:Accompanied by amber “X” on trim indicator.

In Flight:Evaluate aileron trim response. If it works, use as normal.

On Ground: MEL

Antiskid Off ANTISKID switch is selected OFF. Crew Awareness

On Ground: No Go

AP 1 FailAP 2 Fail

AP channel has failed.

NOTE:AP, YD, Mach Trim, Flap Trim, FD and SWPS functions automatically switch to the other AFCS.

Crew Awareness

On Ground: MEL

AP 1-2 Fail Both AP channels have failed.

NOTE:• Red AP is displayed on top of PFD if AP in use.• Continuous Cavalry Charge until silenced via

AP TRIM PUSHER.

Crew AwarenessLoss of CAT 2 capability.Apply appropriate RVSM contingency procedures.

On Ground: MEL

APU Bleed Det Fail One or more temp sensors failed in the APU Bleed system.

In Flight:Unless required for safety, do not run APU if APU fire detection is failed.

On Ground: MEL

APU Door Disagree APU inlet door not in commanded position.

NOTE:• If CLOSED, APU will not start / run.• If OPEN (ground pos), drag increases.• May cause additional buffet and require lateral

and directional trim.

Crew Awareness

On Ground: MEL

APU Fail APU protective shutdown from Fire Detected, Fire Det Fail, Exhaust Gas Temperature (EGT), OIL Temp, OIL Press, RPM Speed, or Integrated Pneumatic Controller.

Crew Awareness

On Ground: MEL




AS-5 P/N 401-590001-0078

APU Fire Det Fail APU Fire Detector Fail. In Flight:Unless required for safety, do not run APU if APU fire detection is failed.

On Ground: MEL

APU Fuel Valve Fail The APU firewall fuel valve is not in its commanded position.

In Flight:Crew Awareness

NOTE• The APU may not be available

depending on whether the valve hasfailed in the open or closed position.

• Do not start APU unless action ispart of an Emergency or AbnormalProcedure.

On Ground: MEL

APU Generator Fail APU Generator commanded on and contactor stayed open.

In Flight:1. APU GEN switch OFF then AUTO.2. If CAS MSG re-post, Crew

Awareness.

On Ground: MEL

APU Running APU is running normally. Crew Awareness N/A

APU Unattended Mode Ground Only CAS MSG.APU may be operated without qualified personnel in the cockpit.

NOTE:• APU Unattended Mode will not activate if any

monitored CAS MSG is posted, when FUEL/IGN switch is not OFF, or low fuel quantity.

• APU Unattended Mode will auto shutdown theAPU if any monitored CAS MSG posts.

• APU Unattended Mode will auto shutdownAPU and discharge Fire Bottle 3 if the

CAS MSG posts.

Crew Awareness N/A

Auto Pressurize Fault Outflow valve operation reduced to single-channel.

In Flight:Crew Awareness

On Ground:MANUAL CONTROL, cycle MAN, then OFF.

MEL

Autothrottle Disc A/T has been disconnected using the A/T DISC switch or the A/T ENG / DISENG switch.

Crew Awareness N/A

Aux Elect Ctrl Fault Lost communication between MAU 2 and A / EPCU.

Crew Awareness

On Ground: No Go

Aux Hyd Pump Not Auto Three position switch is not in AUTO position. Crew Awareness

On Ground: No Go


APU Fire




Avionics Bus Fault Loss of one or both ASCB Backup Bus(es). Crew Awareness

On Ground: No Go

Avionics Config Fault Ground Only CAS MSG.1 or 2 Airplane Personality Modules failed.

NOTE:Loss of redundancy.

Crew Awareness No Go

Avionics Fan Fail Avionics Rack Fan 1 or Avionics Rack Fan 2 has failed.

Crew Awareness

On Ground: MEL

Baggage Smoke Fail Baggage Smoke Detector Fail. In Flight:If cargo is contained in baggage compartment:

1. Descend to 35,000 FT or Minimum Safe Altitude, if higher, (fuel permitting) to conduct periodic inspection of the compartment.

On Ground: MEL

Batt 1 OffBatt 2 OffBatt 1-2 Off

Indicated Battery contactor is open.

NOTE:APU will not start.

Crew Awareness

On Ground: No Go

L Bleed FaultR Bleed Fault

Indicated Bleed system is commanded ON, the Bleed valve is closed or has a control problem.

In Flight:BLEED (affected side), cycle OFF, then AUTO.

On Ground:BLEED (affected side), cycle OFF, then AUTO.

MEL

L-R Bleed Fault Both Bleed systems are commanded ON, both Bleed valves are closed or have a control problem.

In Flight: BLEEDS, cycle OFF, then AUTO.

On Ground:BLEEDS, cycle OFF, then AUTO.

If CAS MSG does not clear:

1. No Dispatch.

No Go

Bleed Isol Not Closed Bleed Isolate valve has failed open. In Flight:Use of Wing Anti-ice is permitted if required by procedure.

On Ground: MEL

Bleed Isol Not Open Bleed isolate valve has failed closed.

NOTE:• Loss of cross-side engine starts.• Unable to supply both packs from single bleed

source.

Crew Awareness

On Ground: MEL





AS-7 P/N 401-590001-0078

L Bleed Leak Det FailR Bleed Leak Det Fail

One or more temp sensors have failed on the Left or Right.

Crew Awareness

On Ground: No Go

L-R Bleed Leak Det Fail One or more temp sensors have failed on both sides.

Crew Awareness

On Ground: No Go

L Bleed OffR Bleed Off

Indicated Bleed has been selected OFF or auto-shutdown.

In Flight:

NOTE:• In a bleed overpressure condition,

the affected bleed valve latchesclosed and the bleed isolation valveremains closed.

• In a bleed overtemperaturecondition, the affected bleed valvelatches closed and the bleedisolation valve automatically opens.

1. Bleed Synoptic, check bleed isolation valve.

If bleed isolation valve is closed:

a. Exit and Avoid Icing.

On Ground: MEL

NOTE:• An SPDA 1 communication problem is

indicated when the CAS MSG isaccompanied with the CAS MSG.

• An SPDA 2 communication problem isindicated when the CAS MSG isaccompanied with the CAS MSG, and the APU will shutdown ifrunning.

In Flight:If CAS MSG is accompanied with

CAS MSG:

1. L BLEED, cycle OFF, then AUTO.

2. L BOOST PUMP, cycle OFF, then AUTO.

If CAS MSG is accompanied with

CAS MSG:

1. R BLEED, cycle OFF, then AUTO.

2. R BOOST PUMP, cycle OFF, then AUTO.

On Ground: No Go

L-R Bleed Off Both Bleeds have been selected OFF or APU Bleed is selected ON during ground operation.

Crew Awareness

On Ground:Verify L and R BLEED, AUTO and APU BLEED, OFF before takeoff.

If CAS MSG does not clear:

1. No Dispatch.

No Go

Boost Pump Not Auto Left or Right, or Left and Right BOOST PUMP switch(es) has been selected to OFF.

Crew Awareness

On Ground: No Go


L Bleed OffL Boost Pump On

R Bleed OffR Boost Pump On

L Bleed Off

L Boost Pump On

R Bleed Off

R Boost Pump On




L Boost Pump OnR Boost Pump On

Left or Right Boost Pump is ON due to low fuel pressure or manual selection, or is an indication of an SPDA communication problem.

Manual selection includes:• Selecting BOOST PUMP to ON.• Pressing the LEFT or RIGHT FUEL/IGN switch

to ON prior to engine start.• Pressing the APU START/STOP switch to ON

with AC power available.• Selecting Crossfeed.

NOTE:Loss of motive flow may cause decrease in fuel temperature.

In Flight:If CAS MSG posts without pilot action and fuel temperature on Fuel Synoptic page shows amber dashes:

1. Decrease altitude and/or increase airspeed as required to increase TAT above -40° C to prevent fuel freezing.

On Ground:Dispatch is permitted if manual selection is corrected before departure. Otherwise:

No Go

L-R Boost Pump On Left and Right Boost Pumps have turned ON due to low fuel pressure or manual selection.

Crew Awareness

On Ground: No Go

Bus Tie Not Auto Bus Tie switch is open.

NOTE:AC, DC, and ESS Bus Ties will not close.

In Flight:Verify Bus Tie switch is in AUTO.

On Ground: No Go

Cabin Auto Temp Fault Temp control system fault. In Flight:

1. L BLEED, cycle OFF, then AUTO.

2. Monitor cabin temps.

3. Use CABIN MANUAL COOL if necessary.

NOTE:Selecting CABIN MANUAL COOL provides full cool only and does not allow temperature control.

On Ground: MEL

CAS System Fault CAS Processor Module Failure. Loss of Master Caution / Warning flasher on one side.

Crew Awareness

On Ground: No Go

Ckpt Auto Temp Fault Temp control system fault. In Flight:

1. R BLEED, cycle OFF, then AUTO.

2. Monitor cockpit temps.

3. Use FLIGHT DECK MANUAL COOL if necessary.

NOTE:Selecting FLIGHT DECK MANUAL COOL provides full cool only and does not allow temperature control.

On Ground: MEL





AS-9 P/N 401-590001-0078

Config Mgmt 1 FailConfig Mgmt 2 Fail

Ground Only CAS MSG.Indicated Configuration Management System failed.



Crossfeed Valve Fail Crossfeed valve is not in commanded position. In Flight:If failed in open position when commanded to close:

1. Left and Right BOOST PUMP ON.

2. Balance fuel using differential thrust as required.

If failed in closed position when commanded to open:

NOTE:It may be required to cycle the TRANSFER switch several times.

1. Balance fuel with differential thrust or TRANSFER, if operative.

On Ground: No Go

CVR Fail Cockpit Voice Recorder (CVR) has failed. Crew Awareness MEL

DC External Power On Ground Only CAS MSG.DC EXT Power connected and ON.

Crew Awareness N/A

DC Fuel Pump Fail The DC pump is not operating in commanded state.

In Flight:Select DC FUEL PUMP switch to OFF.

On Ground: No Go

DLK MSG The CMF system has received an ATS Uplink message.

Crew Awareness N/A

L ECS Bleed Det FailR ECS Bleed Det Fail

One or more temp sensors have failed in the Left or the Right Environmental Control System (ECS).

Crew Awareness

On Ground: MEL

L-R ECS Bleed Det Fail One or more temp sensors have failed in both Environmental Control Systems (ECS).

Crew Awareness

On Ground: No Go

Elect Ctrl Fault Lost communication between GCU 1 or GCU 2 and A / EPCU / MAU 1 or MAU 2.

NOTE:• Loss of control of half Taxi and Landing lights.• APU will not start, but continue to run if on at

time of CAS MSG posting.• Loss of some cabin equipment.

Crew Awareness

On Ground: No Go

Emer Gen Not Auto EMER GEN switch is not in AUTO position. Crew Awareness

On Ground: No Go





Emer Generator Fault Emer Gen BIT Test failed or not performed, Emer Gen Hydraulic relays failed, or PDA 4 relay is not closed.

NOTE:EMER GEN may not be available or AUTO function may be inoperative.

Crew Awareness

On Ground: MEL

Emer Generator On Emer Gen AC and DC contactors are closed. Crew Awareness

On Ground: No Go

Emer Rud Sys Not Auto Three position switch is not in AUTO position. Crew Awareness

On Ground: No Go

Emer Rudder Fluid Low ERS reservoir has a low level. Crew Awareness

On Ground: No Go

L Eng A-Ice Fail OnR Eng A-Ice Fail OnL-R Eng A-Ice Fail On

Indicated Engine Anti-ice Valve(s) is failed open. Crew Awareness

On Ground:If OAT is above 10° C (50° F):

1. Do not use higher thrust than required to taxi, or to perform the pre-flight test.

2. No Dispatch.

If OAT is 10° C (50° F) or below:

1. Dispatch via MEL.

No Go

MEL

L Eng Chip DetectR Eng Chip DetectL-R Eng Chip Detect

Indicated chip detector has failed or engine oil has metallic debris. Could indicate possible engine damage.

Crew Awareness

On Ground: MEL

L Eng Fire Det FailR Eng Fire Det FailL-R Eng Fire Det Fail

Left or Right or both Eng Fire Detector(s) has failed.

Crew Awareness

On Ground: No Go

L Eng ShutdownR Eng ShutdownL-R Eng Shutdown

Indicated engine has been shut down with Left or Right FUEL / IGN switch.

Crew Awareness N/A

L Engine Vib FailR Engine Vib FailL-R Engine Vib Fail

Ground Only CAS MSG.Loss of monitoring system. The engine vibration signal conditioner or the vibration sensor on the Left or Right or both engines have failed.

NOTE:If an engine vibration exceedance is detected on the non-failed side, both vibration indications will post with the failed side displayed as amber dashes.

Crew Awareness MEL

L FADEC FaultR FADEC FaultL-R FADEC Fault

Left or Right or both engines have lost an essential redundant parameter.

Crew Awareness

On Ground: No Go

L FADEC Long TLDR FADEC Long TLDL-R FADEC Long TLD

Ground Only CAS MSG.Left or Right or both engines have lost a non-essential parameter. On Ground: No Go



Section 2 - Limitations


3 of 4

401-590001-0078TC1

Temporary Changeto the


P/N 401-590001-0078TC1(Continued)

SECTION 3B - ADVISORY / STATUS PROCEDURES


Read the following Cyan “L, R, and L-R FADEC Long TLD” CAS MSG in place of the current Cyan “L, R, and L-RFADEC Long TLD” CAS MSG:

Publication Affected FAA Approved Airplane Flight Manual, P/N 401-590001-0078, dated Aug 8, 2011, or later revision for Hawker Model 4000 Airplanes.

Airplane Serial Numbers Affected

RC-59 and After or Prior Airplane Serials with Kit 401-3007 or 401-3008 or 401-3027 or 401-3028 Installed for Block Point Upgrade A.

Description of Change 1. Added new header ENGINE TIME LIMITED DISPATCH with data.

2. Revised Cyan “L, R, L-R FADEC Long TLD” CAS MSGs with new Dispatch procedure.

3. Revised Cyan “L, R, L-R FADEC Short TLD” CAS MSGs with new Dispatch procedure.

Filing Instructions Insert Page 2 of 4 to face page LM-13 in Section 2 - Limitations,Insert Page 3 of 4 to face page AS-10 in Section 3B - Advisory/Status Procedures,Insert Page 4 of 4 to face page AS-11 in Section 3B - Advisory/Status Procedures.


L FADEC Long TLDR FADEC Long TLDL-R FADEC Long TLD

Ground Only CAS MSG.Left or Right or both engines have lost a non-essential parameter. On Ground: MEL

Apr 12, 2012


ts93910

Rectangle


Section 2 - Limitations

4 of 4

401-590001-0078TC1

401-590001-0078TC1(Continued)

Read the following Cyan “L, R, and L-R FADEC Short TLD” CAS MSG in place of the current Cyan “L, R, and L-RFADEC Short TLD” CAS MSG:


L FADEC Short TLDR FADEC Short TLDL-R FADEC Short TLD

Ground Only CAS MSG.Left or Right or both engines have lost a non-essential parameter. On Ground: MEL

Apr 12, 2012


ts93910

Rectangle



AS-11 P/N 401-590001-0078

L FADEC Short TLDR FADEC Short TLDL-R FADEC Short TLD

Ground Only CAS MSG.Left or Right or both engines have lost a non-essential parameter. On Ground: No Go

FDR Fail Flight Data Recorder (FDR) has failed. Crew Awareness MEL

Fire Bottle 1 DischFire Bottle 2 DischFire Bottle 1-2 Disch

Indicated Fire Bottle(s) has low pressure or has been discharged.

Crew Awareness

On Ground: No Go

Fire Bottle 1-2-3 Dis Indicated Fire Bottles have low pressure or have been discharged, or Pilot has initiated the Fire and Overheat Protection System (FOPS) test.

In Flight:Unless required for safety, do not run the APU.

On Ground:Do not run the APU.

No Go

Fire Bottle 1-3 Disch Indicated Fire Bottles have low pressure or have been discharged.

In Flight:Use #2 for APU or engines if needed.

On Ground:Use #2 for APU or engines if needed.

No Go

Fire Bottle 2-3 Disch Indicated Fire Bottles have low pressure or have been discharged.



No Go

Fire Bottle 3 Disch Fire Bottle has low pressure or has been discharged.

In Flight:Use #2 for APU discharge if needed.

On Ground:Use #2 for APU discharge if needed.

MEL

Fire Bottle 1 FailFire Bottle 2 FailFire Bottle 1-2 Fail

Squib(s) is open with bottle pressure retained, or the connector(s) for the pressure switch(es) is not mated.

NOTE:Bottle(s) will not discharge.

Crew Awareness

On Ground: No Go

Fire Bottle 1-2-3 Fail Squibs are open with bottle pressure retained, or the connectors for the pressure switches are not mated.

NOTE:Bottles will not discharge.



No Go

Fire Bottle 1-3 Fail Squibs are open with bottle pressure retained, or the connectors for the pressure switches are not mated.


In Flight:Use #2 for APU or engines if needed.

On Ground:Use #2 for APU or engines if needed.

No Go

Fire Bottle 2-3 Fail Squibs are open with bottle pressure retained, or the connectors for the pressure switches are not mated.




No Go





Fire Bottle 3 Fail Squib is open with bottle pressure retained, or the connector for the pressure switch is not mated.

NOTE:Bottle will not discharge.

In Flight:Use #2 for APU discharge if needed.

On Ground:Use #2 for APU discharge if needed.

MEL

Flap Fault Minor fault in flap system.

NOTE:No loss in functionality.

Crew Awareness

On Ground: MEL

Flap Trim 1 FailFlap Trim 2 Fail

Indicated Flap Trim channel has failed.

NOTE:• Loss of redundancy.• Flap Trim function automatically switches to the

other AFCS.

Crew Awareness

On Ground: MEL

Flap Trim 1-2 Fail Both Flap Trim channels have failed.

NOTE:Flap Trim compensation inoperative.

Crew Awareness

On Ground: MEL

FMS Position Miscomp Airplane position as reported by FMS 1 does not agree with the position reported by FMS 2, while neither of the FMSs is the active NAV source.

Crew Awareness

On Ground: MEL

Fuel Crossfeed CROSSFEED switch has been selected ON. Crew Awareness

On Ground: No Go





AS-13 P/N 401-590001-0078

Fuel Qty Degrade Loss of input to the Left or Right Fuel Quantity Card or fault detected in a sensor or probe or an electrically conductive foreign object in a wing tank.

NOTE:• Total quantity and degraded tank(s) display

loses last two digits.• Fuel contents on degraded tank may be up to

700 LB (318 KG) higher or lower thanindicated.

• Amber “Fuel Imbalance” CAS MSG is disabled.• Amber “# Fuel Qty Low” CAS MSG and “Low

Fuel” indicator on the PFD are independentand accurate if motive flow is operative.

• This CAS MSG may post or may be cleared onground by repeatedly setting and resetting theparking brake. When the parking brake is set,the densitometers are active and provide inputsinto the fuel processing system.

In Flight:If CAS MSG posts with no other CAS MSG(s):1. Do not operate within 50 NM of

thunderstorms.

NOTE:• Imbalance is verified by yoke

deflection into the wing with lessfuel.

• Do not rebalance based on FuelQuantity Display alone.

• Crossfeed can be done into thedirection of the yoke deflection.

2. Review yoke angle to assess fuelbalance.

3. Subtract 700 LB (318 KG) of fuelquantity reading per degraded tankfor endurance and add 700 LB(318 KG) per degraded tank forperformance weight calculations.

On Ground: If CAS MSG posts with no other CAS MSG(s):

1. Do not operate within 50 NM of thunderstorms.

MEL

Fuel Transfer Fuel pressure sensors detect fuel flow through transfer pump.

Crew Awareness

On Ground: No Go

L Fuel Valve ClosedR Fuel Valve ClosedL-R Fuel Valve Closed

Indicated Firewall Fuel Valve(s) is closed.

NOTE:Engine(s) will shut down imminently, or will not start.

Crew Awareness

On Ground: No Go

L Fuel Valve FailR Fuel Valve FailL-R Fuel Valve Fail

Indicated Firewall Fuel Valve(s) is not in commanded position.

Crew Awareness

On Ground: No Go

Gear System Fault Detected failure or loss of communication within LGCIM1 or LGCIM2.

NOTE:• Loss of redundancy in landing gear systems.• Normal Landing Gear extension and retraction

still functional.

Crew Awareness

On Ground: MEL

L Generator OffR Generator Off

Indicated GEN switch is OFF, while engine is running.

Crew Awareness

On Ground: No Go





L-R Generator Off L and R GEN switches are both OFF, while both engines are running.

NOTE:APU start disabled in air.

Crew Awareness

On Ground: No Go

Gnd Spoiler Disarmed GROUND SPOILER switch is selected OFF. Crew Awareness

On Ground: No Go

GPS 1 FailGPS 2 Fail

Indicated GPS has failed a continuous BIT check.

NOTE:• FMS uses operative GPS.• Loss of navigation redundancy.

Crew Awareness. RNP approaches with missed approach RNP less than 1.0 prohibited.

On Ground: MEL

GPS 1-2 Fail Both GPSs have failed a continuous BIT check.

NOTE:Loss of GPS as navigation information source and GPS approach capability.

In Flight:Navigate using other navigational sources: VOR, DME, ADF, FMS.RNP approaches prohibited.On Ground: MEL

Ground Prox Fail Ground Proximity function of TAWS system has failed.

Crew Awareness

On Ground: MEL

Gustlock On Ground Only CAS MSG.Gustlock is not fully OFF.

Ensure Gustlock Handle is fully down before takeoff.

N/A

High Field Operation The airplane is operating in a high field altitude mode.

NOTE:• Cabin Alt High warning reset to 14,200 FT.• CAS MSG clears above 25,000 FT or if cabin

altitude is below 9800 FT.

In Flight:Monitor Cabin Altitude.Observe crew / passenger oxygen requirements.

N/A

L Hyd Fluid LowR Hyd Fluid LowL-R Hyd Fluid Low

Reservoir fluid level is low.

NOTE:PTU is inoperative.

Crew Awareness

On Ground: No Go

L Hyd FW Valve FailR Hyd FW Valve FailL-R Hyd FW Valve Fail

Indicated hydraulic firewall valve is not in commanded position.

In Flight:

1. Verify FIRE Handle position.

If pulled:

a. Hydraulic shutoff may be incomplete.

If not pulled:

a. Hydraulic pressure may be zero.

On Ground: No Go

Hyd PTU Not Auto The POWER TRANSFER switch is in the OFF (depressed) position.

Crew Awareness

On Ground: No Go





AS-15 P/N 401-590001-0078

L Hyd Pump Fail/OffR Hyd Pump Fail/Off

Left or Right hydraulic pump pressure is low, or has been switched OFF.

NOTE:• PTU pressure will be available on Failed / Off

side.• The PTU will shut down if the EMERGENCY /

PARKING Brake is SET. This will cause a lossof hydraulic pressure on the affected side.Nosewheel Steering will fail due to loss of righthydraulic pressure.

Crew Awareness

On Ground: MEL

L-R Hyd Pump Fail/Off Left and Right hydraulic pump pressures are low, or have been switched OFF.

Crew Awareness

On Ground: No Go

Ice Detector 1 FailIce Detector 2 Fail

Indicated ice detector is inoperative.

NOTE:• Ice detection is still functional.• Loss of redundancy.

Crew Awareness

On Ground: MEL

Icing Ice detected with all Anti-ice / De-ice switches selected ON and operational.

Crew Awareness

On Ground: N/A

Int Baggage Door Open Interior Baggage Door not closed below 35,500 FT.

Crew Awareness

On Ground:

1. Check visually and secure if not closed.

If CAS MSG is still posted:

a. Dispatch via MEL. MEL

IRS 1 AligningIRS 2 AligningIRS 1-2 Aligning

Ground Only CAS MSGs. Indicated IRS has not yet completed its alignment.


Lavatory Smoke Fail Lavatory Smoke Detector Fail (If installed). Crew Awareness

On Ground: MEL

Mach Trim 1 FailMach Trim 2 Fail

Indicated Mach Trim channel has failed.

NOTE:• Loss of redundancy.• Mach Trim function automatically switches to

the other AFCS.

Crew Awareness

On Ground: MEL

Mach Trim 1-2 Fail Both Mach Trim channels have failed below 0.78M / 300 KIAS.

In Flight:Do not exceed 0.78M / 300 KIAS.

On Ground: MEL

Maint Computer Fail Ground Only CAS MSG.CMC has failed.

Crew Awareness MEL

Manual Press On Pressurization is in manual mode. Crew Awareness

On Ground: No Go





MAU Fan Fail Modular Avionics Unit (MAU) 1 or 2 has lost a cooling fan.


Crew Awareness

On Ground: No Go

MCDU 1 CB Ctrl FailMCDU 2 CB Ctrl Fail

Loss of communication between SPDA and MCDU on indicated side.

NOTE:Loss of all electronic CB control and access on indicated MCDU.

In Flight:Use other MCDU for CB control.

On Ground: MEL

MCDU 1-2 CB Ctrl Fail Loss of communication between SPDA and MCDU.

NOTE:Loss of all electronic CB control and access.

Crew Awareness

On Ground: No Go

Nosewheel Steer Fault SOV stuck open for >2 seconds.

NOTE:• No loss of steering.• Loss of runaway protection.

Crew Awareness

On Ground:Minimize Taxi time and speed.

No Go

L Oil Filter BypassR Oil Filter BypassL-R Oil Filter Bypass

High differential pressure detected across oil filter for indicated engine, impending filter bypass.

Crew Awareness

On Ground: No Go

Pack High Flow Left or Right, or Left and Right Pack is in high flow.

In Flight:Use High Flow Performance data.

On Ground:Use High Flow Performance data.

N/A

L Pack OffR Pack Off

Indicated Pack has been selected OFF, and the inlet valve has been closed.

Crew Awareness

On Ground: MEL

L-R Pack Off Left and Right Packs have been selected OFF, and the inlet valves have been closed.

Crew Awareness

On Ground: No Go

Park Brake On Ground Only CAS MSG.Park Brake is not fully OFF.

Ensure Park Brake Handle is fully down before takeoff.

N/A

Passenger Oxy Deploy The passenger oxygen pressure switch has activated (automatic or manual deploy).

Crew Awareness

On Ground: MEL

Phone Call Call received on Handset. Retrieve Call. N/A

Pusher 1 FailPusher 2 Fail

Indicated stick pusher channel is inoperative.


Crew Awareness

On Ground: No Go

L Pylon Vent NotOpenR Pylon Vent NotOpen

Indicated Pylon Vent did not open, (failed in closed position).

Crew Awareness

On Ground: MEL

L-R Pylon Vent NotOpen Left and Right Pylon Vents did not open, (failed in closed position).

Crew Awareness

On Ground: No Go





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401-590001-0078TC4

Temporary Changeto the


P/N 401-590001-0078TC4

SECTION 3B - ABNORMAL PROCEDURES


Read the following Cyan “MAU Fan Fail” CAS MSG in place of the current Cyan “MAU Fan Fail” CAS MSG:

Publication Affected FAA Approved Airplane Flight Manual, P/N 401-590001-0078, dated Aug 8, 2011, or later revision for Hawker Model 4000 Airplanes.

Airplane Serial Numbers Affected

RC-59 and After or Prior Airplane Serials with Kit 401-3007 or 401-3008 or 401-3027 or 401-3028 Installed for Block Point Upgrade A.

Description of Change Revised Cyan “MAU Fan Fail” CAS MSG from “No Go” to “MEL”.

Filing Instructions Insert Page 1 of 2 to face page AS-16 in Section 3B - Advisory/Status Procedures.


MAU Fan Fail Modular Avionics Unit (MAU) 1 or 2 has lost a cooling fan.

NOTE:

Loss of redundancy.

Crew Awareness

On Ground: MEL

Aug 2, 2012

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AS-17 P/N 401-590001-0078

Rigging Complete Ground Only CAS MSG.Rigging process has successfully been completed.

NOTE:• Maintenance switch is still out of OFF position.

• CAS MSG will beposted.


Rudder Fault Indicates a loss of redundancy in the rudder system.

NOTE:

A cycling CAS MSG will post below 155 KIAS during PTU operation when the Right Hydraulic System is being operated by the PTU and pressure momentarily drops below 2300 PSI.

In Flight:

NOTE:

CAS MSG will post after switching AUX PUMP to ON.

If CAS MSG is cycling:

1. Select AUX PUMP to ON.

If CAS MSG is steady:

1. Crew Awareness

On Ground: No Go

Rudder Trim Fail A failure is detected in the rudder trim system or RUDDER TRIM POWER has been selected to OFF.

NOTE:Accompanied by amber “X” on trim indicator.

In Flight:

1. Evaluate rudder trim response.

If no response in yaw:

a. Reduce yaw with rudder.

b. Use differential thrust and roll trim to reduce rudder pedal forces.

If response in yaw:

a. Use rudder trim as required to reduce rudder pedal forces.

On Ground: MEL

Selcal HF Com 1Selcal HF Com 2Selcal VHF Com 1Selcal VHF Com 2

An incoming MSG is on HF Com 1 or HF Com 2, or VHF Com 1 or 2.Selective Call ident code received on indicated radio.

In Flight:Retrieve Call.Key mic to clear MSG.

On Ground: N/A

L Shaker FailR Shaker Fail

Indicated stick shaker inoperative.

NOTE:LSA Display and/or AOA Display is available on the operative side.

Crew Awareness

On Ground: MEL


Maintenance Switch On

Rudder FaultAux Hyd Pump Not Auto

Rudder Fault

Rudder Fault




SPDA Fault SPDA detects an internal box failure that may result in none, one, or more of the following:

NOTE:

• The CAS MSG may post brieflywhen operating Thrust Reversers.

• The following systems may not operate andtheir associated CAS MSGs may not post:APU, Stby Trim, Thrust Reversers, FuelTransfer, Nosewheel Steering.

• NAV Lights may be inoperative.

• The CAS MSG may post incombination with incorrect MCDU CB status.

• Start switch “Push to Abort” may illuminate.

In Flight:

1. Perform the applicable Abnormal and/or Advisory Procedures for any posted CAS MSG(s).

NOTE:Plan for APU, Thrust Reversers and Nosewheel Steering being inoperative.

If NAV Lights are inoperative:

a. Recognition Lights ON.

2. Landing Considerations:

a. Select wide runway with minimum crosswind, no tailwind.

b. Multiply landing distance by 1.2.

c. Use rudder and differential braking.

On Ground: If Nosewheel Steering has failed:

CAUTION:Due to limited steering capability, extreme care should be taken when taxiing with Nosewheel Steering inoperative.

1. Use differential braking and/or differential thrust during taxi.

2. No Dispatch.

No Go

Spoiler Fault Minor fault in spoiler system.

NOTE:No reduction in functionality.

Crew Awareness

On Ground: MEL

Spoiler Sw Not Norm ROLL SPOILER CONTROL switch not in NORMAL position.

Crew Awareness

On Ground: No Go

Stab Trim Slow Communication is lost from MAUs.

NOTE:• Normal pitch trim responses will be slow.• AP will disengage.• Mach Trim, AP Stab Trim and Flap Trim will be

inoperative.

Crew Awareness

On Ground: No Go


SPDA Fault

CB Trip




AS-19 P/N 401-590001-0078

Stall Warn Advance Wing Anti-ice system is selected OFF and CAS MSG has been posted for 1.5

minutes, orWing Anti-ice system has been selected ON, with CAS MSG posted, and the system has failed to reach operating temperature within 2 minutes.

NOTE:• Stall Warnings will occur at lower AOAs.• The AOA indicator on the PFD will display if

selected OFF.

In Flight:Review FLIGHT AND LANDING WITH ICE ACCUMULATION ON THE WINGS (A12.17).

On Ground: No Go

Stby Trim On Standby Trim is selected ON.

NOTE:• Stby Pitch Trim rate is slow and fixed.• AP will disengage.• Mach Trim, AP Stab Trim and Flap Trim will be

inoperative.

Crew Awareness

On Ground: No Go

Sync Fail Selected Sync system is unavailable due to a detected failure of one of its required inputs or an internal failure.

NOTE:• A/T System is available.

In Flight:Synchronize engines manually (A/T OFF), or use A/T without Sync.

On Ground: MEL

Tail De-Ice Fault Minor fault in Tail De-ice System.

NOTE:System is still operative.

Crew Awareness

On Ground: MEL

TAT Probe Heat Fail Total Air Temp probe heat has failed.

NOTE:• Following CAS MSGs will be posted:

, .

• Will lose FD, AP, and A/T.• YD performance may be degraded.• Possible inaccuracies in True Airspeed data.• Total Air Temperature on PFD is replaced with

amber dashes.• Left and Right target N1 values may differ.• Stall Warning may occur slightly earlier.

In Flight:Icing Conditions, Exit / Avoid.Flight Control and Thrust, Fly Manually.

Perform the applicable Abnormal and/or Advisory Procedures for any posted CAS MSG(s).

Apply appropriate RVSM contingency procedures.

On Ground: MEL

TAWS Fail TAWS system has failed. Crew Awareness

On Ground: MEL

Terrain Fail Terrain function of Enhanced Ground Proximity Warning System (EGPWS) has failed.

Crew Awareness

On Ground: MEL


Icing

Icing

Autothrottle 1-2 Fail AP 1-2 Fail




L Thrust Rvsr FaultR Thrust Rvsr FaultL-R Thrust Rvsr Fault

Sensors indicate: Thrust Reversers are not stowed or locked, or hydraulic pressure is not isolated, ormiscompare of Thrust Lever input, or miscompare of Thrust Reverser WOW signal.

NOTE:Thrust Reverser deployment may be delayed. May be the result of early selection of Thrust Reversers during landing.

Crew Awareness

On Ground:

NOTE:• Only one deploy cycle is permitted

to check Thrust Reverser operation.• Maintenance Log entry is required.• A maximum of three consecutive

flights is permitted with MaintenanceLog entries.

• After third consecutive entry,maintenance action will be required.

To Check Operation:

1. Thrust Reversers (1 cycle) - Deploy (verify deployed for 3 seconds, T/R icon green).

2. Thrust Reversers - Stow (verify T/R icon clears).

If CAS MSG is still posted or maintenance log entries are exceeding 3 consecutive flight cycles:

a. Dispatch via MEL.

If Cyan “# Thrust Rvsr Fault” CAS MSG clears after 1 cycle and maintenance log entries do not exceed 3 consecutive flight cycles:

a. Normal Dispatch.

MEL

T/O Config Flaps T/O Config SpeedbrakeT/O Config Trim

Ground Only CAS MSGs.Indicated configuration is not permitted for takeoff.


TRU 1 FailTRU 2 Fail

Loss of power to the indicated TRU or internal failure of the indicated TRU.

NOTE:For Single TRU Operation, the following items are automatically shed:Cabin Lighting, Water Heater, Water Pump, Airshow, Additional Cabin and Lavatory items and PA System.

The following optional items are automatically shed:CMF, AirCell, HF 2.

In Flight:Manual restore of electrical loads is prohibited if TRU 1 or TRU 2 is failed.

On Ground: No Go


# Thrust Rvsr Fault




AS-21 P/N 401-590001-0078

TRU 3 Fail Loss of power to the indicated TRU or internal failure of the indicated TRU.

NOTE:Emergency Rudder System (ERS) will use Battery 2 and TRU 2 power.

Crew Awareness

On Ground: MEL

Windshear Fail Windshear warning not available. Crew Awareness

On Ground MEL

Windshield Heat Off One or both Windshield Heat switches are selected OFF.

NOTE:Unheated windshield may frost or fog over.

Crew Awareness

On Ground: No Go

Wing A-Ice On Ground Only CAS MSG.WING ANTI-ICE is selected ON.

Crew Awareness N/A

Wing A-Ice Temp Fault One or more Wing Temp Sensors have failed.

NOTE:System is still operative.

Crew Awareness

On Ground: No Go

Wing Bld Leak Det Fail One or more temp sensors have failed in the Anti-ice system.

Crew Awareness

On Ground: MEL

WOW Fault Loss of at least 1 WOW sensor / switch, or an internal fault in an LGCIM.

NOTE:• Loss of redundancy in WOW system.• Possible loss of Thrust Reversers.

Crew Awareness

On Ground: No Go

Yaw Damper 1 FailYaw Damper 2 Fail

Indicated YD channel has failed.

NOTE:YD, AP, Mach Trim, Flap Trim, FD and SWPS functions automatically switch to the other AFCS.

In Flight:Do not override AFCS channel change.

On Ground: MEL







Documents

HAWKER 4000 FAA APPROVED AIRPLANE FLIGHT · PDF fileFAA Approved Airplane Flight Manual AS-1 P/N 401-590001-0078 TABLE OF CONTENTS ... • An SPDA 1 communication problem is indicated