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HAWKER 400XP/BEECHJET 40

Revision .02 August 2011

MEMORY FLASH CARDS

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INSERT LATEST REVISED CARDS, DESTROY SUPERSEDED CARDSLIST OF EFFECTIVE CARDS

Dates of issue for original and changed pages are:

Original ............ 0................. MARCH 2006Revision........ .01..................... March 2008

Revision........ .02.................... August 2011

TOTAL NUMBER OF CARDS IN THIS SET IS 46CONSISTING OF THE FOLLOWING:

*Zero in this column indicates an original card.

Card *RevisionNo. No.

Title....................................................... .02

ii ............................................................ .02E-1........................................................ .01E-1A...................................................... .02

CardNo.

E-2E-7.......................................

E-7A..............................................E-8E-25A ..................................L-1L-22A ...................................

Revision .02

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Emergency

Hawker 400XP/Beechjet 400A

ENGINE FAILURE DURING TAKEOF

(BELOW V1TAKEOFF ABORTED

Revision .01

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ENGINE FAILURE DURING TAKEOF(BELOW V1TAKEOFF ABORTED

If engine fire indications exist, do not deploy reverser on the affected eWARNING

Hawker 400XP/Beechjet 400ARevision .02

1. Brakes ..............................................................................................A2. Thrust ...............................................................................................3. Thrust Reverser(s) .......................................................................DE

4. Reverser Lights..............................................................................V5. Reverse Thrust ...................................................................AS REQ6. Speed Brakes ...............................................................................EX

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Emergency


ENGINE FAILURE DURING TAKEOF

(ABOVE V1TAKEOFF CONTINUED

Revision .01

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ENGINE FAILURE DURING TAKEOF(ABOVE V1TAKEOFF CONTINUED


1. Nose Up Pitch Attitude at Rotation (VR)......................... 1315 DE2. Landing Gear (When positive climb established).............................3. Airspeed..................................................................................... MAINT

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Emergency


ENGINE FIREBell sounds and

OR

Revision .01

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ENGINE FIRE


1. Thrust (affected engine) .................................................................If ENG FIRE PUSH switch remains illuminated:

2. Thrust Lever (affected engine) ................................................. CU3. Illuminated Engine Fire Switch .....................................................4. Either Fire Bottle Switch................................................................

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Emergency


ENGINE FIRE DETECTOR FAILURE

OR

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ENGINE FIRE DETECTOR FAILURE

If the FIRE DET FAIL annunciator illuminates following an ENG FIREswitch illumination, the fire should be considered to still be burning

3. Land......................................................... NEAREST SUITABLE A

If the FIRE DET FAIL annunciator illuminates without an ENG FIRE PUswitch illumination or any other indication of an engine fire:

4. Repair fault prior to the next flight.


1. Engine Fire Procedures ....................................................... COMP2. Remaining Illuminated Engine Fire Bottle Switch ......................

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Emergency


ENGINE FAILURE IN LANDING

CONFIGURATION

Revision .01

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ENGINE FAILURE IN LANDINGCONFIGURATION


1. Thrust (operating engine)............................................... AS REQ2. Airspeed............................................................................................

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Emergency


DUAL ENGINE FLAMEOUT

Revision .01

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DUAL ENGINE FLAMEOUT


Immediate Relight:

1. N2 .......................................................................... VERIFY ABOV

Engine damage may result if an immediate relightis attempted below 52% N2.

2. Ignitions..........................................................................................

If N2 Is Not Above 52% Or Neither Engine Relights:

3. Battery ..........................................................................................

CAUTION

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Emergency


INADVERTENT THRUST REVERSERDEPLOYMENT DURING TAKEOFF


OR

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1. Brakes ..............................................................................................A2. Thrust ...............................................................................................3. Thrust Reversers...............................................................BOTH DE4. Reverser Lights..............................................................................V

5. Reverse Thrust ...................................................................AS REQ6. Speed Brakes ...............................................................................EX

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OR OR

Emergency


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1. Emergency Stow Push-Switch (affected engine).............................2. Nose Up Pitch Attitude at Rotation (VR)......................... 1315 DE3. Landing Gear (when positive climb established)..............................4. Airspeed.............................................................................................. V

If reverser will not stow and lock:

5. Thrust Lever (affected engine) ................................................. CU

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Emergency


INADVERTENT THRUST REVERSERDEPLOYMENT IN FLIGHT

OR OR

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INADVERTENT THRUST REVERSERDEPLOYMENT IN FLIGHT


1. Emergency Stow Push-Switch (affected engine).............................2. Altitude......................................................................... BELOW 30,0003. Airspeed (until reverser stows/locks) ........................... BELOW 135

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Emergency


INADVERTENT OVERSPEED

Revision .01

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INADVERTENT OVERSPEED


1. Thrust ................................................................................................2. Speed Brakes ............................................................................. EX3. If airplane is in a nosedown attitude, initiate a wings-level pullu

out exceeding structural limits (3.2 g)

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Emergency


LOSS OF AIRSPEED INDICATION

Revision .01

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LOSS OF AIRSPEED INDICATION


1. Autopilot ............................................................................ DISCON2. Airspeed.......................................... SLOW TO AND MAINTAIN 0.3. Thrust ............................................................................... AS REQ4. Speed Brakes................................................................... AS REQ

(SLOW TO 0.25 AOA WITH SPEED BRAKES EXTENDED)

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Emergency


ELECTRICAL FIRE OR SMOKE

Revision .01

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ELECTRICAL FIRE OR SMOKE


1. Oxygen Masks .................................................................................2. Smoke Goggles ...............................................................................

3. Mic Selectors ......................................................................... OXY4. SPKR Switches (Pilot and Copilot) ................... ON or DON HEA5. INTPH Switch (Pilot).........................................................................6. Smoke Removal Procedures......................................... IF NECES

If Known Source:7. Faulted Circuits ......................................................................... ISO

If Unknown Source:8. Battery.............................................................................................9. Master Generator Switches...........................................................

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Emergency


ENVIRONMENTAL SYSTEM

SMOKE OR ODOR

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ENVIRONMENTAL SYSTEMSMOKE OR ODOR


1. Oxygen Masks..........................................................................................2. Smoke Goggles........................................................................................3. Mic Selectors.................................................................................. OXY 4. SPKR Switches (Pilot and Copilot) ......................... ON or DON HEA5. INTPH Switch (Pilot) ................................................................................6. Cabin Pressure Source ...................................... ISOLATE SOUR

SELECTING L ENG OR

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Emergency


SMOKE REMOVAL

Revision .01

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SMOKE REMOVAL


1. Oxygen Masks..........................................................................................

2. Smoke Goggles........................................................................................3. Mic Selectors.................................................................................. OXY 4. SPKR Switches (Pilot and Copilot) ......................... ON or DON HEA5. INTPH Switch (Pilot) ................................................................................

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Emergency


CABIN DECOMPRESSION

Revision .01

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CABIN DECOMPRESSION


1. Oxygen Masks..........................................................................................2. Mic Selectors.................................................................................. OXY 3. SPKR Switches (Pilot and Copilot) ......................... ON or DON HEA4. INTPH Switch (Pilot) ................................................................................

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Emergency


EMERGENCY DESCENT

Revision .01

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EMERGENCY DESCENT


1. Thrust ................................................................................................2. Speed Brakes ............................................................................. EX3. Autopilot...........................................................................................4. Initiate Moderate Bank............................................................... 45

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Emergency


OVERPRESSURIZATION

Revision .01

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OVERPRESSURIZATION


1. Cabin Pressure Source.........................................................................2. Oxygen Masks........................................................................................3. Mic Selectors ............................................................................... OXY 4. SPKR Switches (Pilot and Copilot)........................ ON or DON HEA5. INTPH Switch (Pilot)..............................................................................

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LOSS OF BOTH GENERATORS

AND

Emergency


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LOSS OF BOTH GENERATORS


1. GEN FLD and START/GEN Circuit Breakers(AFT MAIN PANEL) ........................ C

2. Generator Reset (L and R)............................................... RESET/

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Emergency


PITCH TRIM RUNAWAY OR FAILURROLL TRIM RUNAWAY OR FAILUR

RUDDER TRIM RUNAWAY OR FAILU

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PITCH TRIM RUNAWAY OR FAILURROLL TRIM RUNAWAY OR FAILUR

RUDDER TRIM RUNAWAY OR FAILU


1. Trim Interrupt/AP Disengage Switch ........................ PUSH AND

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Emergency


POWER BRAKE FAILURE

POWER BRAKE FAILURE

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POWER BRAKE FAILURE


1. Break Safety Wire and Remove Guard Clip on Emergency Brake

2. Emergency Brakes................................................. APPLY GRAD

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Emergency


AUTOPILOT TRIM FAIL

Revision .01

AUTOPILOT TRIM FAIL

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AUTOPILOT TRIM FAIL


1. Trim Indicators.................................. CHECK FOR PROPER POSFOR FLIGHT COND

2. Trim Interrupt/AP Disengage Switch ............................................

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Emergency


AUTOPILOT OVERSPEED RECOVER

Revision .01


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1. Thrust ................................................................................................

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Emergency


FLIGHT DIRECTOR MALFUNCTION

Revision .01


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1. Trim Interrupt/AP Disengage Switch ............................................

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Limitations

MAXIMUM OPERATING AIRSPEED

VMO S.L. to 8,000 ft ......................................................

VMO

8,000 to 11,000 ft .................................................

VMO 11,000 to 26,000 ft ...............................................

Limiting Mach MMO above 26,000 ft.............................


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MAXIMUM OPERATING AIRSPEED

VMO

S.L. to 8,000 ft ......................................................

VMO 8,000 to 11,000 ft ............ 264 to 320 linear var

VMO 11,000 to 26,000 ft ...............................................

Limiting Mach MMO above 26,000 ft.............................


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Limitations

FLAP EXTENSION AND OPERATIO

VFE/VFO Flaps 10 and 20..........................................

VFO Flaps 30...............................................................

VFE Flaps 30 ...............................................................


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FLAP EXTENSION AND OPERATIO

VFE/VFO Flaps 10 and 20 ..........................................

VFO Flaps 30...............................................................

VFE Flaps 30 ...............................................................


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Limitations

LANDING GEAR & LIGHTS

Landing Gear Normal Operation VLO ...........................

Landing Gear Extended VLE.........................................

Landing Gear Emergency Operation VLO ....................Landing Lights VLL........................................................



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Landing Gear Normal Operation VLO

...........................

Landing Gear Extended VLE.........................................

Landing Gear Emergency Operation VLO.....................

Landing Lights VLL ........................................................


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Limitations

SPEEDBRAKES

VSB


SPEEDBRAKES

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SPEEDBRAKES

VSB

No Limit


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Limitations

MINIMUM CONTROLLABLE AIRSPEAIRBORNE & GROUND

Airborne VMCA Flaps 0................................................

Airborne VMCA Flaps 10 and 20 ................................Ground VMCG Flaps 0, 10, and 20...........................


MINIMUM CONTROLLABLE AIRSPE

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MINIMUM CONTROLLABLE AIRSPEAIRBORNE & GROUND

Airborne VMCA Flaps 0................................................

Airborne VMCA Flaps 10 and 20 ................................

Ground VMCG Flaps 0, 10, and 20 ...........................


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Limitations

WINDSHIELD WIPERS

VWW


WINDSHIELD WIPERS

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WINDSHIELD WIPERS

VWW

200 (If Installed)


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Limitations

TIRE LIMITING SPEED

VTIRE


TIRE LIMITING SPEED

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TIRE LIMITING SPEED

VTIRE

165

True speed on the ground


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Limitations

ENGINE SPEEDS

Takeoff N1 Fan .................................................................

Takeoff N2 Turbine............................................................

Idle N2 Turbine, Engine EFC ON.....................................Idle N2 Turbine, Engine EFC OFF, in nonicing condition


ENGINE SPEEDS

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Takeoff N1 Fan............................................................

Takeoff N2 Turbine ........................................................

Idle N2 Turbine, Engine EFC ON..................................

Idle N2 Turbine, Engine EFC OFF,

in nonicing conditions ...................................................


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Limitations

ENGINE TEMPERATURES

Takeoff ITT....................................................................

Starting ITT...................................................................

...................................................................ITT for maximum continuous thrust..............................


ENGINE TEMPERATURES

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Takeoff ITT................................................................ 7

Starting ITT.... 550 C to 600 C for 4 seconds max

.... 600 C to 700 C for 2 seconds max

ITT for maximum continuous thrust .......................... 6


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Limitations

ENGINE OIL

Oil Temperature takeoff and max continuous thrust .....

Oil Pressure takeoff and max continuous thrust ..........

Minimum Oil Temperature for Starting ..........................Oil Pressure at Idle RPM..............................................


ENGINE OIL

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Oil Temperature takeoff and

max continuous thrust ................................... 10 to 1Oil Pressure takeoff andmax continuous thrust ..................................... 60 to 8

Minimum Oil Temperature for Starting......................

Oil Pressure at Idle RPM ......................... 40 PSI min


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Limitations

THRUST REVERSER LIMITATIONS

Full Reverse Cutoff Speed ...........................................

Time For Continuous Reverse Thrust above reverse idle

Deployed Time during taxi operations ..........................


THRUST REVERSER LIMITATIONS

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Full Reverse Cutoff Speed..................... 55 KIAS or a

Continuous Reverse Thrustabove reverse idle .......................... 30 seconds max

Deployed Time during taxi operations................ 5 sec


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Limitations

External Power Assisted StartLimited to three (3) cycles as follow


1st Cycle: ?Seconds ON ?Minutes O

2nd Cycle: ?Seconds ON ?Minutes O

3rd Cycle: ?Seconds ON ?Minutes O

External Power Assisted Start

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External Power Assisted StartLimited to three (3) cycles as follow


1st Cycle: 30Seconds ON 5Minutes O

2nd Cycle: 30Seconds ON 15Minutes

3rd Cycle: 30Seconds ON 60Minutes

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Limitations

BATTERY START

Do not attempt battery start if

battery voltage is below _____ volts.


BATTERY START

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Do not attempt battery start ifbattery voltage is below 22 volts.


Li i i

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Limitations

GENERATOR ASSISTED START

Do not attempt to start the second engine

until the generator load is below ____ amps.


GENERATOR ASSISTED START

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Do not attempt to start the second engineuntil the generator load is below 150 amps.


Li it ti

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Limitations

STARTER-GENERATOR LIMITS

Ground Operation

Maximum Generator Load



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Ground Operation

Maximum Generator Load

280 AMPS EACH GENERATOR


Li it ti

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Limitations


In-Flight Operation:


Both Generators Operating Up to 41,000 ft ?

Both Generators Operating Above 41,000 ft ?


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Both Generators Operating Up to 41,000 ft 280 AM EAC

Both Generators Operating Above 41,000 ft260 AM

EAC

Limitations

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Limitations



One Generator Operating Up to 29,000 ft

One Generator Operating Up to 29,000 ft Icing Cond.

TRANSIENT Below 20,000 ft, 30 Seconds Maximum One Generator Operating From 29,000 ft to 41,000 ft

One Generator Operating Above 41,000 ft


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g p


One Generator Operating Up to 29,000 ft

One Generator Operating Up to 29,000 ft Icing Cond.

TRANSIENT Below 20,000 ft, 30 Seconds Maximum

One Generator Operating From 29,000 ft to 41,000 ft

One Generator Operating Above 41,000 ft

Limitations

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STRUCTURAL LIMITATIONS

Limitations


UNMODIFIED RK 344 AND A RK 1-343 OR MODIFI

Maximum Ramp Weight ? ?

Maximum Takeoff Weight ? ?Maximum Landing Weight ?

Maximum Zero Fuel Weight ?

STRUCTURAL LIMITATIONS

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UNMODIFIED RK 344 AND A RK 1-343 OR MODIFI

Maximum Ramp Weight 16,300 lbs 16,500 lbs

Maximum Takeoff Weight 16,100 lbs 16,300 lbs

Maximum Landing Weight 15,700 lbs

Maximum Zero Fuel Weight 13,000 lbs

Limitations

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Limitations

MANEUVERING LOAD FACTORS

Flaps 0 ........................................................................

Flaps 10, 20, and 30 ................................................


MANEUVERING LOAD FACTORS

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Flaps 0......................................................... -1.0 to +Flaps 10, 20, and 30..................................... 0 to +


Limitations

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Limitations

TAKEOFF AND LANDING OPERATIO

Airfield Operation Pressure Altitude .............................

Ambient Temperature....................................................

Maximum Tailwind Component for Takeoff and LandingMaximum Fuel Unbalance for Takeoff ..........................

Maximum Fuel Unbalance for Landing.........................


TAKEOFF AND LANDING OPERATIO

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Airfield Operation Pressure Altitude ...... UP TO 10,00

Ambient Temperature....................... 40 C to ISA + Maximum Tailwind Componentfor Takeoff and Landing......................................... 10

Maximum Fuel Unbalance for Takeoff ..................... 10

Maximum Fuel Unbalance for Landing.................... 30


Limitations

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Limitations

FUEL LIMITS

Minimum Fuel Temperature ..........................................

Maximum Fuel Temperature .........................................


FUEL LIMITS

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Minimum Fuel Temperature ...................................... Maximum Fuel Temperature..................................... +


Limitations

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Limitations

ENROUTE OPERATIONSCertified Ceiling ............................................................

Ambient Air Temperature..............................................

Maximum Fuel Unbalance............................................

Yaw Damper .................................................................

Extension of gear, flaps, or landing lights.....................

Refrigerant Air Conditioning .........................................


ENROUTE OPERATIONSCertified Ceiling.................................................... 45,0

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g ,

Ambient Air Temperature .................. 65 C to ISA +

Maximum Fuel Unbalance....................................... 30Yaw Damper............... Operable and on for flight in

conditions or flight above 28,0

Extension of gear, flaps,or landing lights...................... Prohibited above 20,0

Refrigerant Air Conditioning .... Prohibited above 18,0


h4xpbj4a mfc r02

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