be20 flashcards

King Air BEKing Air BE--200/B200200/B200

Flash CardsFlash Cards

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Memory ItemsMemory Items

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ENGINE FAILURE/EMERGENCY ENGINE ENGINE FAILURE/EMERGENCY ENGINE


SHUTDOWNSHUTDOWN

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ENGINE FAILURE/EMERGENCY ENGINE ENGINE FAILURE/EMERGENCY ENGINE


SHUTDOWNSHUTDOWN

11 C diti lC diti l FUEL CUTOFFFUEL CUTOFF1.1. Condition lever Condition lever –– FUEL CUTOFFFUEL CUTOFF2.2. Propeller lever Propeller lever –– FEATHERFEATHER3.3. Firewall shutoff valve Firewall shutoff valve –– CLOSECLOSE4.4. Fire extinguisher (if installed) Fire extinguisher (if installed) –– ACTUATE ACTUATE

IF FIRE WARNING PERSISTSIF FIRE WARNING PERSISTS

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ENGINE FAILURE INENGINE FAILURE IN--FLIGHT BELOW VFLIGHT BELOW VMCAMCA


MCAMCA

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ENGINE FAILURE INENGINE FAILURE IN--FLIGHT BELOW VFLIGHT BELOW VMCAMCA


MCAMCA

1.1. Power Power –– REDUCE AS REQUIRED TO REDUCE AS REQUIRED TO MAINTAIN DIRECTIONAL CONTROLMAINTAIN DIRECTIONAL CONTROL

2.2. Nose Nose –– LOWER TO ACCELERATE ABOVE VLOWER TO ACCELERATE ABOVE VMCAMCA

3.3. Power (operating engine) Power (operating engine) –– ADJUST AS ADJUST AS REQUIREDREQUIRED

44 F il d iF il d i SECURE (EMERGENCYSECURE (EMERGENCY4.4. Failed engine Failed engine –– SECURE (EMERGENCY SECURE (EMERGENCY ENGINE SHUTDOWN)ENGINE SHUTDOWN)

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ENGINE FAILURE DURING TAKEOFF ENGINE FAILURE DURING TAKEOFF


(AT OR BELOW V(AT OR BELOW V11) TAKEOFF ABORTED) TAKEOFF ABORTED

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(AT OR BELOW V(AT OR BELOW V11) TAKEOFF ABORTED) TAKEOFF ABORTED1.1. Power leversPower levers –– IDLEIDLE1.1. Power levers Power levers IDLEIDLE2.2. Brakes Brakes –– AS REQUIREDAS REQUIRED33 Operating engineOperating engine MAXIMUM REVERSEMAXIMUM REVERSE3.3. Operating engine Operating engine –– MAXIMUM REVERSE MAXIMUM REVERSE

(if required)(if required)

W iW i E i t hE i t hWarning: Warning: Exercise extreme care when Exercise extreme care when using single engine reversing onusing single engine reversing onsurfaces with reduced tractionsurfaces with reduced traction

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surfaces with reduced traction.surfaces with reduced traction.




(AT OR BELOW V(AT OR BELOW V11) TAKEOFF ABORTED ) TAKEOFF ABORTED (Cont’d.)(Cont’d.)

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(AT OR BELOW V(AT OR BELOW V11) TAKEOFF ABORTED ) TAKEOFF ABORTED (Cont’d.)(Cont’d.)

If i ffi i t i f t iIf i ffi i t i f t iIf insufficient runway remains for stopping:If insufficient runway remains for stopping:Emergency Engine Shutdown Emergency Engine Shutdown —— EXECUTEEXECUTE4.4. Condition Levers Condition Levers —— FUEL CUTOFFFUEL CUTOFF5.5. Propeller Levers Propeller Levers —— FEATHERFEATHER6.6. Fuel Firewall Valves Fuel Firewall Valves —— CLOSEDCLOSED7.7. Master Switch Master Switch —— OFF (gang bar down)OFF (gang bar down)

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(g g )(g g )


ENGINE FIRE ON GROUNDENGINE FIRE ON GROUND


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ENGINE FIRE ON GROUNDENGINE FIRE ON GROUND


1.1. Condition lever Condition lever –– FUEL CUTOFFFUEL CUTOFF2.2. Fuel firewall valve Fuel firewall valve –– CLOSECLOSE3.3. Ignition and engine start switch Ignition and engine start switch ––

STARTER ONLYSTARTER ONLYIf fire persists:If fire persists:4.4. Fire extinguisher Fire extinguisher –– ACTUATEACTUATE

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(AT OR ABOVE V(AT OR ABOVE V11) TAKEOFF CONTINUED) TAKEOFF CONTINUED

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11 PP MAXIMUM ALLOWABLEMAXIMUM ALLOWABLE1.1. Power Power –– MAXIMUM ALLOWABLEMAXIMUM ALLOWABLE2.2. Airspeed Airspeed –– MAINTAIN TAKEOFF SPEED OR MAINTAIN TAKEOFF SPEED OR

ABOVEABOVEABOVEABOVE3.3. Landing gear Landing gear –– UPUP44 P ll (P ll (ii i )i ) CONFIRMCONFIRM4.4. Propeller (Propeller (inopinop engine) engine) –– CONFIRM CONFIRM

AUTOFEATHER OR FEATHERAUTOFEATHER OR FEATHER55 AirspeedAirspeed VV (after obstacles cleared V(after obstacles cleared V ))

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5.5. Airspeed Airspeed –– VV22 (after obstacles cleared, V(after obstacles cleared, VYSEYSE))


ENGINE FLAMEOUT (2ENGINE FLAMEOUT (2NDND ENGINE)ENGINE)


(( ))

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ENGINE FLAMEOUT (2ENGINE FLAMEOUT (2NDND ENGINE)ENGINE)


(( ))

1.1. Power lever Power lever –– IDLEIDLE2.2. Propeller Propeller –– DO NOT FEATHERDO NOT FEATHER3.3. Condition lever Condition lever –– FUEL CUTOFFFUEL CUTOFF4.4. AirstartAirstart procedures procedures –– CONDUCTCONDUCT

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GLIDE (BOTH ENGINES INOPERATIVE)GLIDE (BOTH ENGINES INOPERATIVE)


( )( )

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GLIDE (BOTH ENGINES INOPERATIVE)GLIDE (BOTH ENGINES INOPERATIVE)


( )( )

1.1. Landing gear Landing gear –– UPUP2.2. Flaps Flaps –– UPUP3.3. Propellers Propellers –– FEATHEREDFEATHERED4.4. Airspeed Airspeed –– 135 KTS135 KTS

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CHIP DETECTCHIP DETECT


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CHIP DETECTCHIP DETECT


1.1. Affected engine Affected engine –– EMERGENCY EMERGENCY SHUTDOWN (BESHUTDOWN (BE 200 Only)200 Only)SHUTDOWN (BESHUTDOWN (BE--200 Only)200 Only)

2.2. BEBE--B200 B200 –– No memory itemsNo memory items

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DUAL GENERATOR FAILUREDUAL GENERATOR FAILURE


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DUAL GENERATOR FAILUREDUAL GENERATOR FAILURE


1.1. Generators Generators –– RESET, THEN ONRESET, THEN ONIf either generator will reset:If either generator will reset:2.2. Operating generator Operating generator loadmeterloadmeter –– DO NOT DO NOT

EXCEED 100% (88% above 31,000 ft.)EXCEED 100% (88% above 31,000 ft.)Note: This checklist applies to BBNote: This checklist applies to BB--1439,1439,

BBBB--1444 thru BB1444 thru BB--1842 except BB1842 except BB--14631463and BBand BB--1834; BL1834; BL--139 thru BL139 thru BL--147; BW147; BW--11thru BWthru BW--2929

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thru BWthru BW--2929


INVERTER FAILUREINVERTER FAILURE



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1.1. Other inverter Other inverter –– SELECTSELECT

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L or R FUEL PRESSL or R FUEL PRESS


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L or R FUEL PRESSL or R FUEL PRESS


1.1. Standby boost pump (failed side) Standby boost pump (failed side) –– ONON

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UNSCHEDULED ELECTRIC ELEVATOR TRIMUNSCHEDULED ELECTRIC ELEVATOR TRIM


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UNSCHEDULED ELECTRIC ELEVATOR TRIMUNSCHEDULED ELECTRIC ELEVATOR TRIM


1.1. Aircraft attitude Aircraft attitude –– MAINTAIN USING MAINTAIN USING ELEVATOR CONTROLELEVATOR CONTROLELEVATOR CONTROLELEVATOR CONTROL

2.2. Control wheel disconnect Control wheel disconnect –– DEPRESS DEPRESS FULLY (2FULLY (2ndnd level)level)FULLY (2FULLY (2ndnd level)level)

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UNSCHEDULED RUDDER BOOST ACTIVATIONUNSCHEDULED RUDDER BOOST ACTIVATION


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UNSCHEDULED RUDDER BOOST ACTIVATIONUNSCHEDULED RUDDER BOOST ACTIVATION


1.1. Directional control Directional control –– MAINTAIN WITH MAINTAIN WITH RUDDER PEDALSRUDDER PEDALSRUDDER PEDALSRUDDER PEDALS

2.2. Rudder boost Rudder boost –– OFFOFFIf condition persists:If condition persists:3.3. Rudder boost CB Rudder boost CB –– PULLPULL

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INADVERTENT SPININADVERTENT SPIN


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INADVERTENT SPININADVERTENT SPIN


1.1. Control column Control column –– FULL FORWARD, FULL FORWARD, AILERONS NEUTRALAILERONS NEUTRALAILERONS NEUTRALAILERONS NEUTRAL

2.2. Full rudder Full rudder –– OPPOSITE DIRECTION OF OPPOSITE DIRECTION OF SPINSPINSPINSPIN

3.3. Power levers Power levers –– IDLEIDLE44 C t lC t l NEUTRALIZE WHEN ROTATIONNEUTRALIZE WHEN ROTATION4.4. Controls Controls –– NEUTRALIZE WHEN ROTATION NEUTRALIZE WHEN ROTATION

STOPSSTOPS55 E t th ll tE t th ll t

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5.5. Execute smooth pulloutExecute smooth pullout


EMERGENCY DESCENTEMERGENCY DESCENT


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EMERGENCY DESCENTEMERGENCY DESCENT


1.1. Power levers Power levers –– IDLEIDLE2.2. Propeller levers Propeller levers –– FULL FORWARDFULL FORWARD3.3. Flaps Flaps –– APPROACHAPPROACH4.4. Landing gear Landing gear –– DOWNDOWN5.5. AirspeedAirspeed –– 181 KIAS181 KIAS5.5. Airspeed Airspeed 181 KIAS181 KIAS

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ENGINE FIRE INENGINE FIRE IN--FLIGHTFLIGHT


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ENGINE FIRE INENGINE FIRE IN--FLIGHTFLIGHT


If visual indication of fire:If visual indication of fire:1.1. Engine shutdown checklist Engine shutdown checklist ––

ACCOMPLISHACCOMPLISHIf fire persists:If fire persists:2.2. Emergency descent Emergency descent –– ACCOMPLISHACCOMPLISH

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ENVIRONMENTAL SYSTEM SMOKE OR FUMESENVIRONMENTAL SYSTEM SMOKE OR FUMES


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ENVIRONMENTAL SYSTEM SMOKE OR FUMESENVIRONMENTAL SYSTEM SMOKE OR FUMES


1.1. Crew masks (diluter demand) Crew masks (diluter demand) ––DON/EMERGDON/EMERGDON/EMERGDON/EMERG

2.2. Oxygen system ready Oxygen system ready –– CONFIRM ON CONFIRM ON (BB(BB 1439; BB1439; BB 1444 and sub1444 and sub EMERG)EMERG)(BB(BB--1439; BB1439; BB--1444 and sub. 1444 and sub. –– EMERG)EMERG)

3.3. Audio speaker Audio speaker –– ONON444.4. MicMic selector selector –– OXYGEN MASKOXYGEN MASK

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CABIN OR CARGO DOOR UNLOCKEDCABIN OR CARGO DOOR UNLOCKED


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CABIN OR CARGO DOOR UNLOCKEDCABIN OR CARGO DOOR UNLOCKED


1.1. All Occupants All Occupants –– SEATED/SEAT BELTS SEATED/SEAT BELTS FASTENED SECURELYFASTENED SECURELYFASTENED SECURELYFASTENED SECURELY

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PRESSURIZATION LOSSPRESSURIZATION LOSS


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PRESSURIZATION LOSSPRESSURIZATION LOSS


1.1. Crew masks Crew masks –– DONDON2.2. Oxygen system ready Oxygen system ready –– PULL ON (verify)PULL ON (verify)3.3. Passenger manual dropout Passenger manual dropout –– PULL ONPULL ON4.4. Audio speaker Audio speaker –– ONON5.5. MicMic selectorselector –– OXYGEN MASKOXYGEN MASK5.5. MicMic selector selector OXYGEN MASKOXYGEN MASK6.6. Descend Descend –– AS REQUIREDAS REQUIRED

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AUTOAUTO--DEPLOYMENTDEPLOYMENT OXYGEN SYSTEM FAILUREOXYGEN SYSTEM FAILURE


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AUTOAUTO--DEPLOYMENTDEPLOYMENT OXYGEN SYSTEM FAILUREOXYGEN SYSTEM FAILURE


1.1. Passenger manual dropout Passenger manual dropout –– PULL ONPULL ON

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USE OF OXYGENUSE OF OXYGEN


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USE OF OXYGENUSE OF OXYGEN


Crew:Crew:1.1. Crew masks (diluter demand) Crew masks (diluter demand) –– DONDON2.2. Oxygen system ready Oxygen system ready –– PULL ON (verify)PULL ON (verify)3.3. Audio speaker Audio speaker –– ONON4.4. MicMic selectorselector –– OXYGEN MASKOXYGEN MASK4.4. MicMic selector selector OXYGEN MASKOXYGEN MASK

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BLEED AIR LINE FAILUREBLEED AIR LINE FAILURE


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BLEED AIR LINE FAILUREBLEED AIR LINE FAILURE


1.1. Bleed air valve (affected engine) Bleed air valve (affected engine) ––INSTR/ENVIR OFF (monitor ITT and torqueINSTR/ENVIR OFF (monitor ITT and torqueINSTR/ENVIR OFF (monitor ITT and torque INSTR/ENVIR OFF (monitor ITT and torque to ensure valve closed)to ensure valve closed)

BL AIR FAIL L or RBL AIR FAIL L or R

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AnnunciatorsAnnunciators

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Engine and PropellerEngine and Propeller

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- ENGINE FIRE IN DESIGNATED ENGINEENGINE FIRE IN DESIGNATED ENGINE

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- ENGINE FIRE IN DESIGNATED ENGINEENGINE FIRE IN DESIGNATED ENGINE

Illumination of ENG FIRE lights Illumination of ENG FIRE lights indicates fire detected in indicates fire detected in nacelle area. Moisture in nacelle area. Moisture in

t fl t d li htt fl t d li htsystem or reflected sunlight system or reflected sunlight can activate can activate annunciatorannunciator(s) for (s) for aircraft prior to BB1439 1444aircraft prior to BB1439 1444aircraft prior to BB1439, 1444, aircraft prior to BB1439, 1444, BL 139 and BW1 except BL 139 and BW1 except BB 1463BB 1463

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- ENGINE FIRE TEST LIGHTSENGINE FIRE TEST LIGHTS

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Illumination of D light Illumination of D light

Annunciators Annunciators -- ENGINE FIRE TEST LIGHTSENGINE FIRE TEST LIGHTS

indicates extinguisher indicates extinguisher explosive squib has explosive squib has di h d I t t d li htdi h d I t t d li htdischarged. In test mode, light discharged. In test mode, light bulb tests OKbulb tests OK

Illumination of OK lightIllumination of OK light Illumination of OK light Illumination of OK light indicates explosive squib has indicates explosive squib has not discharged; electricalnot discharged; electricalnot discharged; electrical not discharged; electrical circuitry for fire extinguisher circuitry for fire extinguisher system is intact. Does not system is intact. Does not

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indicate bottle pressureindicate bottle pressure

King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator -- CHIP DETECT (200 only)CHIP DETECT (200 only)

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Indicates possible metal Indicates possible metal

AnnunciatorAnnunciator -- CHIP DETECT (200 only)CHIP DETECT (200 only)

contamination in the engine oil contamination in the engine oil supply. May indicate Nsupply. May indicate N22 power power

ti f il i diti f il i disection failure or impending section failure or impending failurefailure

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- CHIP DETECT (B200 only)CHIP DETECT (B200 only)

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Indicates possible metal Indicates possible metal

Annunciators Annunciators -- CHIP DETECT (B200 only)CHIP DETECT (B200 only)

contamination in the engine oil contamination in the engine oil supply. May indicate Nsupply. May indicate N22 power power

ti f il i diti f il i disection failure or impending section failure or impending failurefailure

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ENGINE LOW OIL PRESSUREENGINE LOW OIL PRESSURE

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Indicates engine oil pressure Indicates engine oil pressure

Annunciators Annunciators –– ENGINE LOW OIL PRESSUREENGINE LOW OIL PRESSURE

is below 60 PSIis below 60 PSI

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ENGINE IGNITERS ONENGINE IGNITERS ON

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ENGINE IGNITERS ONENGINE IGNITERS ON

Indicates ignition system is Indicates ignition system is activated; either the ignition activated; either the ignition

d t t it h i i ONd t t it h i i ONand start switch is in ON, or and start switch is in ON, or auto ignition switch is in ARM auto ignition switch is in ARM and engine torque is belowand engine torque is belowand engine torque is below and engine torque is below approximately 400 ft. lbsapproximately 400 ft. lbs

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King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator –– RVS NOT READYRVS NOT READY

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King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator –– RVS NOT READYRVS NOT READY

Propeller control lever(s) not Propeller control lever(s) not ( )( )full forward when landing gear full forward when landing gear switch handle is in DOWNswitch handle is in DOWN

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King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator -- PROPELLER SYNCHROPHASER IS ON PROPELLER SYNCHROPHASER IS ON

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King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator -- PROPELLER SYNCHROPHASER IS ON PROPELLER SYNCHROPHASER IS ON

Propeller Propeller synchrophasersynchrophaser is ON is ON pp y py pwith landing gear extendedwith landing gear extended

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King Air BEKing Air BE--200/B200200/B200AnnunciatorsAnnunciators –– LEFT AND RIGHT AUTOFEATHERLEFT AND RIGHT AUTOFEATHER

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King Air BEKing Air BE--200/B200200/B200AnnunciatorsAnnunciators –– LEFT AND RIGHT AUTOFEATHERLEFT AND RIGHT AUTOFEATHER

lluminationllumination of both lights of both lights indicates the AUTOFEATHER indicates the AUTOFEATHER is active. Unless both is active. Unless both

i t ill i t di t ill i t dannunciators are illuminated, annunciators are illuminated, the the autofeatherautofeather system is not system is not fully armed and operationalfully armed and operationalfully armed and operational.fully armed and operational.

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Electrical SystemElectrical System

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- DUAL GENERATOR FAILUREDUAL GENERATOR FAILURE

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- DUAL GENERATOR FAILUREDUAL GENERATOR FAILURE

I di t b th tI di t b th tIndicates both generators are Indicates both generators are offoff--lineline

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King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– INVERTER FAILUREINVERTER FAILURE

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King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– INVERTER FAILUREINVERTER FAILURE

Indicates the selected inverter Indicates the selected inverter is inoperativeis inoperative

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– GENERATOR OVERHEATGENERATOR OVERHEAT

75

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– GENERATOR OVERHEATGENERATOR OVERHEAT

Indicates the generator frame Indicates the generator frame temperature is above 157temperature is above 157°°C C (315(315°°F)F)

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– GENERATOR OFFGENERATOR OFF--LINELINE

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– GENERATOR OFFGENERATOR OFF--LINELINE

Indicates the associated Indicates the associated generator is offgenerator is off--line or failedline or failed

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King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– EXTERNAL POWEREXTERNAL POWER

79

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– EXTERNAL POWEREXTERNAL POWER

Indicates external power plug Indicates external power plug is connected to the aircraft; is connected to the aircraft; does not indicate the does not indicate the

ti l t t f thti l t t f thoperational status of the operational status of the external power unitexternal power unit

80

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– BATTERY CHARGINGBATTERY CHARGING

81

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– BATTERY CHARGINGBATTERY CHARGING

Illumination indicates battery Illumination indicates battery is being charged with 7 Amps is being charged with 7 Amps or more for 6 seconds or moreor more for 6 seconds or more

82

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– BLANK ANNUNCIATORBLANK ANNUNCIATOR

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– BLANK ANNUNCIATORBLANK ANNUNCIATOR

Spare Spare annunciatorannunciator light light position for optional position for optional equipment not installed. Spare equipment not installed. Spare li ht h ld ill i t d ili ht h ld ill i t d ilights should illuminate during lights should illuminate during annunciatorannunciator testtest

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Fuel SystemFuel System

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- FUEL PRESSUREFUEL PRESSURE

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King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- FUEL PRESSUREFUEL PRESSURE

Indicates fuel pressure Indicates fuel pressure between the engine driven between the engine driven boost pump and the main fuel boost pump and the main fuel

i b l 10i b l 10 ±±1 PSI1 PSIpump is below 10 pump is below 10 ±±1 PSI1 PSI

87

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– FUEL TRANSFER FAILUREFUEL TRANSFER FAILURE

88

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– FUEL TRANSFER FAILUREFUEL TRANSFER FAILURE

Indicates fuel is the auxiliary Indicates fuel is the auxiliary tank, and fuel is not tank, and fuel is not transferring from the auxiliary transferring from the auxiliary t k t th ll t kt k t th ll t ktank to the nacelle tanktank to the nacelle tank

89

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– FUEL CROSSFEED SELECTEDFUEL CROSSFEED SELECTED

90

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– FUEL CROSSFEED SELECTEDFUEL CROSSFEED SELECTED

Indicates the fuel Indicates the fuel crossfeedcrossfeedswitch is in the switch is in the crossfeedcrossfeedposition (left or right); the position (left or right); the

i ti t d td tannunciatorannunciator does not prove does not prove the valve is openthe valve is open

91


Landing Gear SystemLanding Gear System

92

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– HYDRAULIC FLUID LOWHYDRAULIC FLUID LOW

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King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– HYDRAULIC FLUID LOWHYDRAULIC FLUID LOW

I di t h d li fl id l lI di t h d li fl id l l Indicates hydraulic fluid level Indicates hydraulic fluid level in power pack is below critical in power pack is below critical level on the following:level on the following:level on the following:level on the following: aircraft with Beech Kit P/N aircraft with Beech Kit P/N

101101--80188018--1;1;101101 80188018 1;1; BBBB--1158 and BB1158 and BB--1167;1167; BBBB--1193 and subsequent;1193 and subsequent;BBBB--1193 and subsequent;1193 and subsequent; BLBL--73 and subsequent73 and subsequent

94

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– LANDING OR TAXI LIGHT ONLANDING OR TAXI LIGHT ON

95

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– LANDING OR TAXI LIGHT ONLANDING OR TAXI LIGHT ON

Indicates the landing and/or Indicates the landing and/or taxi lights are ON with the gear taxi lights are ON with the gear retractedretractedretractedretracted

96

King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator -- LANDING GEAR IN TRANSITION OR UNSAFELANDING GEAR IN TRANSITION OR UNSAFE

97


Indicates one ore more of theIndicates one ore more of the

AnnunciatorAnnunciator -- LANDING GEAR IN TRANSITION OR UNSAFELANDING GEAR IN TRANSITION OR UNSAFE

Indicates one ore more of the Indicates one ore more of the following:following: landing gear in transitlanding gear in transitlanding gear in transitlanding gear in transit one or more gear not down and one or more gear not down and

lockedlockedt f ll t t dt f ll t t d one or more gear not fully retractedone or more gear not fully retracted

landing gear UP and one or both landing gear UP and one or both power levers below approximately power levers below approximately yy78% N78% N11

landing gear UP and flaps extended landing gear UP and flaps extended beyond APPROACH positionbeyond APPROACH position

98

beyond APPROACH position beyond APPROACH position (regardless of power lever position)(regardless of power lever position)

King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator -- LANDING GEAR DOWNLANDING GEAR DOWN

99

King Air BEKing Air BE--200/B200200/B200AnnunciatorAnnunciator -- LANDING GEAR DOWNLANDING GEAR DOWN

If all three lights are not on, If all three lights are not on, Left, right main gear, or nose Left, right main gear, or nose gear may not be down andgear may not be down andgear may not be down and gear may not be down and lockedlocked

100


Flight ControlsFlight Controls

101

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– AUTOPILOT DISCONNECTAUTOPILOT DISCONNECT

102

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– AUTOPILOT DISCONNECTAUTOPILOT DISCONNECT

Sperry Equipped Aircraft: Sperry Equipped Aircraft: Autopilot disengaged by other Autopilot disengaged by other than pilot’s AP/YD (control than pilot’s AP/YD (control

h l) di t it hh l) di t it hwheel) disconnect switchwheel) disconnect switch

103

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– AUTOPILOT TRIM FAILAUTOPILOT TRIM FAIL

104


Sperry Equipped Aircraft: Sperry Equipped Aircraft:

Annunciators Annunciators –– AUTOPILOT TRIM FAILAUTOPILOT TRIM FAIL

Indicates improper trim Indicates improper trim commands, trim runaway, or commands, trim runaway, or t i f il C t l h l t it i f il C t l h l t itrim failure. Control wheel trim trim failure. Control wheel trim switches activated with switches activated with autopilot engagedautopilot engagedautopilot engagedautopilot engaged

105

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ELECTRIC TRIM OFFELECTRIC TRIM OFF

106


Sperry Equipped Aircraft: Sperry Equipped Aircraft:

Annunciators Annunciators –– ELECTRIC TRIM OFFELECTRIC TRIM OFF

Electric elevator trim system is Electric elevator trim system is disarmeddisarmed

107


EnvironmentalEnvironmental

108

King Air BEKing Air BE--200/B200200/B200AnnunciatorsAnnunciators -- CABIN OR CARGO DOOR UNLOCKEDCABIN OR CARGO DOOR UNLOCKED

109

King Air BEKing Air BE--200/B200200/B200AnnunciatorsAnnunciators -- CABIN OR CARGO DOOR UNLOCKEDCABIN OR CARGO DOOR UNLOCKED

Indicates cabin Indicates cabin airstairairstair or cargo or cargo door is unlocked or opendoor is unlocked or open

110

King Air BEKing Air BE--200/B200200/B200AnnunciatorsAnnunciators -- CABIN ALTITUDE WARNINGCABIN ALTITUDE WARNING

111


Indicates cabin altitude is Indicates cabin altitude is

AnnunciatorsAnnunciators -- CABIN ALTITUDE WARNINGCABIN ALTITUDE WARNING

12,500 ft or higher12,500 ft or higher

112

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– PASSENGER OXYGEN DEPLOYEDPASSENGER OXYGEN DEPLOYED

113

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– PASSENGER OXYGEN DEPLOYEDPASSENGER OXYGEN DEPLOYED

Indicates passenger oxygen Indicates passenger oxygen masks deployed. If masks masks deployed. If masks automatically deploy and automatically deploy and

bi ltit d d d b lbi ltit d d d b lcabin altitudes descend below cabin altitudes descend below 12,500 ft, 12,500 ft, annunciatorannunciatorextinguishes If manuallyextinguishes If manuallyextinguishes. If manually extinguishes. If manually deployed, deployed, annunciatorsannunciators will will remain onremain on

114

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– ALT WARN ON AND PASS OXY OFFALT WARN ON AND PASS OXY OFF

115


ALT WARN ALT WARN annunciatorannunciator

Annunciator Annunciator –– ALT WARN ON AND PASS OXY OFFALT WARN ON AND PASS OXY OFF

illuminated; PASS OXY ON illuminated; PASS OXY ON annunciatorannunciator not illuminated. not illuminated. I di t th f il fI di t th f il fIndicates the failure of Indicates the failure of automatic passenger mask automatic passenger mask deploymentdeploymentdeploymentdeployment

116

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ASSOCIATED BLEED AIR OFFASSOCIATED BLEED AIR OFF

117

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ASSOCIATED BLEED AIR OFFASSOCIATED BLEED AIR OFF

Indicates the environmental Indicates the environmental bleed air valves are selected bleed air valves are selected closedclosed

118

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– BLEED AIR FAILUREBLEED AIR FAILURE

119


Indicates a possible rupture of Indicates a possible rupture of

Annunciators Annunciators –– BLEED AIR FAILUREBLEED AIR FAILURE

the bleed air line. Bleed air the bleed air line. Bleed air warning system is warning system is d i dd i ddepressurizeddepressurized

120

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– AIR CONDITION NAIR CONDITION N11 LOWLOW

121

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– AIR CONDITION NAIR CONDITION N11 LOWLOW

Indicates air conditioning Indicates air conditioning compressor clutch has compressor clutch has disengaged due to right disengaged due to right

i Ni N b l i t lb l i t lengine Nengine N11 below approximately below approximately 62%.62%.

122

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– ELECTRIC HEAT ONELECTRIC HEAT ON

123


Illumination indicates electric Illumination indicates electric

Annunciator Annunciator –– ELECTRIC HEAT ONELECTRIC HEAT ON

heat system operating. When heat system operating. When system selected to OFF, the system selected to OFF, the

i ti t t ti i ht ti i hannunciatorannunciator must extinguish must extinguish before blowers are switched to before blowers are switched to OFFOFFOFFOFF

124

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator –– DUCT OVERDUCT OVER--TEMPERATURETEMPERATURE

125


Indicates the environmental air Indicates the environmental air

Annunciator Annunciator –– DUCT OVERDUCT OVER--TEMPERATURETEMPERATURE

duct temperature exceeds duct temperature exceeds 149149°°C (300C (300°°F)F)

126


Ice and RainIce and Rain

127

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator ––BRAKE DEBRAKE DE--ICE ONICE ON

128

King Air BEKing Air BE--200/B200200/B200Annunciator Annunciator ––BRAKE DEBRAKE DE--ICE ONICE ON

Indicates the brake deice Indicates the brake deice switch is ONswitch is ONswitch is ONswitch is ON

129

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ASSOCIATED ICE VANE FAILASSOCIATED ICE VANE FAIL

130

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators –– ASSOCIATED ICE VANE FAILASSOCIATED ICE VANE FAIL

Engine antiEngine anti--ice vane position ice vane position does not agree with the does not agree with the position of the ice vane switchposition of the ice vane switch

131


MiscellaneousMiscellaneous

132

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- ENGINE ANTIENGINE ANTI--ICE/ICE VANE ONICE/ICE VANE ON

133

King Air BEKing Air BE--200/B200200/B200Annunciators Annunciators -- ENGINE ANTIENGINE ANTI--ICE/ICE VANE ONICE/ICE VANE ON

Indicates the associated Indicates the associated engine antiengine anti--ice / ice vane is ice / ice vane is on / extendedon / extended

134


Airspeeds andAirspeeds andAirspeeds and Airspeeds and LimitationsLimitationsLimitationsLimitations

135

King Air BEKing Air BE--200/B200200/B200Airspeeds and LimitationsAirspeeds and Limitations

Single engine best angle of climb (VSingle engine best angle of climb (VXSEXSE):):Single engine best angle of climb (VSingle engine best angle of climb (VXSEXSE):):

136


Answer:Answer:

115 KIAS115 KIAS

Answer:Answer:

137


Single engine best rate of climb (VSingle engine best rate of climb (V ):):Single engine best rate of climb (VSingle engine best rate of climb (VYSEYSE):):

138


Answer:Answer:

121 KIAS (blue line)121 KIAS (blue line)

Answer:Answer:

139


Single engine enSingle engine en--route climb:route climb:Single engine enSingle engine en route climb:route climb:

140


Answer:Answer:

121 KIAS (blue line)121 KIAS (blue line)

Answer:Answer:

141


Air minimum control speed (VAir minimum control speed (VMCAMCA):):p (p ( MCAMCA))

142


Answer:Answer:

86 KIAS (red line)86 KIAS (red line)

143


Emergency descent maximum speed:Emergency descent maximum speed:g y pg y p

144


Answer:Answer:

181 KIAS181 KIAS

145


Maximum range glide:Maximum range glide:Maximum range glide:Maximum range glide:

146


Answer:Answer:135 KIAS135 KIASAnswer:Answer:

147


Minimum airspeed in icing conditions:Minimum airspeed in icing conditions:u a speed c g co d t o su a speed c g co d t o s

148


Answer:Answer:140 KIAS140 KIAS

s es e

149


Turbulent air penetration:Turbulent air penetration:pp

150



151


Airborne maneuvering speed (VAirborne maneuvering speed (VAA):):g p (g p ( AA))

152



153


Ground maneuvering speed:Ground maneuvering speed:g pg p

154



155


Maximum landing gear extend Maximum landing gear extend g gg g(V(VLELE)/operate (V)/operate (VLOLO):):

156


Answer:Answer:

181 KIAS181 KIAS

157


Maximum gear retraction:Maximum gear retraction:gg

158



159


Maximum flaps 40% (VMaximum flaps 40% (VFEFE):):p (p ( FEFE))

160


Answer:Answer:200 KIAS (white triangle)200 KIAS (white triangle)

161


Flaps 100%:Flaps 100%:pp

162


Answer:Answer:

146 KIAS (top of white arc) BE146 KIAS (top of white arc) BE--200200S ( f )S ( f )157 KIAS (top of white arc) BE157 KIAS (top of white arc) BE--B200B200

163


Balked landing climb speed (VBalked landing climb speed (VXX) full flaps:) full flaps:g p (g p ( XX) p) p

164



165


Stall speed Stall speed –– flaps up (Vflaps up (VS1S1):):pp p p (p p ( S1S1))

166


Answer:Answer:

99 KIAS (top of wide white arc)99 KIAS (top of wide white arc)

167


Stall speed Stall speed –– flaps 40%:flaps 40%:pp pp

168


Answer:Answer:

85 KIAS85 KIAS

169


Stall speed Stall speed –– flaps 100% (Vflaps 100% (VSOSO):):pp p (p ( SOSO))

170


Answer:Answer:75 KIAS (bottom of white arc)75 KIAS (bottom of white arc)

171


Safe single engine speed:Safe single engine speed:g g pg g p

172


Answer:Answer:

104 KIAS104 KIAS

173


Maximum speed (VMaximum speed (VNENE/V/VMOMO):):p (p ( NENE MOMO))

174


Answer:Answer:

259 KIAS/.52 Mach or depending on serial no259 KIAS/.52 Mach or depending on serial no269 KIAS/.48 Mach (red line for V269 KIAS/.48 Mach (red line for VNENE/Barber /Barber

pole for Vpole for VMOMO))

175


Cruise climb profile:Cruise climb profile:pp

176


Answer:Answer:

To 10,000 ft. 160 KIASTo 10,000 ft. 160 KIASTo 20,000 ft. 140 KIASTo 20,000 ft. 140 KIASTo 25,000 ft. 130 KIASTo 25,000 ft. 130 KIASAbove 25,000 ft. 125 KIASAbove 25,000 ft. 125 KIAS

177


VVNENE/V/VMOMO::NENE MOMO

178


Answer:Answer:

BEBE--200 200 –– 269 KIAS/.48 Mach269 KIAS/.48 MachBEBE--B200 B200 –– 259 KIAS/.52 Mach259 KIAS/.52 Mach

179


Maximum effective windshield deMaximum effective windshield de--ice:ice:

180


Answer:Answer:

226 KIAS226 KIAS

181


Maximum operating pressure altitude:Maximum operating pressure altitude:p g pp g p

182


Answer:Answer:

BEBE--200 200 –– 31,000 ft. (some later SN 35,000 ft.) 31,000 ft. (some later SN 35,000 ft.) (see AFM)(see AFM)(see AFM)(see AFM)BEBE--B200 B200 –– 35,000 ft.35,000 ft.

183


Maximum PSID (pressurization):Maximum PSID (pressurization):(p )(p )

184


Answer:Answer:

BEBE--200 200 –– 6.1 PSID 6.1 PSID BEBE--B200 B200 –– 6.6 PSID6.6 PSID

185


Minimum battery volts for a battery start:Minimum battery volts for a battery start:y yy y

186


Answer:Answer:

23 Volts23 Volts

187


Minimum battery volts for plugging in a Minimum battery volts for plugging in a y p gg gy p gg gground power unit:ground power unit:

188


Answer:Answer:

20 Volts20 Volts

189


GPU limits:GPU limits:

190


Answer:Answer: BEBE--200200 28 to 28 2 Volts28 to 28 2 Volts 28 to 28.2 Volts28 to 28.2 Volts 400 Amps continuous400 Amps continuous

1 000 A1 000 A 1,000 Amps surge1,000 Amps surge BEBE--B200B200 28 to 28.4 Volts28 to 28.4 Volts 300 Amps continuous300 Amps continuous

191

1,000 Amps surge1,000 Amps surge


Generator limits:Generator limits:

192


Answer:Answer:

Up to 31,000 ft. Up to 31,000 ft. –– 100%100%Above 31,000 ft. Above 31,000 ft. –– 88%88%On ground On ground –– 85%85%gg

193


Starter limits:Starter limits:Starter limits:Starter limits:

194


Answer:Answer:

40 sec. on/60 sec. off40 sec. on/60 sec. off

Answer:Answer:

40 sec. on/60 sec. off40 sec. on/60 sec. off40 sec. on/30 min. off 40 sec. on/30 min. off Optional 300 Amps Lear Optional 300 Amps Lear SieglerSiegler generator generator

has different limits. See AFM.has different limits. See AFM.

195


OAT limits:OAT limits:

196


Answer:Answer:

Sea level to 25,000 ft. Sea level to 25,000 ft. –– ISA + 37ISA + 37°°CCAbove 25,000 ft. Above 25,000 ft. –– ISA + 31ISA + 31°°CC

197


Towing limits:Towing limits:gg

198


Answer:Answer:

Do not tow with rudder gust lock installedDo not tow with rudder gust lock installedDo not tow with deflated strutDo not tow with deflated strutDo not exceed turn limit set by crush blockDo not exceed turn limit set by crush blockyy

199


Maximum ramp weight:Maximum ramp weight:p gp g

200


Answer:Answer:12,590 lbs12,590 lbs

201


Maximum takeoff weight:Maximum takeoff weight:gg

202


Answer:Answer:

12,000 lbs12,000 lbs

203


Maximum zero fuel weight:Maximum zero fuel weight:gg

204


Answer:Answer:

BEBE--200 200 –– 10,400 lbs10,400 lbsBEBE--B200 B200 –– 11,000 lbs11,000 lbs

205


Maximum landing weight:Maximum landing weight:g gg g

206


Answer:Answer:

12,500 lbs12,500 lbs

207


Aviation gasoline limits:Aviation gasoline limits:gg

208


Answer:Answer:

150 hours/engine overhaul period150 hours/engine overhaul period31,000 ft maximum altitude31,000 ft maximum altitude20,000 ft maximum without 20,000 ft maximum without crossfeedcrossfeed or if or if

electric boost pump electric boost pump MEL’dMEL’d

209


Aux fueling limits (order of fueling):Aux fueling limits (order of fueling):g ( g)g ( g)

210


Answer:Answer:

Do not put any fuel in the Aux tanks unless Do not put any fuel in the Aux tanks unless the main tanks are fullthe main tanks are fullthe main tanks are fullthe main tanks are full

211


When is When is crossfeedcrossfeed permitted?permitted?pp

212


Answer:Answer:

Single engine operations onlySingle engine operations only

213


Minimum fuel quantity for takeoff:Minimum fuel quantity for takeoff:q yq y

214


Answer:Answer:

265 lbs or top of yellow arc265 lbs or top of yellow arc

215


Maximum fuel imbalance:Maximum fuel imbalance:

216


Answer:Answer:

1,000 lbs1,000 lbs

217


How long can an engine be operated with the How long can an engine be operated with the g g pg g pL/R FUEL PRESS annunciator on?L/R FUEL PRESS annunciator on?

218


Answer:Answer:

10 hours/high pressure fuel pump 10 hours/high pressure fuel pump overhaul periodoverhaul periodoverhaul periodoverhaul period

219


Maximum brake deMaximum brake de--ice temperature:ice temperature:pp

220


Answer:Answer:

1515°°CC

221


Maximum brake deMaximum brake de--ice time ice time (landing gear retracted):(landing gear retracted):

222


Answer:Answer:

10 min.10 min.

223


Minimum deMinimum de--icing boot operating temperature:icing boot operating temperature:g p g pg p g p

224


Answer:Answer:

--4040°°C or C or --4040°°FF

225


Maximum engine antiMaximum engine anti--ice temperature:ice temperature:gg pp

226


Answer:Answer:

1515°°C (inC (in--flight)flight)

227


When must the engine antiWhen must the engine anti--ice be on?ice be on?gg

228


Answer:Answer:

On ground for FOD protectionOn ground for FOD protection InIn--flight:flight: Below +5Below +5°°C and flight free of visible C and flight free of visible

moisture cannot be assuredmoisture cannot be assured

ENG ANTI-ICE L or R

229


What are the gear cycle limits?What are the gear cycle limits?g yg y

230


Answer:Answer:

Mechanical gear Mechanical gear –– no limitno limitHydraulic gear Hydraulic gear –– 1 cycle each 5 minutes with a 1 cycle each 5 minutes with a

15 minute 15 minute cooldowncooldown after the 6after the 6thth cycle cycle

231


Are there any operational restrictions on the Are there any operational restrictions on the y py puse of brake deuse of brake de--ice?ice?

232


Answer:Answer:

YesYes Brake deBrake de--ice cannot be operated more than ice cannot be operated more than

10 min after gear retraction 10 min after gear retraction C t if OAT i b 15C t if OAT i b 15°°CC Cannot use if OAT is above 15Cannot use if OAT is above 15°°CC If also using the deIf also using the de--ice boots, the min Nice boots, the min N1 1 is 85%is 85% Both sources of bleed air must be operatingBoth sources of bleed air must be operating Rudder boost may not functionRudder boost may not function

233

yy


Maximum continuous ITT:Maximum continuous ITT:

234


Answer:Answer:

PT6APT6A--41 is 75041 is 750°°C (solid red line)C (solid red line)PT6APT6A--42 is 80042 is 800°°C (solid red line)C (solid red line)

235


Maximum ITT for start:Maximum ITT for start:

236


Answer:Answer:

1,0001,000°°C for maximum 5 secondsC for maximum 5 seconds

237


General OverviewGeneral Overview

238


What is the wing span?What is the wing span?


What is the wing span?What is the wing span?

239


Answer:Answer:


54 ft. 6 inches.54 ft. 6 inches.Answer:Answer:

240


How tall is a King Air?How tall is a King Air?


How tall is a King Air?How tall is a King Air?

241


Answer:Answer:


15 ft. to top of rudder15 ft. to top of rudder

Answer:Answer:

242


Air stair door limits:Air stair door limits:


Air stair door limits:Air stair door limits:

243


Answer:Answer:


One person on the air stair at any timeOne person on the air stair at any time

Answer:Answer:

300 lbs weight limit (military C12 only)300 lbs weight limit (military C12 only)

244


Occupancy limits:Occupancy limits:


Occupancy limits:Occupancy limits:

245


Answer:Answer:


Part 91 Part 91 –– 15 (including crew)15 (including crew)

Answer:Answer:

Part 135 Part 135 –– 9 Passengers (plus crew)9 Passengers (plus crew)

246


Maneuver category:Maneuver category:


Maneuver category:Maneuver category:

247


Answer:Answer:


NORMAL NORMAL –– All aerobatic maneuvers All aerobatic maneuvers

Answer:Answer:

including spins are prohibitedincluding spins are prohibited

248


Maximum demonstrated crosswind component:Maximum demonstrated crosswind component:


Maximum demonstrated crosswind component:Maximum demonstrated crosswind component:

249


Answer:Answer:


25 25 KtsKts

Answer:Answer:

250


Maximum tailwind component (takeoff/landing):Maximum tailwind component (takeoff/landing):


Maximum tailwind component (takeoff/landing):Maximum tailwind component (takeoff/landing):

251


Answer:Answer:


10 10 KtsKts

Answer:Answer:

252



253


What is the maximum prop RPM under normalWhat is the maximum prop RPM under normal


What is the maximum prop RPM under normal What is the maximum prop RPM under normal conditions?conditions?

254


Answer:Answer:


2,000 RPM (redline)2,000 RPM (redline)

Answer:Answer:

255


What does it mean if the propeller is notWhat does it mean if the propeller is not


What does it mean if the propeller is not What does it mean if the propeller is not controllable and is at 2,080 RPM?controllable and is at 2,080 RPM?

256


Answer:Answer:Engine and PropellerEngine and Propeller

Primary governor has failedPrimary governor has failedF l t i h l f il dF l t i h l f il dFuel topping governor has also failedFuel topping governor has also failedReverse cannot be used as engine speed Reverse cannot be used as engine speed

ill t b t ll bl ith i /f lill t b t ll bl ith i /f lwill not be controllable with primary/fuel will not be controllable with primary/fuel topping governor failuretopping governor failure

257


What conditions have to be met forWhat conditions have to be met for autofeatherautofeather toto


What conditions have to be met for What conditions have to be met for autofeatherautofeather to to function?function?

258


Answer:Answer:Engine and PropellerEngine and Propeller

Switch must be in “ARM” positionSwitch must be in “ARM” positionP l t b b th 90% iP l t b b th 90% iPower levers must be above the 90% micro Power levers must be above the 90% micro switchesswitchesB th i t b tiB th i t b tiBoth engines must be operatingBoth engines must be operating

AUTOFEATHER L or R

259


Is it possible for the second engine toIs it possible for the second engine to autofeatherautofeather??


Is it possible for the second engine to Is it possible for the second engine to autofeatherautofeather??

260


Answer:Answer:


No:No:

Answer:Answer:

The first engine to The first engine to autofeatherautofeather will will remove power from the second engine remove power from the second engine p gp gautofeatherautofeather circuit circuit

261


What should the pilot do if theWhat should the pilot do if the autofeatherautofeather doesdoes


What should the pilot do if the What should the pilot do if the autofeatherautofeather does does not feather the propeller?not feather the propeller?

262


Answer:Answer:


Feather the propeller manuallyFeather the propeller manually

Answer:Answer:

263


Should the pilot feather the second engine in theShould the pilot feather the second engine in the


Should the pilot feather the second engine in the Should the pilot feather the second engine in the event of a failure?event of a failure?

264


Answer:Answer:


Only if a restart is not possibleOnly if a restart is not possible

Answer:Answer:

265


Should the propellerShould the propeller syncrophasersyncrophaser be on duringbe on during


Should the propeller Should the propeller syncrophasersyncrophaser be on during be on during takeoff?takeoff?

266


Answer:Answer:


Type 1 Type 1 –– No, it should be OFFNo, it should be OFF

Answer:Answer:

If left on, the PROP SYNC ON If left on, the PROP SYNC ON annunciatorannunciatorwill illuminatewill illuminate

Type 2 Type 2 –– It does not matterIt does not matter

PROP SYNC ON

267


What RPM should be avoided withWhat RPM should be avoided with


What RPM should be avoided with What RPM should be avoided with 33--bladed props in the approach phase?bladed props in the approach phase?

268


Answer:Answer:


1,750 to 1,850 RPM1,750 to 1,850 RPM

Answer:Answer:

Should be avoided as it may cause ILS Should be avoided as it may cause ILS signal interference signal interference

269


What type of engine is installed on theWhat type of engine is installed on the


What type of engine is installed on the What type of engine is installed on the BEBE--200/BE200/BE--B200:B200:

270


Answer:Answer:


BEBE--200 200 –– PT6APT6A--4141

Answer:Answer:

BEBE--B200 B200 –– PT6APT6A--4242

271


How much horsepower does the engine developHow much horsepower does the engine develop


How much horsepower does the engine develop How much horsepower does the engine develop under ideal conditions?under ideal conditions?

272


Answer:Answer:


850 shaft horsepower850 shaft horsepower

Answer:Answer:

273


On a PTOn a PT--6 what6 what doesdoes free turbine (split shaft)free turbine (split shaft)


On a PTOn a PT--6, what 6, what doesdoes free turbine (split shaft) free turbine (split shaft) mean?mean?

274


Answer:Answer:


The NThe N11 and Nand N22 shafts are not physically shafts are not physically t dt d

Answer:Answer:

connectedconnectedThe engine can be started or idled with the The engine can be started or idled with the

propeller feathered (maximum of 1,100 lbs propeller feathered (maximum of 1,100 lbs torque)torque)

275


Are there potential problems with a featheredAre there potential problems with a feathered


Are there potential problems with a feathered Are there potential problems with a feathered propeller on the ground for extended periods?propeller on the ground for extended periods?

276


Answer:Answer:


FOD on contaminated surfaces entering the FOD on contaminated surfaces entering the i di th ll bl di di th ll bl d

Answer:Answer:

engine, or eroding the propeller bladesengine, or eroding the propeller bladesHigherHigher--thanthan--normal oil temperaturesnormal oil temperatures In certain wind conditions, damage may In certain wind conditions, damage may

occur to the deoccur to the de--ice boots, or side windows ice boots, or side windows due to excessive heatdue to excessive heat Very low quartering tail wind, and not a Very low quartering tail wind, and not a

277

common eventcommon event

King Air BEKing Air BE--200/B200200/B200Engine and PropellerEngine and Propeller

What does “reverse flow” mean on this engine?What does “reverse flow” mean on this engine?

278


The intake air enters the engine at the rearThe intake air enters the engine at the rear

Answer:Answer:

The intake air enters the engine at the rear, The intake air enters the engine at the rear, and the exhaust air exits at the front of the and the exhaust air exits at the front of the engineengineThe airflow reverses at the combustion The airflow reverses at the combustion

chamber in order to shorten the overall chamber in order to shorten the overall length of the enginelength of the engine

279


What is the function of the P2 5 (low and highWhat is the function of the P2 5 (low and high


What is the function of the P2.5 (low and high What is the function of the P2.5 (low and high pressure) bleed valves?pressure) bleed valves?

280


Answer:Answer:


To automatically open and close in order to To automatically open and close in order to

Answer:Answer:

vent excess pressure at power settingsvent excess pressure at power settings This prevents compressor stallsThis prevents compressor stalls

281


What items are driven by the oil pump shaft?What items are driven by the oil pump shaft?

282


Oil pumpOil pump

Answer:Answer:

Oil pumpOil pumpTwo dualTwo dual--element oil scavenge pumpselement oil scavenge pumpsThe low pressure, engineThe low pressure, engine--driven fuel pumpdriven fuel pump

283


How is the fuel deHow is the fuel de--iced prior to the fuel control unit?iced prior to the fuel control unit?

284


Hot oil is used to warm the fuel in the oilHot oil is used to warm the fuel in the oil--toto--

Answer:Answer:

Hot oil is used to warm the fuel in the oilHot oil is used to warm the fuel in the oil totofuel heat exchangerfuel heat exchanger

285


When is the most accurate time to check the oil level?When is the most accurate time to check the oil level?

286


Within 15 minutes after shutdownWithin 15 minutes after shutdown

Answer:Answer:

Within 15 minutes after shutdownWithin 15 minutes after shutdown

287


If the oil dipstick comes loose inIf the oil dipstick comes loose in--flight what willflight what will


If the oil dipstick comes loose inIf the oil dipstick comes loose in--flight, what will flight, what will happen?happen?

288


Answer:Answer:


All of the oil will be vented out of the engineAll of the oil will be vented out of the engine

Answer:Answer:

289


Does the engine have flameDoes the engine have flame--out protection?out protection?

290


Yes:Yes:

Answer:Answer:

Yes:Yes: AutoAuto--ignition comes on any time the ignition comes on any time the

torque drops below 400 lbs (if armed)torque drops below 400 lbs (if armed)torque drops below 400 lbs (if armed)torque drops below 400 lbs (if armed)

IGNITION ON L or R

291


Is the torque limited in the event of power beingIs the torque limited in the event of power being


Is the torque limited in the event of power being Is the torque limited in the event of power being set too high?set too high?

292


Answer:Answer:


Yes:Yes:

Answer:Answer:

The torque limiter will vent air from the FCU The torque limiter will vent air from the FCU resulting in power reductionresulting in power reduction

Torque limiterTorque limiter is Calibrated at 2,430 lbs torqueis Calibrated at 2,430 lbs torqueEngine surging is likelyEngine surging is likelyg g g yg g g y

293


What should the pilot do if ITT limits areWhat should the pilot do if ITT limits are


What should the pilot do if ITT limits are What should the pilot do if ITT limits are exceeded during start?exceeded during start?

294


Answer:Answer:


Condition lever Condition lever –– CUTTOFFCUTTOFF

Answer:Answer:

Starter Starter –– STARTER ONLYSTARTER ONLYObserve starter limitsObserve starter limitsObserve starter limitsObserve starter limits

295


What should the pilot do if there is no ITT riseWhat should the pilot do if there is no ITT rise


What should the pilot do if there is no ITT rise What should the pilot do if there is no ITT rise within 10 seconds after adding fuel during start?within 10 seconds after adding fuel during start?

296


Answer:Answer:


Condition lever Condition lever –– CUTTOFFCUTTOFF

Answer:Answer:

Starter Starter –– OFFOFF Wait 60 seconds (minimum) for unburnedWait 60 seconds (minimum) for unburnedWait 60 seconds (minimum) for unburned Wait 60 seconds (minimum) for unburned

fuel to drainfuel to drain

StarterStarter –– STARTER ONLYSTARTER ONLYStarter Starter STARTER ONLYSTARTER ONLY Observe starter limitsObserve starter limits

297


Pneumatic and PressurizationPneumatic and Pressurization

298

King Air BEKing Air BE--200/B200200/B200Pneumatic and PressurizationPneumatic and Pressurization

What is the source of pressurization air?What is the source of pressurization air?

299


PP33 air (bleed air) from each engine using aair (bleed air) from each engine using a

Answer:Answer:

PP33 air (bleed air) from each engine using a air (bleed air) from each engine using a flow pack on each sideflow pack on each side

300


How does a flow pack cool PHow does a flow pack cool P33 air?air?

301


It uses expansionIt uses expansionAnswer:Answer:

pp It uses mixing of ambient airIt uses mixing of ambient airThe flow packs do not function on theThe flow packs do not function on theThe flow packs do not function on the The flow packs do not function on the

groundground

302


How is vacuum air generated?How is vacuum air generated?

303


Instrument air is passed through an injectorInstrument air is passed through an injector

Answer:Answer:

Instrument air is passed through an injector Instrument air is passed through an injector ((VenturiVenturi))

304


What is vacuum air used for?What is vacuum air used for?

305


Deflating and holding the boots to the wings Deflating and holding the boots to the wings

Answer:Answer:

g g gg g gwhile not inflatedwhile not inflatedPowering the copilot instrumentsPowering the copilot instrumentsPowering the copilot instrumentsPowering the copilot instruments Attitude indicatorAttitude indicator T d liT d li Turn and slipTurn and slip

Powering the outflow valves to control Powering the outflow valves to control i tii ti

306

pressurizationpressurization


What powers the flight hour meter?What powers the flight hour meter?

307


28 VDC power, controlled by a pressure28 VDC power, controlled by a pressure

Answer:Answer:

28 VDC power, controlled by a pressure 28 VDC power, controlled by a pressure switch measuring instrument airswitch measuring instrument air

308


Which engine must be running for the Freon ACWhich engine must be running for the Freon AC


Which engine must be running for the Freon AC Which engine must be running for the Freon AC system to operate?system to operate?

309


Answer:Answer:


Right engineRight engine

Answer:Answer:

310


What will happen if the aft blower is left on inWhat will happen if the aft blower is left on in--flight?flight?

311


The rear heater vents will only be used forThe rear heater vents will only be used for

Answer:Answer:

The rear heater vents will only be used for The rear heater vents will only be used for AC coolingAC cooling

312


What causes the BLEED AIR FAILWhat causes the BLEED AIR FAIL annunciatorannunciator toto


What causes the BLEED AIR FAIL What causes the BLEED AIR FAIL annunciatorannunciator to to illuminate?illuminate?

313


Answer:Answer:


If a bleed air leak melts the If a bleed air leak melts the PolyflowPolyflow tubing, tubing, th d i d t t dth d i d t t d

Answer:Answer:

the pressure drop is detectedthe pressure drop is detected

BL AIR FAIL L or R

314


If the bleed air switch is set to “INSTR&ENVIRIf the bleed air switch is set to “INSTR&ENVIR


If the bleed air switch is set to INSTR&ENVIR If the bleed air switch is set to INSTR&ENVIR OFF”, will the rudder boost function?OFF”, will the rudder boost function?

315


Answer:Answer:


NoNo

Answer:Answer:

BL AIR OFF L or RBL AIR OFF L or R

316


What is the function of the outflow valve?What is the function of the outflow valve?

317


To control pressurization at the command ofTo control pressurization at the command of

Answer:Answer:

To control pressurization at the command of To control pressurization at the command of the pressurization controllerthe pressurization controller

318


What is the function of the safety valve?What is the function of the safety valve?

319


To open if the pressure exceeds maximum PSIDTo open if the pressure exceeds maximum PSID

Answer:Answer:

To open if the pressure exceeds maximum PSIDTo open if the pressure exceeds maximum PSIDTo open if DUMP is selectedTo open if DUMP is selectedTo open on the ground To open on the ground

(weight on wheels switch)(weight on wheels switch)

320


How should the pressurization be set prior toHow should the pressurization be set prior to


How should the pressurization be set prior to How should the pressurization be set prior to landing?landing?

321


Answer:Answer:


Such that there is 0 PSID upon landingSuch that there is 0 PSID upon landing

Answer:Answer:

500 ft. above field pressure altitude500 ft. above field pressure altitudeUse chart to determine proper setting forUse chart to determine proper setting forUse chart to determine proper setting for Use chart to determine proper setting for

current field altimeter setting current field altimeter setting

322


Why is the pressurization set forWhy is the pressurization set for


Why is the pressurization set for Why is the pressurization set for 1,000 ft above cruise altitude?1,000 ft above cruise altitude?

323


Answer:Answer:


To ensure that the max PSID is not reachedTo ensure that the max PSID is not reached

Answer:Answer:

324


At what cabin altitude does the ALT WARNAt what cabin altitude does the ALT WARN


At what cabin altitude does the ALT WARN At what cabin altitude does the ALT WARN annunciatorannunciator illuminate?illuminate?

325


Answer:Answer:


12,500 ft.12,500 ft.

Answer:Answer:

ALT WARNALT WARN

326


At what cabin altitude do the passenger masksAt what cabin altitude do the passenger masks


At what cabin altitude do the passenger masks At what cabin altitude do the passenger masks automatically drop?automatically drop?

327


Answer:Answer:

12,000 ft.12,000 ft.

Answer:Answer:

328


If the cabin is above 12 000 ft and the passengerIf the cabin is above 12 000 ft and the passenger


If the cabin is above 12,000 ft. and the passengerIf the cabin is above 12,000 ft. and the passengermasks have not dropped, what can you do?masks have not dropped, what can you do?

329


Answer:Answer:


Pull the manual drop handlePull the manual drop handle

Answer:Answer:

330


If the OIf the O22 system is not armed, is oxygen available?system is not armed, is oxygen available?

331


NoNo

Answer:Answer:

NoNo Oxygen must be armed for the entire flight in Oxygen must be armed for the entire flight in

order to prevent the arming mechanism fromorder to prevent the arming mechanism fromorder to prevent the arming mechanism from order to prevent the arming mechanism from freezing in the OFF positionfreezing in the OFF position

332


If the cabin is below 12,000 ft. and the passenger If the cabin is below 12,000 ft. and the passenger Pneumatic and PressurizationPneumatic and Pressurization

masks have dropped, how can the Omasks have dropped, how can the O22 flow be flow be stopped?stopped?

333


Answer:Answer:Pneumatic and PressurizationPneumatic and Pressurization

Push the manual drop handle back inPush the manual drop handle back inT dT d ti t th B t i it h llti t th B t i it h llTo deTo de--activate the Barometric switch, pull activate the Barometric switch, pull the OXY CONTROL breakerthe OXY CONTROL breaker

334



335


What type of battery is used?What type of battery is used?


What type of battery is used? What type of battery is used? Where is it located?Where is it located?

336


Answer:Answer:


24 Volt 24 Volt NiCdNiCd (original equipment on older (original equipment on older

Answer:Answer:

aircraft) or 24 Volt lead acid battery (most aircraft) or 24 Volt lead acid battery (most aircraft now have the lead acid battery)aircraft now have the lead acid battery)Located in the right wing center section Located in the right wing center section

forward of the sparforward of the spar

337


Why is it important to know if your aircraft hasWhy is it important to know if your aircraft has


Why is it important to know if your aircraft has Why is it important to know if your aircraft has the the NiCdNiCd battery?battery?

338


Answer:Answer:


They are subject to thermal runaway inThey are subject to thermal runaway in--flightflight

Answer:Answer:

They have periodic maintenance They have periodic maintenance requirements for deep cycle checks that do requirements for deep cycle checks that do q p yq p ynot apply to lead acid typesnot apply to lead acid types

339


If the battery is below 23 Volts how can theIf the battery is below 23 Volts how can the


If the battery is below 23 Volts, how can the If the battery is below 23 Volts, how can the engine be started?engine be started?

340


Answer:Answer:


Ground power unit onlyGround power unit only

Answer:Answer:

341


If the battery is below 20 volts how can theIf the battery is below 20 volts how can the


If the battery is below 20 volts, how can the If the battery is below 20 volts, how can the engine be started?engine be started?

342


Answer:Answer:


It cannot be startedIt cannot be started

Answer:Answer:

The battery must be removed from the The battery must be removed from the aircraft and recharged or replacedaircraft and recharged or replacedgg

343


If the battery is below 20 volts will the GPUIf the battery is below 20 volts will the GPU


If the battery is below 20 volts, will the GPU If the battery is below 20 volts, will the GPU recharge the battery?recharge the battery?

344


Answer:Answer:


Yes, but in a harmful wayYes, but in a harmful way

Answer:Answer:

The wiring will be overloadedThe wiring will be overloaded The start contactor may weldThe start contactor may weldThe start contactor may weldThe start contactor may weld The battery will recharge at the max The battery will recharge at the max

amperage of the GPU and potentially be amperage of the GPU and potentially be p g p yp g p ydamaged or overheatdamaged or overheat

This is a violation of a limitationThis is a violation of a limitation

345

King Air BEKing Air BE--200/B200200/B200Electrical SystemElectrical System

Can the GPU connect if the battery switch is off?Can the GPU connect if the battery switch is off?

346


No:No:

Answer:Answer:

No:No: The GPU switch and the battery switch are The GPU switch and the battery switch are

the samethe samethe samethe same

The battery switch should be ONThe battery switch should be ON

347


What causes the “EXT PWR” to illuminate?What causes the “EXT PWR” to illuminate?

348


A GPU plug is connectedA GPU plug is connected

Answer:Answer:

A GPU plug is connectedA GPU plug is connected It is detected by a micro switchIt is detected by a micro switch

EXT PWREXT PWR

349


How do you detect a failed isolation limiter?How do you detect a failed isolation limiter?

350


With less than t o generators online theWith less than t o generators online the

Answer:Answer:

With less than two generators online, the With less than two generators online, the voltage on both sides should be equalvoltage on both sides should be equal If t i l ti li it h f il dIf t i l ti li it h f il d If not, an isolation limiter has failedIf not, an isolation limiter has failed

351


May the dualMay the dual fed buss 50 Amps breakers be resetfed buss 50 Amps breakers be reset


May the dualMay the dual--fed buss 50 Amps breakers be resetfed buss 50 Amps breakers be resetinin--flight?flight?

352


Answer:Answer:


NoNo

Answer:Answer:

353


What causes the battery chargeWhat causes the battery charge annunciatorannunciator toto


What causes the battery charge What causes the battery charge annunciatorannunciator to to illuminate?illuminate?

354


Answer:Answer:


A battery charge rate of at least 7 Amps for A battery charge rate of at least 7 Amps for 6 seconds6 seconds

Answer:Answer:

6 seconds6 seconds

BATTERY CHARGE

355


Fire ProtectionFire Protection

356


How does the older infrared system work?How does the older infrared system work?

357


Answer:Answer:


Three photoconductive cells for each engineThree photoconductive cells for each engineD t t hi hD t t hi h thth l h t (i f d)l h t (i f d)

Answer:Answer:

Detects higherDetects higher--thanthan--normal heat (infrared) normal heat (infrared) source and triggers L/R ENGINE FIRE source and triggers L/R ENGINE FIRE annunciationannunciationannunciationannunciationProne to false triggers due to stray light and Prone to false triggers due to stray light and

rain in the engine cowlrain in the engine cowlrain in the engine cowlrain in the engine cowl

ENG FIRE L or R

358

ENG FIRE L or R


How does the fire detection system with theHow does the fire detection system with the


How does the fire detection system with the How does the fire detection system with the temperature detecting loop work?temperature detecting loop work?

359


Answer:Answer:


Coaxial tube with dissimilar gasses detects Coaxial tube with dissimilar gasses detects ffff

Answer:Answer:

heat using differing expansion ratesheat using differing expansion ratesSystem is very reliableSystem is very reliable Detection could be a result of fire or possibly Detection could be a result of fire or possibly

a bleed air leaka bleed air leak SN BB 1444 and afterSN BB 1444 and after

360


Where would you find the optional fireWhere would you find the optional fire


Where would you find the optional fire Where would you find the optional fire extinguisher bottle?extinguisher bottle?

361


Answer:Answer:


Inside of the main landing gear wellInside of the main landing gear well

Answer:Answer:

362


Why would you need to check the fire bottleWhy would you need to check the fire bottle


Why would you need to check the fire bottle Why would you need to check the fire bottle during preflight?during preflight?

363


Answer:Answer:


To verify that the charge pressure has not To verify that the charge pressure has not l k dl k d

Answer:Answer:

leakedleaked

364


After using the first fire bottle can the otherAfter using the first fire bottle can the other


After using the first fire bottle, can the other After using the first fire bottle, can the other bottle be used to fight the fire?bottle be used to fight the fire?

365


Answer:Answer:


No:No:

Answer:Answer:

The fire bottle cannot cross over to the other The fire bottle cannot cross over to the other side side

366


What does the “FIRE EXT” test do?What does the “FIRE EXT” test do?

367


It tests the electrical capability of the systemIt tests the electrical capability of the system

Answer:Answer:

It tests the electrical capability of the system It tests the electrical capability of the system to fireto fire

368


If the battery switch is OFF and the FIREIf the battery switch is OFF and the FIRE


If the battery switch is OFF, and the FIRE If the battery switch is OFF, and the FIRE EXTINGUISHER switch is pushed, will it fire?EXTINGUISHER switch is pushed, will it fire?

369


Answer:Answer:


Yes:Yes:

Answer:Answer:

The fire extinguisher is on the hot battery The fire extinguisher is on the hot battery bus, and will fire any timebus, and will fire any time

370


How many hand fire extinguishers should beHow many hand fire extinguishers should be


How many hand fire extinguishers should be How many hand fire extinguishers should be inside the aircraft?inside the aircraft?

371


Answer:Answer:


Two:Two:

Answer:Answer:

One in the cockpit, under the copilot seatOne in the cockpit, under the copilot seat One in the back, near the air stair doorOne in the back, near the air stair doorOne in the back, near the air stair doorOne in the back, near the air stair door

372


How are the portable fire extinguishers How are the portable fire extinguishers preflightedpreflighted??

373


Check pressure inside of the green arcCheck pressure inside of the green arc

Answer:Answer:

Check pressure inside of the green arcCheck pressure inside of the green arcCheck expiration date on tagCheck expiration date on tag

374



375


Procedure for L/R ENG ANTIProcedure for L/R ENG ANTI--ICE FAILICE FAIL


Procedure for L/R ENG ANTIProcedure for L/R ENG ANTI--ICE FAILICE FAIL(electric standby system):(electric standby system):

376


Answer:Answer:


Use standby actuator motor to extend and Use standby actuator motor to extend and t tt t

Answer:Answer:

retractretract

ENG ICE FAIL L or R

377

King Air BEKing Air BE--200/B200200/B200Ice and RainIce and Rain

What powers the deWhat powers the de--ice boots?ice boots?

378


Pneumatic air (18 PSI) inflates and suctionPneumatic air (18 PSI) inflates and suction

Answer:Answer:

Pneumatic air (18 PSI) inflates and suction Pneumatic air (18 PSI) inflates and suction air deflates and holds them to the surfaceair deflates and holds them to the surface

379


What does “SINGLE CYCLE” do?What does “SINGLE CYCLE” do?

380


Inflates the wing boots for 6 seconds,Inflates the wing boots for 6 seconds,

Answer:Answer:

Inflates the wing boots for 6 seconds, Inflates the wing boots for 6 seconds, followed by 4 seconds to the wingfollowed by 4 seconds to the wing

381


Referring to the deReferring to the de--ice boots what does theice boots what does the


Referring to the deReferring to the de--ice boots, what does the ice boots, what does the “MANUAL” switch position do?“MANUAL” switch position do?

382


Answer:Answer:


Inflates all boots for the period of time that Inflates all boots for the period of time that th it h i h ldth it h i h ld

Answer:Answer:

the switch is heldthe switch is held

383


When should the deWhen should the de--ice boots be cycled?ice boots be cycled?

384


After ½ to 1 inch of iceAfter ½ to 1 inch of ice

Answer:Answer:

After ½ to 1 inch of iceAfter ½ to 1 inch of iceNever during takeoffNever during takeoff

385


How is the engine inlet heated?How is the engine inlet heated?

386


Engine exhaust is directed through theEngine exhaust is directed through the

Answer:Answer:

Engine exhaust is directed through the Engine exhaust is directed through the engine inlet ringengine inlet ring

387


How do the ice vanes (engine antiHow do the ice vanes (engine anti--ice) work?ice) work?

388


When the system is on, particulate matterWhen the system is on, particulate matter

Answer:Answer:

When the system is on, particulate matter When the system is on, particulate matter (FOD or ice) is vented out to the bottom of (FOD or ice) is vented out to the bottom of the engine cowling, while the clean air is the engine cowling, while the clean air is d i t th id i t th idrawn up into the engine.drawn up into the engine.

389


When must the engine antiWhen must the engine anti--ice be on?ice be on?

390


On ground for FOD protectionOn ground for FOD protection

Answer:Answer:

g pg p Oil temps may be higher than normalOil temps may be higher than normal

InIn flightflight InIn--flightflight Below +5Below +5°°C and flight free of visible moisture C and flight free of visible moisture

cannot be assuredcannot be assuredcannot be assuredcannot be assured

391


Are there any limitations on propeller heat?Are there any limitations on propeller heat?

392


Yes:Yes:Answer:Answer:

The propeller must be turning in order to The propeller must be turning in order to prevent damageprevent damage

393


When the prop heat is set to “AUTO”, what is the cycle?When the prop heat is set to “AUTO”, what is the cycle?

394


ThreeThree--blade propsblade props

Answer:Answer:

FourFour--blade propsblade propsThreeThree blade props blade props (with dual boots)(with dual boots) 44--30 sec timer sequence30 sec timer sequence

FourFour blade props blade props (single boot system)(single boot system) 90 sec sequentially on 90 sec sequentially on

each propeach prop Outer, inner, Outer, inner, –– other side other side ––

outer, innerouter, inner 14 to 18 Amps for each14 to 18 Amps for each

each propeach prop 18 to 24 Amps for each 18 to 24 Amps for each

segmentsegment14 to 18 Amps for each 14 to 18 Amps for each segmentsegment

395


When the prop heat is set to “MANUAL” what isWhen the prop heat is set to “MANUAL” what is

IceIce and Rainand Rain

When the prop heat is set to MANUAL , what is When the prop heat is set to MANUAL , what is the cycle?the cycle?

396


Answer:Answer:

IceIce and Rainand Rain

ThreeThree--blade props (with blade props (with d l b t )d l b t )

Answer:Answer:

FourFour--blade props (single blade props (single b t t )b t t )dual boots)dual boots)

No timer sequenceNo timer sequence Manual inner heats bothManual inner heats both

boot system)boot system) No timer sequence, both No timer sequence, both

props heated while switch props heated while switch Manual inner heats both Manual inner heats both prop inner boots while prop inner boots while switch is heldswitch is held

Manual outer heats bothManual outer heats both

heldheld

Manual outer heats both Manual outer heats both outer while switch heldouter while switch held

397


How can the pilot tell that the prop heat isHow can the pilot tell that the prop heat is


How can the pilot tell that the prop heat is How can the pilot tell that the prop heat is functioning in manual mode?functioning in manual mode?

398


Answer:Answer:


The prop amp meter will not workThe prop amp meter will not work

Answer:Answer:

The pilot must observe the slight increase in The pilot must observe the slight increase in load meters when activatedload meters when activated

399


When operating the windshield antiWhen operating the windshield anti--ice systemice system


When operating the windshield antiWhen operating the windshield anti--ice system, ice system, what are the best practices?what are the best practices?

400


Answer:Answer:


Do not allow windshield to become cold Do not allow windshield to become cold

Answer:Answer:

soakedsoaked Use windshield heat any time the temp is Use windshield heat any time the temp is

b l 5b l 5°°CCbelow 5below 5°°CC Some checklists have windshield heat in the Some checklists have windshield heat in the

climb checkclimb checkclimb checkclimb check Windshield heat should be off on ground in Windshield heat should be off on ground in

warm weather to avoid delaminatingwarm weather to avoid delaminating

401

warm weather to avoid delaminatingwarm weather to avoid delaminating


What does the “NORMAL” windshield heat switchWhat does the “NORMAL” windshield heat switch


What does the NORMAL windshield heat switch What does the NORMAL windshield heat switch position do?position do?

402


Answer:Answer:


Heats the entire windshield panelHeats the entire windshield panel

Answer:Answer:

Heat is not thermostatically controlledHeat is not thermostatically controlled

403


What does the “HIGH” windshield heat switchWhat does the “HIGH” windshield heat switch


What does the HIGH windshield heat switch What does the HIGH windshield heat switch position do?position do?

404


Answer:Answer:


Heats only the outer twoHeats only the outer two--thirds of thirds of i d hi ld li d hi ld l

Answer:Answer:

windshield panelwindshield panelHeat is thermostatically controlled at Heat is thermostatically controlled at

100 to 105100 to 105°°FF

405


What is the max effective windshield antiWhat is the max effective windshield anti--ice speed?ice speed?

406


226226 KtsKts

Answer:Answer:

226 226 KtsKts

407


What is meant by the slang term “hot 5 ON”?What is meant by the slang term “hot 5 ON”?

408


Left and right Left and right pitotpitot heat heat –– ONON

Answer:Answer:

gg ppLeft and right fuel vent heat Left and right fuel vent heat –– ONON

St ll i h tSt ll i h t ONONStall warning heat Stall warning heat –– ONONThese should be final items before each These should be final items before each

t k fft k fftakeofftakeoff

409


Will the stall warning heat function on the ground?Will the stall warning heat function on the ground?

410


Yes but at a reduced powerYes but at a reduced power

Answer:Answer:

Yes, but at a reduced powerYes, but at a reduced power

411


Can the windshield wipers be used on a dryCan the windshield wipers be used on a dry


Can the windshield wipers be used on a dry Can the windshield wipers be used on a dry windshield?windshield?

412


Answer:Answer:


No:No:

Answer:Answer:

It causes windshield damageIt causes windshield damage

413


Procedure for L/R ICE VANE FAILProcedure for L/R ICE VANE FAIL


Procedure for L/R ICE VANE FAIL Procedure for L/R ICE VANE FAIL (manual backup system)(manual backup system)

414


Answer:Answer:


Extend and retract with manual handlesExtend and retract with manual handles

Answer:Answer:

Do not use electric motors until system reset Do not use electric motors until system reset in maintenancein maintenancePull ice vane breakers, and use switches to Pull ice vane breakers, and use switches to

match position of handles in order to retain match position of handles in order to retain ppfunction of function of annunciatorsannunciators

415


Flight ControlsFlight Controls

416

King Air BEKing Air BE--200/B200200/B200Flight ControlsFlight Controls

What powers the primary flight controls?What powers the primary flight controls?

417


The pilot through cables and push rodsThe pilot through cables and push rods

Answer:Answer:

The pilot, through cables and push rodsThe pilot, through cables and push rods

418


What powers the flaps?What powers the flaps?

419


Electric motor through flexible drives andElectric motor through flexible drives and

Answer:Answer:

Electric motor through flexible drives and Electric motor through flexible drives and screwscrew--type actuatorstype actuators

420


Is there split flap protection?Is there split flap protection?

421


Yes between inside and outside flap panels onlyYes between inside and outside flap panels only

Answer:Answer:

Yes, between inside and outside flap panels onlyYes, between inside and outside flap panels onlyThere is no split flap protection between the There is no split flap protection between the

right and left side of the aircraftright and left side of the aircraftright and left side of the aircraftright and left side of the aircraft If activated, the flaps will not moveIf activated, the flaps will not move

422


How are the trim tabs How are the trim tabs preflightedpreflighted??

423


With tabs set to zero, all tabs should alignWith tabs set to zero, all tabs should align

Answer:Answer:

With tabs set to zero, all tabs should align With tabs set to zero, all tabs should align with trailing edge of respective surfacewith trailing edge of respective surfaceThere is no tolerance on the elevator trimThere is no tolerance on the elevator trimThere is no tolerance on the elevator trimThere is no tolerance on the elevator trim

424


What powers the rudder boost?What powers the rudder boost?

425


Instrument air (18 PSI bleed air)Instrument air (18 PSI bleed air)

Answer:Answer:

Instrument air (18 PSI bleed air)Instrument air (18 PSI bleed air)

426


What causes the rudder boost to activate?What causes the rudder boost to activate?

427


Rudder boost activation occurs if there is aRudder boost activation occurs if there is a

Answer:Answer:

Rudder boost activation occurs if there is a Rudder boost activation occurs if there is a 60 PSI difference between P60 PSI difference between P33 output of each output of each engineengine

428



429

King Air BEKing Air BE--200/B200200/B200Landing Gear SystemLanding Gear System

What causes the gear horn warn to sound?What causes the gear horn warn to sound?

430


Throttle below a preset positionThrottle below a preset position

Answer:Answer:

Throttle below a preset position Throttle below a preset position (approximately 70%)(approximately 70%)Flaps past approachFlaps past approachFlaps past approachFlaps past approach

431


Can the gear warning be silenced?Can the gear warning be silenced?

432


If caused by power lever position it can beIf caused by power lever position it can be

Answer:Answer:

If caused by power lever position, it can be If caused by power lever position, it can be silencedsilenced If caused by flaps past approach then it cannotIf caused by flaps past approach then it cannot If caused by flaps past approach, then it cannot If caused by flaps past approach, then it cannot

be silencedbe silenced In either case the gear handle will remain redIn either case the gear handle will remain red In either case, the gear handle will remain redIn either case, the gear handle will remain red

433


Does a King Air have Does a King Air have uplocksuplocks??

434


NoNo

Answer:Answer:

On the mechanical gear, they are held in the On the mechanical gear, they are held in the up position by frictionup position by frictionup position by frictionup position by frictionOn the hydraulic gear, they are held up by On the hydraulic gear, they are held up by

hydraulic pressurehydraulic pressurehydraulic pressurehydraulic pressure

435


What holds the gear down?What holds the gear down?

436


On the mains overOn the mains over--center lockscenter locks

Answer:Answer:

On the mains, overOn the mains, over--center lockscenter locksOn the nose:On the nose: Mechanical nose gear held in position by Mechanical nose gear held in position by

geometry of actuatorgeometry of actuator Hydraulic nose gear has a locking pin in the Hydraulic nose gear has a locking pin in the

nose gear hydraulic ram actuatornose gear hydraulic ram actuator

437


How much system pressure does the hydraulicHow much system pressure does the hydraulic


How much system pressure does the hydraulic How much system pressure does the hydraulic gear use?gear use?

438


Answer:Answer:


2,775 PSI in the up position2,775 PSI in the up position

Answer:Answer:

When the system pressure drops 300 lbs, the When the system pressure drops 300 lbs, the pressure switch cycles the pump on pressure switch cycles the pump on

0 PSI in the down position:0 PSI in the down position: The system uses mechanical locksThe system uses mechanical locksThe system uses mechanical locksThe system uses mechanical locks

439


What type of fluid does the hydraulic gear use?What type of fluid does the hydraulic gear use?

440


MILMIL HH 56065606

Answer:Answer:

MILMIL--HH--56065606

441


What type of fluid is used in the brakes?What type of fluid is used in the brakes?

442


MILMIL--HH--56065606Answer:Answer:

443


How is the parking brake set?How is the parking brake set?

444


Depress brakes and hold, then pull theDepress brakes and hold, then pull the

Answer:Answer:

Depress brakes and hold, then pull the Depress brakes and hold, then pull the parking brake handleparking brake handle

445


How is the parking brake released?How is the parking brake released?

446


Depress brakes and hold then push theDepress brakes and hold then push the

Answer:Answer:

Depress brakes and hold, then push the Depress brakes and hold, then push the parking brake handleparking brake handle

447



448

King Air BEKing Air BE--200/B200200/B200Fuel SystemFuel System

What is the capacity of each main tank?What is the capacity of each main tank?

449


193 U.S. gallons (usable)193 U.S. gallons (usable)Answer:Answer:

g ( )g ( )

450


What is the capacity of each auxiliary tank?What is the capacity of each auxiliary tank?

451


79 U S gallons (usable)79 U S gallons (usable)

Answer:Answer:

79 U.S. gallons (usable)79 U.S. gallons (usable)

452


What is the total capacity of each wing?What is the total capacity of each wing?

453


272 U S gallons272 U S gallons

Answer:Answer:

272 U.S. gallons272 U.S. gallons

454


How does fuel get from the wing to the nacelle?How does fuel get from the wing to the nacelle?

455


Gravity flowGravity flow

Answer:Answer:

yy

456


How does fuel get from the auxiliary tank up toHow does fuel get from the auxiliary tank up to


How does fuel get from the auxiliary tank up to How does fuel get from the auxiliary tank up to the nacelle?the nacelle?

457


Answer:Answer:


Motive flow; fuel, under pressure, flows Motive flow; fuel, under pressure, flows h h j (h h j (V iV i) d d) d d

Answer:Answer:

through a jet pump (through a jet pump (VenturiVenturi) and drawn out ) and drawn out of the auxiliary tank and routed into the of the auxiliary tank and routed into the nacellenacellenacellenacelle

458


What is a jet transfer pump?What is a jet transfer pump?

459


It is a It is a VenturiVenturi

Answer:Answer:

It uses suction generated by the fuel flow to It uses suction generated by the fuel flow to draw the fuel from the auxiliary tankdraw the fuel from the auxiliary tankdraw the fuel from the auxiliary tankdraw the fuel from the auxiliary tank

460


What is the purpose of the standby boost pump?What is the purpose of the standby boost pump?

461


It is to provide backup for the engineIt is to provide backup for the engine--driven driven

Answer:Answer:

p p gp p gfuel boost pumpfuel boost pump It is used ifIt is used if crossfeedcrossfeed is selectedis selectedIt is used if It is used if crossfeedcrossfeed is selectedis selected

462


When When crossfeedcrossfeed is selected, what four things occur?is selected, what four things occur?

463


CrossfeedCrossfeed light comes onlight comes on

Answer:Answer:

ggStandby boost pump activates on the supply sideStandby boost pump activates on the supply sideC f dC f d llCrossfeedCrossfeed valve opensvalve opensMotive flow valve closes on the receiving sideMotive flow valve closes on the receiving side

464


How long is engine operation permissible withHow long is engine operation permissible with


How long is engine operation permissible with How long is engine operation permissible with the “L/R LOW FUEL PRESS” light on?the “L/R LOW FUEL PRESS” light on?

465


Answer:Answer:


10 hours between overhaul/replacement of 10 hours between overhaul/replacement of

Answer:Answer:

ppthe high pressure fuel pumpthe high pressure fuel pump

FUEL PRESS L or R

466


What is indicated by the illumination of the “L/RWhat is indicated by the illumination of the “L/R


What is indicated by the illumination of the L/R What is indicated by the illumination of the L/R LOW FUEL PRESS” light?LOW FUEL PRESS” light?

467


Answer:Answer:


Low pressure, engineLow pressure, engine--driven boost pump driven boost pump

Answer:Answer:

has failedhas failedAlso could indicate failure of an oil scavenge Also could indicate failure of an oil scavenge gg

pump as they share the same drive shaftpump as they share the same drive shaft

468


What does illumination of the “NO TRANSFER”What does illumination of the “NO TRANSFER”


What does illumination of the NO TRANSFER What does illumination of the NO TRANSFER light indicate?light indicate?

469


Answer:Answer:


It is normal for this light to be on for It is normal for this light to be on for 30 to 45 seconds after engine start30 to 45 seconds after engine start

Answer:Answer:

30 to 45 seconds after engine start30 to 45 seconds after engine start Fuel is not transferring from the aux tank to the nacelleFuel is not transferring from the aux tank to the nacelle There is fuel in the Aux TankThere is fuel in the Aux Tank There is fuel in the Aux TankThere is fuel in the Aux Tank Motive flow pressure switch does not see pressureMotive flow pressure switch does not see pressure

470


Why would the “NO TRANSFER” light flicker inWhy would the “NO TRANSFER” light flicker in--flight?flight?

471


It is the unusable fuel sloshing in turbulenceIt is the unusable fuel sloshing in turbulence

Answer:Answer:

It is the unusable fuel sloshing in turbulenceIt is the unusable fuel sloshing in turbulenceThe float switch must indicate fuel The float switch must indicate fuel

ti l f 30 t 45 f th ti tti l f 30 t 45 f th ti tcontinuously for 30 to 45 sec for the timer to continuously for 30 to 45 sec for the timer to open the motive flow valveopen the motive flow valve

472


What operational limitations would exist if flyingWhat operational limitations would exist if flying


What operational limitations would exist if flying What operational limitations would exist if flying with a standby boost pump out of inoperative?with a standby boost pump out of inoperative?

473


Answer:Answer:


CrossfeedCrossfeed would not be available from the would not be available from the

Answer:Answer:

side of the inoperative boost pumpside of the inoperative boost pump

474


What will be the indication of a high pressure fuelWhat will be the indication of a high pressure fuel


What will be the indication of a high pressure fuel What will be the indication of a high pressure fuel pump failure?pump failure?

475


Answer:Answer:


The engine will failThe engine will fail

Answer:Answer:

476


Wh d i i f l f th f tiWh d i i f l f th f ti


When draining fuel for the purpose of separating When draining fuel for the purpose of separating water and debris, how long must you wait after water and debris, how long must you wait after moving or refueling the aircraft?moving or refueling the aircraft?moving or refueling the aircraft?moving or refueling the aircraft?

477


AA


A minimum of three hoursA minimum of three hours

Answer:Answer:

478


Wh h ld th f l t k bWh h ld th f l t k b dd l l il l i


Why should the fuel tanks be Why should the fuel tanks be sumpedsumped regularly in regularly in order to reduce water content?order to reduce water content?

479


AA


To reduce fungus growthTo reduce fungus growth

Answer:Answer:

To reduce fungus growthTo reduce fungus growthTo reduce fuel gauge inaccuracyTo reduce fuel gauge inaccuracy

480


What fuel additive should be used in order toWhat fuel additive should be used in order to


What fuel additive should be used in order to What fuel additive should be used in order to reduce fungus growth?reduce fungus growth?

481


Answer:Answer:


BioborBiobor JF (preferred)JF (preferred)

Answer:Answer:

PristPrist can also be usedcan also be used

482


CanCan PristPrist be added any time?be added any time?


Can Can PristPrist be added any time?be added any time?

483


Answer:Answer:


It must be properly blended with the fuelIt must be properly blended with the fuelAnswer:Answer:

PrePre--mixmix Blended as the fuel is pumped into the tankBlended as the fuel is pumped into the tank

484


Is the use ofIs the use of PristPrist required?required?


Is the use of Is the use of PristPrist required?required?

485


Answer:Answer:


No, it is optional, but should be used if the fuel No, it is optional, but should be used if the fuel is allowed to cool below approximatelyis allowed to cool below approximately 2020°°CC

Answer:Answer:

is allowed to cool below approximately is allowed to cool below approximately --2020°°CC

486

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