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Citat ionCitat ion II II
Flash Cards Flash Cards
FLASH CARDS FLASH CARDS
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October 2013, R1
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Memory ItemsMemory Items
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ENGINE FAILURE/FIRE OR MASTER WARNING DURINGENGINE FAILURE/FIRE OR MASTER WARNING DURING
Memory ItemsMemory Items
11 – –
1.1. BrakesBrakes – – AS REQUIRED AS REQUIRED
2.2. ThrottlesThrottles – – IDLEIDLE
3.3. SpeedbrakesSpeedbrakes – – EXTENDEXTEND4.4. Thrust ReverserThrust Reverser – – DEPLOY ON UNAFFECTED ENGINEDEPLOY ON UNAFFECTED ENGINE
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ENGINE FAILURE/FIRE DURING TAKEOFF ABOVE VENGINE FAILURE/FIRE DURING TAKEOFF ABOVE V11
Memory ItemsMemory Items
– –
After establishing positive rate of climb: After establishing positive rate of climb:
1.1. Landing GearLanding Gear – – RETRACTRETRACT
At 400 ft AGL (Minimum At 400 ft AGL (Minimum – – Clear of Obstacles) and VClear of Obstacles) and V22 + 10:+ 10:
2.2. FlapsFlaps – – RETRACTRETRACT
3.3. Airspeed Airspeed – – ACCELERATE TO V ACCELERATE TO VENRENR
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EMERGENCY EVACUATIONEMERGENCY EVACUATION
Memory ItemsMemory Items
1.1. Throttles (BOTH)Throttles (BOTH) – – CUTOFFCUTOFF
If no fire:If no fire:
2.2. Fire Switches (BOTH)Fire Switches (BOTH) – – PRESSPRESSIf fire suspected:If fire suspected:
3.3. Illuminated Fire SwitchesIlluminated Fire Switches – – LIFT COVER/PUSHLIFT COVER/PUSH
4.4. Both Illuminated Bottle Armed LightsBoth Illuminated Bottle Armed Lights – – PRESSPRESS
5.5. Remaining Fire SwitchRemaining Fire Switch – – PRESSPRESS
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EMERGENCY EVACUATION (Cont’d.)EMERGENCY EVACUATION (Cont’d.)
Memory ItemsMemory Items
5.5. Parking BrakeParking Brake – – SETSET
6.6. Advise ATC Advise ATC
7.7. Battery SwitchBattery Switch – – OFFOFF8.8. Evacuate Aircraft Via Appropriate ExitEvacuate Aircraft Via Appropriate Exit
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Indicates fire loop detectsIndicates fire loop detectsLH ENGINE RH ENGINE
Annunciators Annunciators
500500°°F (fire or overheat). PushingF (fire or overheat). PushingFIREFIRE switchlightswitchlight::
FIRE
PUSH
FIRE
PUSH
– – Closes associated fuel and hydraulicCloses associated fuel and hydraulic
firewall shutoff valvesfirewall shutoff valves
– – Removes power from associatedRemoves power from associated
BOTTLE 1BOTTLE 1
ARMED ARMED
PUSHPUSH
BOTTLE 2BOTTLE 2
ARMED ARMED
PUSHPUSH
thrust reverser isolation valvethrust reverser isolation valve
– – Arms both fire extinguisher bottles Arms both fire extinguisher bottles
and illuminates both white BOTTLEand illuminates both white BOTTLE
Pushing light discharges to
selected engine. Both bott les
can be directed to same
ARMED PUSH lights ARMED PUSH lights
– – Opens affective engine’s generatorOpens affective engine’s generator
field relayfield relay
.
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ENGINE FIRE (LH OR RH ENGINE FIRE WARNINGENGINE FIRE (LH OR RH ENGINE FIRE WARNING
Memory ItemsMemory Items
LIGHT/SWITCH ILLUMINATED)LIGHT/SWITCH ILLUMINATED)BOTTLE 1BOTTLE 1 LH ENGINE BOTTLE 2BOTTLE 2RH ENGINE
Engine Fire Switch IlluminatedEngine Fire Switch Illuminated – – Fire Bell ActivatedFire Bell Activated
PUSHPUSH PUSH PUSHPUSHPUSH
1.1. Throttle (affective engine)Throttle (affective engine) – – IDLEIDLE
If f ire light remains illuminated:If fire light remains illuminated:
2.2. Engine Fire Switch (affective engine)Engine Fire Switch (affective engine) – – LIFTLIFTCOVER/PUSHCOVER/PUSH
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.. Either White Bottle Armed LightEither White Bottle Armed Light – – PUSHPUSH
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THRUST REVERSER INADVERTENT DEPLOYMENTTHRUST REVERSER INADVERTENT DEPLOYMENT
Memory ItemsMemory Items
11 – –
1.1. BrakesBrakes – – MAXIMUM PILOT EFFORTMAXIMUM PILOT EFFORT
2.2. ThrottlesThrottles – – IDLEIDLE
3.3. SpeedbrakesSpeedbrakes – – ExtendExtend4.4. Thrust ReversersThrust Reversers – – DEPLOY BOTHDEPLOY BOTH
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THRUST REVERSER INADVERTENT DEPLOYMENTTHRUST REVERSER INADVERTENT DEPLOYMENT
Memory ItemsMemory Items
11 – –
1.1. Emer Emer STOW Switch (affective engine)STOW Switch (affective engine) – – EMEREMER
2.2. Throttle ( Affective Engine)Throttle ( Affective Engine) – – CHECK IDLECHECK IDLE
At positive rate of climb At positive rate of climb3.3. Landing GearLanding Gear – – RETRACTRETRACT
4.4. Airspeed Airspeed – – 125 KIAS MAXIMUM UNTIL T/R STOWS125 KIAS MAXIMUM UNTIL T/R STOWS
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THRUST REVERSER INADVERTENT DEPLOYMENTTHRUST REVERSER INADVERTENT DEPLOYMENT
’’
Memory ItemsMemory Items
11 – – . .
At 400 ft AGL (Minimum) At 400 ft AGL (Minimum) – – Clear of Obstacles and VClear of Obstacles and V22 + 10:+ 10:
5.5. FlapsFlaps – – RETRACTRETRACT
6.6. Airspeed Airspeed – – ACCERATE ACCERATEIf Reverser stows:If Reverser stows:
7.7. Airspeed Airspeed – – 200 KIAS MAXIMUM200 KIAS MAXIMUM
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THRUST REVERSER INADVERTENT INFLIGHTTHRUST REVERSER INADVERTENT INFLIGHT
Memory ItemsMemory Items
DEPLOYMENTDEPLOYMENT
1.1. Control Wheel/AutopilotControl Wheel/Autopilot – – GRIP/DISENGAGEGRIP/DISENGAGE
2.2. Emergency STOW SwitchEmergency STOW Switch – – EMER (affective engine)EMER (affective engine)
3.3. Affected Throttle Affected Throttle – – CHECK IDLECHECK IDLE4.4. Airspeed Airspeed – – REDUCE TO 125 KIAS OR BELOWREDUCE TO 125 KIAS OR BELOW
If thrust reverser stows (DEPLOY and UNLOCK Lights out):If thrust reverser stows (DEPLOY and UNLOCK Lights out):
5.5. Airspeed Airspeed – – DO NOT EXCEED 200 KIASDO NOT EXCEED 200 KIAS
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THRUST REVERSER UNLOCK LIGHT ON INTHRUST REVERSER UNLOCK LIGHT ON IN
Memory ItemsMemory Items
FLIGHTFLIGHT
1.1. Emer Emer Stow Switch (Affective Engine)Stow Switch (Affective Engine) – – EMEREMER
2.2. Thrust Reverser LeversThrust Reverser Levers – – CHECK/STOWED (FULLCHECK/STOWED (FULL
FORWARD)FORWARD)
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EMERGENCY RESTARTEMERGENCY RESTART – – TWO ENGINESTWO ENGINES
Memory ItemsMemory Items
1.1. IgnitionIgnition – – BOTH ONBOTH ON
2.2. Fuel Boost PumpFuel Boost Pump – – BOTH ONBOTH ON
3.3. ThrottlesThrottles – – IDLEIDLEIf alti tude allows:If alti tude allows:
4.4. Airspeed Airspeed – – INCREASE TO 200 KIASINCREASE TO 200 KIAS
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ENGINE FAILURE DURING COUPLEDENGINE FAILURE DURING COUPLED
Memory ItemsMemory Items
APPROACH APPROACH
1.1. Power (Operating Engine)Power (Operating Engine) – –INCREASEINCREASE
2.2. Autopilot/Yaw Damper Autopilot/Yaw Damper – – OFFOFF.. rspeerspee – – REFREF ++
4.4. Rudder TrimRudder Trim – – TRIM TOWARDTRIM TOWARD
5.5. FlapsFlaps – – TAKEOFF AND APPROACHTAKEOFF AND APPROACH
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ELECTRICAL FIRE OR SMOKEELECTRICAL FIRE OR SMOKE
Memory ItemsMemory Items
1.1. Oxygen MaskOxygen Mask – – DON/100%DON/100%
.. – – MASKMASK
3.3. Pressurization Source SelectorPressurization Source Selector – –NORMNORM
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SMOKE REMOVALSMOKE REMOVAL
Memory ItemsMemory Items
1.1. Oxygen MasksOxygen Masks – – DON/100%DON/100%
.. – –
3.3. Crew Oxygen Priority ValveCrew Oxygen Priority Valve – –CHECK NORMALCHECK NORMAL
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BATTERY OVERHEATBATTERY OVERHEAT
Memory ItemsMemory Items
1.1. Amperage Amperage – – NOTENOTE
2.2. Battery SwitchBattery Switch – – EMEREMER
3.3. Amperage Amperage – – NOTE DECREASENOTE DECREASE
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CABIN DECOMPRESSION (CAB ALT 10KCABIN DECOMPRESSION (CAB ALT 10K
Memory ItemsMemory Items
WARNING LIGHT ON)WARNING LIGHT ON)
1.1. Oxygen MasksOxygen Masks – – DON/100%DON/100%
2.2. Emergency DescentEmergency Descent – – AS REQUIRED AS REQUIRED
3.3. Passenger OxygenPassenger Oxygen – – ENSURE USEENSURE USE4.4. OxygenOxygen MicMic SwitchesSwitches – – MIC OXY MASKMIC OXY MASK
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EMERGENCY DESCENTEMERGENCY DESCENT
Memory ItemsMemory Items
1.1. ThrottlesThrottles –– IDLEIDLE
2.2. SpeedbrakesSpeedbrakes – – EXTENDEXTEND
3.3. Landing GearLanding Gear – – DOWN (speed below 250 KIAS)DOWN (speed below 250 KIAS)4.4. Initiate Moderate BankInitiate Moderate Bank
5.5. Pitch AttitudePitch Attitude – – APPROX. 25 APPROX. 25°° NOSE DOWNNOSE DOWN
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ENVIRONMENTAL SYSTEM SMOKE OR ODORENVIRONMENTAL SYSTEM SMOKE OR ODOR
Memory ItemsMemory Items
1.1. OXYGEN MASKSOXYGEN MASKS – – DON/100%DON/100%
2.2. OxygenOxygen MicMic SwitchesSwitches – – MIC OXYMIC OXYMASKMASK
.. – –
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SMOKE REMOVALSMOKE REMOVAL
Memory ItemsMemory Items
1.1. Oxygen MasksOxygen Masks – – DON/100%DON/100%
2.2. Oxygen Control ValveOxygen Control Valve – – MANUALMANUALDROPDROP
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AUTOPILOT HARDOVER AUTOPILOT HARDOVER
Memory ItemsMemory Items
1.1. Autopilot TRIM DISC Switch Autopilot TRIM DISC Switch – – PRESSPRESS
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ELECTRIC ELEVATOR RUNAWAY TRIMELECTRIC ELEVATOR RUNAWAY TRIM
Memory ItemsMemory Items
1.1. Autopilot/Trim Disengage Switch Autopilot/Trim Disengage Switch – – PRESS AND HOLDPRESS AND HOLDContinue to HOLD until PITCH TRIM CB is pulled.Continue to HOLD until PITCH TRIM CB is pulled.
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Annunciators Annunciators
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Annunciators Annunciators
MASTER WARNING RESETMASTER WARNING RESET
WARNINGRESET
lights flash in conjunction withlights flash in conjunction withillumination of a red warningillumination of a red warning
annunc a or annunc a or. ey a so as. ey a so as
Both GEN OFF or BothBoth GEN OFF or Both
illuminate. Reset by pressingilluminate. Reset by pressing
eithereither switchli htswitchli ht
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Indicates fire loop detectsIndicates fire loop detectsLH ENGINE RH ENGINE
Annunciators Annunciators
500500°°F (fire or overheat). PushingF (fire or overheat). PushingFIREFIRE switchlightswitchlight::
FIRE
PUSH
FIRE
PUSH
– – Closes associated fuel andCloses associated fuel and
hydraulic firewall shutoff valveshydraulic firewall shutoff valves
– – ’’
BOTTLE 1BOTTLE 1
ARMED ARMED
PUSHPUSH
BOTTLE 2BOTTLE 2
ARMED ARMED
PUSHPUSH
reverser isolation valvereverser isolation valve
– – Arms both fire extinguisher Arms both fire extinguisher
Pushing light discharges to
selected engine. Both bott les
can be directed to same
white BOTTLE ARMED PUSHwhite BOTTLE ARMED PUSH
lightslights
.
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– – Opens affective engine’sOpens affective engine’s
generator field relaygenerator field relay
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Annunciators Annunciators
Operated by the ENGINE FIREOperated by the ENGINE FIREF/W
switchlightsswitchlights, illumination, illuminationindicates the respective fuelindicates the respective fuelSHUTOFF
an y rau c rewa s u oan y rau c rewa s u o
valves are closed. To reopenvalves are closed. To reopen
,,
switchswitchL F/W
SHUTOFF
R F/W
SHUTOFF
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Annunciators Annunciators
Indicates isolation valve isIndicates isolation valve is ARM
open and system isopen and system ispressurizedpressurized
Indicates thrust reverser is notIndicates thrust reverser is not
fully stowed. Reverser doorsfully stowed. Reverser doors
UNLOCK
are un oc e . g on n gare un oc e . g on n g
triggers Master Warningtriggers Master Warning
fully deployedfully deployedDEPLOY
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Annunciators Annunciators
Indicates oil pressure is belowIndicates oil pressure is belowLO OIL
safe limits (35 PSI) onsafe limits (35 PSI) ondesignated engine. Andesignated engine. An
PRESS
n epen en sensor r ves en epen en sensor r ves e
oil pressure gaugeoil pressure gauge
PRESS LO
R OIL
PRESS LO
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FuelFuel
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Annunciators Annunciators – – FuelFuel
Illumination indicates fuelIllumination indicates fuelFUEL
boost pump is turned on by:boost pump is turned on by:
– – Low fuel pressureLow fuel pressure
BOOST ON
– – CrossfeedCrossfeed operationsoperations
– – En ine start orEn ine start or
– – Manual boost pump switchManual boost pump switchBOOST ON
R FUEL
BOOST ON
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Illumination indicates fuelIllumination indicates fuelFUEL LOW
Annunciators Annunciators – – FuelFuel
pressure is low. The low fuelpressure is low. The low fuel
pressure switch (5 PSI) willpressure switch (5 PSI) will
PRESS
ac va e e assoc a e oosac va e e assoc a e oos
pump to on if the boost pumppump to on if the boost pump
PRESS LO
R FUEL
PRESS LO
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Illumination indicatesIllumination indicatesFUEL FLTR
Annunciators Annunciators – – FuelFuel
designated fuel filter isdesignated fuel filter is
contaminate and that an actualcontaminate and that an actual
BYPASS
or mpen ng ypassor mpen ng ypass
condition existcondition exist
ons er e poss y oons er e poss y o
partial or total loss of bothpartial or total loss of bothFUEL FILTBYPASS
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Indicates fuel quantity, asIndicates fuel quantity, asFUEL LOW
Annunciators Annunciators – – FuelFuel
determined by a float switch,determined by a float switch,
is below 169 lbsis below 169 lbs
LEVEL
approx ma e y o usea e ueapprox ma e y o usea e ue
in designated tankin designated tank
L FUEL
LEVEL LO
R FUELLEVEL LO
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ElectricalElectrical
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Steady illumination indicatesSteady illumination indicatesBATT
Annunciators Annunciators – – ElectricalElectrical
battery temp is between 145battery temp is between 145°°FF
and 160and 160°°FFO’ TEMP
Flashing illumination indicatesFlashing illumination indicates
battery temp exceeds 160battery temp exceeds 160°°FF
BAT
O’HEAT
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Also triggers the Red MASTER WARNING.
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Indicates the designatedIndicates the designatedGEN
Annunciators Annunciators – – ElectricalElectrical
generator power relay is opengenerator power relay is open
Loss of both generatorsLoss of both generators
OFF
triggers the Red MASTERtriggers the Red MASTER
WARNINGWARNING
L GEN OFF
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Indicates one or both invertersIndicates one or both inverters AC
Annunciators Annunciators – – ElectricalElectrical
failed or AC BUS CB openedfailed or AC BUS CB openedFAIL
AC Indicates one or both invertersIndicates one or both inverters
failedfailed
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Also triggers the Red MASTER WARNING.
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Indicates the loss of powerIndicates the loss of powerINVERTER
Annunciators Annunciators – – ElectricalElectrical
from designated inverter.from designated inverter.
Failure of either inverterFailure of either inverter
FAIL
r ggers er ggers e
annunciator annunciator, which triggers, which triggers
1 FAIL
INVERTER
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Steady illumination indicatesSteady illumination indicates
Annunciators Annunciators – – ElectricalElectrical
WARNINGRESET
loss of power to Masterloss of power to Master
Warning System and mayWarning System and may
n ca e oss o power o en ca e oss o power o e
Main Bus Extension onMain Bus Extension on
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EnvironmentEnvironment
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Indicates cabin pressureIndicates cabin pressure
Annunciators Annunciators – – EnvironmentEnvironment
altitude is above 10,000 ftalti tude is above 10,000 ft10000 FT
CAB ALT
10000 FT
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Also triggers the Red MASTER WARNING lights.
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Indicates emergencyIndicates emergency
Annunciators Annunciators – – EnvironmentEnvironment
pressurization is on eitherpressurization is on either
from manual selection orfrom manual selection orPRESS ON
au oma c ac va on yau oma c ac va on y
overheat; ACM shuts downoverheat; ACM shuts down
GND
EMER PRESS
ON
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Also triggers the Red MASTER WARNING lights.
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Indicates a high flow rate ofIndicates a high flow rate of
Annunciators Annunciators – – EnvironmentEnvironment
bleed air is selected from thebleed air is selected from the
right engine for ACM groundright engine for ACM groundPRESS ON
opera ons; pressur za onopera ons; pressur za on
source selector is in GNDsource selector is in GND
GND
nnunc a or nnunc a or mus emus e
extinguished before takeoff extinguished before takeoff BLEED AIRGND/HI
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Indicates temperature in theIndicates temperature in the
Annunciators Annunciators – – EnvironmentEnvironment
duct past the ACM leading toduct past the ACM leading to
the cabin exceeds 157the cabin exceeds 157°°CC
O’HEAT
O’ PRESS
AIR DUCT
’
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Indicates ACM ejector jetIndicates ACM ejector jet
Annunciators Annunciators – – EnvironmentEnvironment
pump valve is open. This ispump valve is open. This is
normal during groundnormal during groundON
opera ons w poweropera ons w power 22or brakes appliedor brakes applied
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Indicates overheat condition.Indicates overheat condition.L PRECOOL
Annunciators Annunciators – – EnvironmentEnvironment
Temperature of bleed air at theTemperature of bleed air at the
exit side of theexit side of the precooler precooler
FAIL
R PRECOOL
excee sexcee s approx ma e yapprox ma e y
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Indicates ACM bleed air supplyIndicates ACM bleed air supply
Annunciators Annunciators – – EnvironmentEnvironment
pressure is more than 42 PSIpressure is more than 42 PSI
O’HEAT
O’ PRESS
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Indicates one of the following:Indicates one of the following:
Annunciators Annunciators – – EnvironmentEnvironment
– – Nose orNose or tailconetailcone doors aredoors are
unlockedunlocked
-
INOP
– – A failure or improper position of A failure or improper position of
one or more door switchesone or more door switches
– –
LOCKED
forwardforward cabin door pincabin door pinDOOR NOT
LOCKED
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Flight ControlsFlight Controls
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Indicates autopilotIndicates autopilot
Annunciators Annunciators – – Flight ControlsFlight Controls
disconnected, accompanieddisconnected, accompanied
by 2by 2--second tonesecond tone
AUTO PILOT
OFF
MOMENTARY: IndicatesMOMENTARY: Indicates
disengaged by normal means:disengaged by normal means: AP TORQUE
– – A/P TRIM DISC button on either A/P TRIM DISC button on either
control wheel was pressedcontrol wheel was pressed
– – --
– – Either electric elevator trim switchEither electric elevator trim switch
was actuatedwas actuated
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STEADY: Indicates theSTEADY: Indicates the
Annunciators Annunciators – – Flight Controls (Cont’d.)Flight Controls (Cont’d.)
autopilot disengaged byautopilot disengaged by
abnormal means:abnormal means:
AUTO PILOT
OFF
– – AC or DC power loss AC or DC power loss
– – Vertical or directional gyro failedVertical or directional gyro failed AP TORQUE
– – u on was pus e u on was pus e
– – Vertical gyro switch (HI) wasVertical gyro switch (HI) was
– – L/R gyro slaving switch wasL/R gyro slaving switch wasactuatedactuated
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Indicates a torque failure wasIndicates a torque failure was
Annunciators Annunciators – – Flight ControlsFlight Controls
sensed or the torque servosensed or the torque servo
switching at 14,500 MSL failedswitching at 14,500 MSL failed
AUTO PILOT
OFF
AP TORQUE
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Anti Anti--IceIce
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IntermittentIntermittent: Indicates bleed air: Indicates bleed air
Annunciators Annunciators – – Anti Anti--IceIce
temp in the duct to thetemp in the duct to the
windshield exceeds safewindshield exceeds safeO’HEAT
empera ure m sempera ure m s ,,
system inoperativesystem inoperative
on nuouson nuous: n ca es poss e: n ca es poss e
temp controller failure ortemp controller failure orW/S AIRO’HEAT
valve failed openvalve failed open
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Steady illuminationSteady illumination indicates oneindicates one
Annunciators Annunciators – – Anti Anti--IceIce
or more of the following: engineor more of the following: engine
cowl leading edge is below 77cowl leading edge is below 77°°CC ANTI ICE
eng ne s a or va ve no openeng ne s a or va ve no open
Inboard wing leading edge sectionInboard wing leading edge section
°°
LH RH
temp sensor temp sensor L ENG
ICE FAIL
failure in a low or high tempfailure in a low or high tempsensor. Normal ice rotectionsensor. Normal ice rotection
R ENG
ICE FAIL
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should still be availableshould still be available
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Indicates wing and/orIndicates wing and/or
Annunciators Annunciators – – Anti Anti--IceIce
horizontal stabilizer deicehorizontal stabilizer deice
system pressure switchessystem pressure switchesSURF DEICE
sense a m n mum osense a m n mum o
SURFACE
DEICE
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CitationCitation IIII
Indicates either:Indicates either:
Annunciators Annunciators – – Anti Anti--IceIce
– – Power is lost toPower is lost to pitotpitot tube heatertube heater
or one or both static ports inor one or both static ports inOFF
– – Associated Associated pitotpitot heat switch isheat switch is
OFFOFF
LH RH
P/S HTR
OFF
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CitationCitation IIII
HydraulicsHydraulics
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Gear Handle Down:Gear Handle Down:
Annunciators Annunciators – – HydraulicsHydraulics
– – Indicates one or more gear notIndicates one or more gear not
down and lockeddown and lockedGEAR
UNLOCKED
ear an e p:ear an e p:
– – Indicates at least one gear hasIndicates at least one gear hasNOSE
,,
but is not yet up and lockedbut is not yet up and locked
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ADVISORY, indicates output ADVISORY, indicates outputL HYD
Annunciators Annunciators – – HydraulicsHydraulics
from the designated hydraulicfrom the designated hydraulic
pump(s) is below normalpump(s) is below normalR HYD
PRESS LO
LOW
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Indicates fluid in hydraulicIndicates fluid in hydraulicHYD LEVEL
Annunciators Annunciators – – HydraulicsHydraulics
reservoir is below acceptablereservoir is below acceptable
level (0.2 gallon or less)level (0.2 gallon or less)
LOW
HYD LOW
LEVEL
HYD PRESS
ON
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Advises that the hydraulic Advises that the hydraulicHYD PRESS
Annunciators Annunciators – – HydraulicsHydraulics
system is pressurizedsystem is pressurizedON
HYD LOW
LEVEL
HYD PRESS
ON
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Indicates antiIndicates anti--skid system isskid system is ANTI-SKID
Annunciators Annunciators – – HydraulicsHydraulics
inoperative or the controlinoperative or the control
switch is OFFswitch is OFF
INOP
ANTI-SKID
INOP
DOOR NOT
LOCKED
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Advises that the power Advises that the power--wheelwheel--PWR BRK
Annunciators Annunciators – – HydraulicsHydraulics
brake hydraulic pressure isbrake hydraulic pressure is
lowlow
PRESS LO
NOTE: If the power brake pump fails afterNOTE: If the power brake pump fails after
accumulator pressure exceeds 750 PSI, theaccumulator pressure exceeds 750 PSI, the
annunciator annunciator may not illuminate untilmay not illuminate until
POWER
BRAKE norma ra es are use .norma ra es are use .LOW PRESS
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Avionics Avionics
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Illumination indicates aIllumination indicates a
Annunciators Annunciators – – Avionics Avionics
overheat of symbol generator overheat of symbol generator
HOT FAN
HOT HOTM
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A red A red annunciator annunciator of ATT FAILof ATT FAIL
Annunciators Annunciators – – Avionics Avionics
above the aircraft wings (EFIS)above the aircraft wings (EFIS)
indicates a PFD attitude failureindicates a PFD attitude failure ATT
R1
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Illumination indicates aIllumination indicates a
Annunciators Annunciators – – Avionics Avionics
overheat of associated displayoverheat of associated display
indicator(s)indicator(s)
EADI DISP
HOT FAN
HOT HOT
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UNIT 627+: IlluminationUNIT 627+: Illumination
Annunciators Annunciators – – Avionics Avionics
indicates a high tempindicates a high temp
condition exists in the nosecondition exists in the noseO’TREMPav on cs compar menav on cs compar men
Annunciator Annunciator should notshould notMP
um na e n g un essum na e n g un esssome equipment failure existsome equipment failure exist
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Illumination indicates failure ofIllumination indicates failure of
Annunciators Annunciators – – Avionics Avionics
pilot’s EFIS cooling fanpilot’s EFIS cooling fanEADI DISP
HOT FAN
HOT HOT
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Indicates multifunction displayIndicates multifunction display
Annunciators Annunciators – – Avionics Avionics
symbol generator issymbol generator is
overheatingoverheating
MFD SG
HOT
FAN HOT
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Indicates multifunction displayIndicates multifunction display
Annunciators Annunciators – – Avionics Avionics
is overheatingis overheatingMFD SG
HOT
FAN HOT
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Indicates multifunction displayIndicates multifunction display
Annunciators Annunciators – – Avionics Avionics
cooling fan failedcooling fan failedMFD SG
HOT
FAN HOT
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Operational LimitationsOperational Limitations
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Minimum Crew:Minimum Crew:
General LimitationsGeneral Limitations
Pilot and Copilot:Pilot and Copilot:
The pilot must have a CEThe pilot must have a CE--500 type rating and500 type rating and
meet the requirements of FAR 61.58meet the requirements of FAR 61.58
The copilot shall possess a multiThe copilot shall possess a multi--engine rating,engine rating,
an ns rumen ra ng or g a ove or n oan ns rumen ra ng or g a ove or n oand meet the requirements of FAR 61.55and meet the requirements of FAR 61.55
completedcompleted
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Baggage Limits:Baggage Limits:
General LimitationsGeneral Limitations
Nose Baggage Compartment:Nose Baggage Compartment:__350 lbs______ __350 lbs______
__ ______ __ ______
TailconeTailcone Baggage Compartment:____ Baggage Compartment:____ 500 lbs500 lbs ____ ____
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Passenger Seat Position:Passenger Seat Position:
General LimitationsGeneral Limitations
For Takeoff and Landings, the following apply:For Takeoff and Landings, the following apply:
Passenger seat belts and shoulder harnesses mustPassenger seat belts and shoulder harnesses must
be fastenedbe fastened
The seat just aft of the emergency exist must be inThe seat just aft of the emergency exist must be in
most aft posit ionmost aft posit ion
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What is Maximum Taxi and Ramp Weight?What is Maximum Taxi and Ramp Weight?
WeightsWeights
,,
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What is the Maximum Takeoff Weight?What is the Maximum Takeoff Weight?
WeightsWeights
,
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What is the Maximum Landing Weight?What is the Maximum Landing Weight?
WeightsWeights
,
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Maximum Zero Fuel Weight:Maximum Zero Fuel Weight:
WeightsWeights
, , ,
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Minimum Flight Weight:Minimum Flight Weight:
WeightsWeights
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Maximum Flaps Extended (VMaximum Flaps Extended (V ) for:) for:
SpeedsSpeeds
Full Flaps (40Full Flaps (40°°):):
Partial Flaps, T.O. & APPR. (15Partial Flaps, T.O. & APPR. (15°°))
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What is Maximum Landing Gear ExtendedWhat is Maximum Landing Gear Extended
SpeedsSpeeds
176 KIAS176 KIAS
Speed (VSpeed (VLELE)?)?
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CitationCitation IIII
S dS d
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What is Maximum Landing Gear OperatingWhat is Maximum Landing Gear Operating
SpeedsSpeeds
Extendin = 176 KIASExtendin = 176 KIAS
Speed (VSpeed (VLOLO)?)?
Retracting = 176 KIASRetracting = 176 KIAS
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S dS d
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What is VWhat is V (Minimum Control(Minimum Control -- Air)? Air)?
SpeedsSpeeds
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S dS d
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What is VWhat is V (Minimum Control(Minimum Control -- Ground)?Ground)?
SpeedsSpeeds
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SpeedsSpeeds
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What is Maximum VWhat is Maximum V Below 14,000 ft?Below 14,000 ft?
SpeedsSpeeds
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CitationCitation IIII
SpeedsSpeeds
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What is Maximum VWhat is Maximum V between 14 000 andbetween 14 000 and
SpeedsSpeeds
28,000 ft?28,000 ft?
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CitationCitation IIII
SpeedsSpeeds
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What is Maximum MWhat is Maximum M (above 28,000 ft)?(above 28,000 ft)?
SpeedsSpeeds
..
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CitationCitation IIII
SpeedsSpeeds
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What is MaximumWhat is Maximum SpeedbrakeSpeedbrake ExtensionExtension
SpeedsSpeeds
(V(VSBSB)?)?
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CitationCitation IIII
SpeedsSpeeds
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What is Maximum Autopilot OperationWhat is Maximum Autopilot Operation
SpeedsSpeeds
(Speed):(Speed):
..
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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What is the Maximum Airport PressureWhat is the Maximum Airport Pressure
TakeoffTakeoff & Landing& Landing
14,000 ft14,000 ft
Altitude for Takeoff and Landing? Altitude for Takeoff and Landing?
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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What is the Maximum Air TemperatureWhat is the Maximum Air Temperature
TakeoffTakeoff & Landing& Landing
ISA+39ISA+39°°CC
Approved for Takeoff and Landing? Approved for Takeoff and Landing?
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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Is AntiIs Anti--skid required for takeoff?skid required for takeoff?
TakeoffTakeoff & Landing& Landing
Anti Anti--skid must be operational for takeoffskid must be operational for takeoff
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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Maximum CrosswindMaximum Crosswind -- Demonstrated?Demonstrated?
TakeoffTakeoff & Landing& Landing
2323 KtsKts
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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Maximum Tailwind com onent is:Maximum Tailwind com onent is:a eoa eo & a d g& a d g
R1
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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Maximum Tailwind component is:Maximum Tailwind component is:
gg
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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What is the Maximum Water/Slush onWhat is the Maximum Water/Slush on
gg
Runway?Runway?
..
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CitationCitation IIII
TakeoffTakeoff & Landing& Landing
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Vertical navigation (VNAV) system must beVertical navigation (VNAV) system must be
gg
off below:off below:
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EnrouteEnroute LimitsLimits
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CitationCitation IIII
Loads Factor Loads Factor
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Minimum Airs eed for sustained fli ht inMinimum Airs eed for sustained fli ht in
icing conditions (except for approach andicing conditions (except for approach and
landing):landing):
160 KIAS160 KIAS
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CitationCitation IIII
Loads Factor Loads Factor
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What is the Maximum Calibrated OperatingWhat is the Maximum Calibrated Operating
Altitude? Altitude?
,,
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CitationCitation IIII
Loads Factor Loads Factor
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What is the Generator Load in flight?What is the Generator Load in flight?
400 Amps Up to 35,000 ft400 Amps Up to 35,000 ft
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CitationCitation IIII
Loads Factor Loads Factor
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What is Maximum Load Factor In Flight for:What is Maximum Load Factor In Flight for:
--1.52 to +3.5G at 13 300 lbs1.52 to +3.5G at 13 300 lbs
Flaps UP?Flaps UP?
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CitationCitation IIII
Wh i M i L d F I Fli h fWh i M i L d F I Fli h fLoads Factor Loads Factor
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What is Maximum Load Factor In Flight forWhat is Maximum Load Factor In Flight for
--0.0 to +2.0G at 13 300 lbs0.0 to +2.0G at 13 300 lbs
Flaps 15Flaps 15°°??
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CitationCitation IIII
Loads Factor Loads Factor
Wh t i M i L d F t fWh t i M i L d F t f
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What is Maximum Load Factor for What is Maximum Load Factor for
+3.5 at 12 700 lbs+3.5 at 12 700 lbs
Landing, flaps 15Landing, flaps 15°° to 40to 40°°??
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Avionics Avionics
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CitationCitation IIII
Wh t i th Mi i Altit d f A t il tWh t i th Mi i Altit d f A t il t Avionics Avionics
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What is the Minimum Altitude for AutopilotWhat is the Minimum Altitude for Autopilot
1000 ft AGL1000 ft AGL – – EnrouteEnroute
Use?Use?
300 ft AGL Non300 ft AGL Non--precision Approachprecision Approach
– – pproac espproac es
The autopilot and yawThe autopilot and yaw--damper must bedamper must be
off for takeoff and landingoff for takeoff and landing
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CitationCitation IIII
Can you dispatch if either the PFD HOT MFDCan you dispatch if either the PFD HOT MFD Avionics Avionics
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Can you dispatch if either the PFD HOT, MFDCan you dispatch if either the PFD HOT, MFD
HOT or IC HOTHOT or IC HOT annunciator annunciator illuminated?illuminated?
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CitationCitation IIII
Can you dispatch with the NOSE AVN FANCan you dispatch with the NOSE AVN FAN
Avionics Avionics
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Can you dispatch with the NOSE AVN FANCan you dispatch with the NOSE AVN FAN
FAILFAIL annunciator annunciator illuminated?illuminated?
,,
procedures are followedprocedures are followed
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CitationCitation IIII
What standby instruments must beWhat standby instruments must be
Avionics Avionics
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Airplanes)? Airplanes)?
ATT ATT
ALT/ASI ALT/ASI
HSIHSI
accomplished on the standby gyroaccomplished on the standby gyros stems stem
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ElectricalElectrical
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CitationCitation IIII
What is the Maximum Load Factor in FlightWhat is the Maximum Load Factor in FlightElectricalElectrical
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What is the Maximum Load Factor in FlightWhat is the Maximum Load Factor in Flight
for Flaps UP?for Flaps UP?
,,
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CitationCitation IIII
What are the Battery limitations for engineWhat are the Battery limitations for engineElectricalElectrical
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What are the Battery limitations for engineWhat are the Battery limitations for engine
starts?starts?
Three generator Three generator--assisted crossassisted cross--startsstarts
equa one a ery s ar equa one a ery s ar
A GPU start does not count as a battery A GPU start does not count as a battery
cyclecycle
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CitationCitation IIII
What are the Starter Limitations for engineWhat are the Starter Limitations for engineElectricalElectrical
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What are the Starter Limitations for engineWhat are the Starter Limitations for engine
starts?starts?
Three engine starts per 30 minutes withThree engine starts per 30 minutes with
secon res per o e ween cyc essecon res per o e ween cyc es
With GPU or GEN. Asst. Cross Start:With GPU or GEN. Asst. Cross Start:
TWO engine starts per 30 minutes withTWO engine starts per 30 minutes with90 second rest eriod between c cles90 second rest eriod between c cles
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PressurizationPressurization
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CitationCitation IIII
What is the Maximum Pressure Differential?What is the Maximum Pressure Differential?PressurizationPressurization
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What is the Maximum Pressure Differential?What is the Maximum Pressure Differential?
..
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CitationCitation IIII
Flood Cooling is prohibited above?Flood Cooling is prohibited above?PressurizationPressurization
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g pg p
,,
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CitationCitation IIII
Operation in HIGH (PAC flow) mode is notOperation in HIGH (PAC flow) mode is notPressurizationPressurization
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p ( )p ( )
approved for?approved for?
45,000 ft45,000 ft
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Flight ControlsFlight Controls
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CitationCitation IIII
The Stall Warning System:The Stall Warning System:Flight ControlsFlight Controls
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g yg y
the preflight test in the AFMthe preflight test in the AFM
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CitationCitation IIII
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FuelFuel
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CitationCitation IIII
What is the MaximumWhat is the Maximum Ass metric Ass metric Fuel wei htsFuel wei hts
FuelFuel
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for Normal and Emergency conditions?for Normal and Emergency conditions?
Emergency: 600 lbsEmergency: 600 lbs
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HydraulicsHydraulics
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CitationCitation IIII
HydraulicsHydraulics
Name some approved types of HydraulicName some approved types of Hydraulic
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fluid and it’s color?fluid and it’s color?
SkydrolSkydrol 500 B500 B--4,C or LD4,C or LD--4/Green or use4/Green or use
HyjetHyjet
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Ice and RainIce and Rain
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CitationCitation IIII
Permissible Operating TimePermissible Operating Time
Ice and RainIce and Rain
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Limit ground operations ofLimit ground operations of pitotpitot/static heat/static heat
toto 2 minute2 minute to reclude dama e to theto reclude dama e to the __ __pitotpitot--static tubes and the anglestatic tubes and the angle--of of--attackattack
probe.probe.
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CitationCitation IIII
When must Engine and Windshield antiWhen must Engine and Windshield anti--iceice
Ice and RainIce and Rain
t b t dt b t d
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When o eratin in visible moisture andWhen o eratin in visible moisture and
systems be turned on.systems be turned on.
when OAT is atwhen OAT is at --3030°°C to +10C to +10°°CC
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OxygenOxygen
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CitationCitation IIII
Continuous use of the su lemental ox enContinuous use of the su lemental ox en
OxygenOxygen
t i hibit d b th f ll it i hibit d b th f ll i
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system is prohibited above the followingsystem is prohibited above the following
cabin alti tudes:cabin alti tudes:
Carrying Passengers:_ Carrying Passengers:_25,000 ft25,000 ft _ _
Crew Only:_ Crew Only:_37,000 ft EROS37,000 ft EROS _ _
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CitationCitation IIII
Reverse thrust must be reduced to idleReverse thrust must be reduced to idle
PowerplantPowerplant & Thrust Reversers& Thrust Reversers
reverse by what speed?reverse by what speed?
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60 KIAS60 KIAS
reverse by what speed?reverse by what speed?
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CitationCitation IIII
Maximum reverse thrust is limited to:Maximum reverse thrust is limited to:
PowerplantPowerplant & Thrust Reversers& Thrust Reversers
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Maximum takeoff ower less 2% NMaximum takeoff ower less 2% N
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CitationCitation IIII
Additional T/R Limitations: Additional T/R Limitations:
PowerplantPowerplant & Thrust Reversers& Thrust Reversers
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Must be verif ied operational per preflight testMust be verif ied operational per preflight test
Prohibited during touch and go landingsProhibited during touch and go landings
Max deployment speed is 115 KIASMax deployment speed is 115 KIAS
Prohibited on sod or gravel runwaysProhibited on sod or gravel runways
Max deployed time is 15 minutes in any oneMax deployed time is 15 minutes in any one
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hour periodhour period