Citation I-II-SII Flashcards Dallas

8/19/2019 Citation I-II-SII Flashcards Dallas

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Citat ionCitat ion II II

Flash Cards Flash Cards

FLASH CARDS FLASH CARDS

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Copyright © 2013 CAE 1

October 2013, R1


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CitationCitation IIII

Memory ItemsMemory Items

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ENGINE FAILURE/FIRE OR MASTER WARNING DURINGENGINE FAILURE/FIRE OR MASTER WARNING DURING


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


– –

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


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.)


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


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


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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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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’’


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


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


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


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


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


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


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


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


WARNING LIGHT ON)WARNING LIGHT ON)


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


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


1.1. OXYGEN MASKSOXYGEN MASKS – – DON/100%DON/100%

2.2. OxygenOxygen MicMic SwitchesSwitches – – MIC OXYMIC OXYMASKMASK

.. – –

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SMOKE REMOVALSMOKE REMOVAL



2.2. Oxygen Control ValveOxygen Control Valve – – MANUALMANUALDROPDROP

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AUTOPILOT HARDOVER AUTOPILOT HARDOVER


1.1. Autopilot TRIM DISC Switch Autopilot TRIM DISC Switch – – PRESSPRESS

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ELECTRIC ELEVATOR RUNAWAY TRIMELECTRIC ELEVATOR RUNAWAY TRIM


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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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


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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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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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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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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Also triggers the Red MASTER WARNING.


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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


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


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


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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Indicates the designatedIndicates the designatedGEN


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


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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Indicates the loss of powerIndicates the loss of powerINVERTER


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


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


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


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


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


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


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


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:


– – 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


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


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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Indicates either:Indicates either:


– – 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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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


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


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


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


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


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


above the aircraft wings (EFIS)above the aircraft wings (EFIS)

indicates a PFD attitude failureindicates a PFD attitude failure ATT

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Illumination indicates aIllumination indicates a


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


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


pilot’s EFIS cooling fanpilot’s EFIS cooling fanEADI DISP

HOT FAN

HOT HOT

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Indicates multifunction displayIndicates multifunction display


symbol generator issymbol generator is

overheatingoverheating

MFD SG

HOT

FAN HOT

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is overheatingis overheatingMFD SG

HOT

FAN HOT

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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:


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:


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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S dS d


87/138

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


88/138

What is VWhat is V (Minimum Control(Minimum Control -- Air)? Air)?

SpeedsSpeeds

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S dS d


89/138

What is VWhat is V (Minimum Control(Minimum Control -- Ground)?Ground)?

SpeedsSpeeds

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SpeedsSpeeds


90/138

What is Maximum VWhat is Maximum V Below 14,000 ft?Below 14,000 ft?

SpeedsSpeeds

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90


SpeedsSpeeds


91/138

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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SpeedsSpeeds


92/138

What is Maximum MWhat is Maximum M (above 28,000 ft)?(above 28,000 ft)?

SpeedsSpeeds

..

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SpeedsSpeeds


93/138

What is MaximumWhat is Maximum SpeedbrakeSpeedbrake ExtensionExtension

SpeedsSpeeds

(V(VSBSB)?)?

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SpeedsSpeeds


94/138

What is Maximum Autopilot OperationWhat is Maximum Autopilot Operation

SpeedsSpeeds

(Speed):(Speed):

..

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95/138

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TakeoffTakeoff & Landing& Landing


96/138

What is the Maximum Airport PressureWhat is the Maximum Airport Pressure


14,000 ft14,000 ft

Altitude for Takeoff and Landing? Altitude for Takeoff and Landing?

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97/138

What is the Maximum Air TemperatureWhat is the Maximum Air Temperature


ISA+39ISA+39°°CC

Approved for Takeoff and Landing? Approved for Takeoff and Landing?

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98/138

Is AntiIs Anti--skid required for takeoff?skid required for takeoff?


Anti Anti--skid must be operational for takeoffskid must be operational for takeoff

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99/138

Maximum CrosswindMaximum Crosswind -- Demonstrated?Demonstrated?


2323 KtsKts

R1

99




100/138

Maximum Tailwind com onent is:Maximum Tailwind com onent is:a eoa eo & a d g& a d g

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101/138

Maximum Tailwind component is:Maximum Tailwind component is:

gg

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101




102/138

What is the Maximum Water/Slush onWhat is the Maximum Water/Slush on

gg

Runway?Runway?

..

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102




103/138

Vertical navigation (VNAV) system must beVertical navigation (VNAV) system must be

gg

off below:off below:

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104/138

EnrouteEnroute LimitsLimits

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Loads Factor Loads Factor


105/138

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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105




106/138

What is the Maximum Calibrated OperatingWhat is the Maximum Calibrated Operating

Altitude? Altitude?

,,

R1

106




107/138

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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108/138

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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Wh i M i L d F I Fli h fWh i M i L d F I Fli h fLoads Factor Loads Factor


109/138

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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Wh t i M i L d F t fWh t i M i L d F t f


110/138

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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111/138

Avionics Avionics

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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


112/138

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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Can you dispatch if either the PFD HOT MFDCan you dispatch if either the PFD HOT MFD Avionics Avionics


113/138

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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Can you dispatch with the NOSE AVN FANCan you dispatch with the NOSE AVN FAN

Avionics Avionics


114/138

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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What standby instruments must beWhat standby instruments must be

Avionics Avionics


115/138

Airplanes)? Airplanes)?

ATT ATT

ALT/ASI ALT/ASI

HSIHSI

accomplished on the standby gyroaccomplished on the standby gyros stems stem

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116/138

ElectricalElectrical

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What is the Maximum Load Factor in FlightWhat is the Maximum Load Factor in FlightElectricalElectrical


117/138

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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What are the Battery limitations for engineWhat are the Battery limitations for engineElectricalElectrical


118/138

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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118


What are the Starter Limitations for engineWhat are the Starter Limitations for engineElectricalElectrical


119/138

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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120/138

PressurizationPressurization

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What is the Maximum Pressure Differential?What is the Maximum Pressure Differential?PressurizationPressurization


121/138

What is the Maximum Pressure Differential?What is the Maximum Pressure Differential?

..

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121


Flood Cooling is prohibited above?Flood Cooling is prohibited above?PressurizationPressurization


122/138

g pg p

,,

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122


Operation in HIGH (PAC flow) mode is notOperation in HIGH (PAC flow) mode is notPressurizationPressurization


123/138

p ( )p ( )

approved for?approved for?

45,000 ft45,000 ft

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124/138

Flight ControlsFlight Controls

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The Stall Warning System:The Stall Warning System:Flight ControlsFlight Controls


125/138

g yg y

the preflight test in the AFMthe preflight test in the AFM

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126/138

FuelFuel

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126


What is the MaximumWhat is the Maximum Ass metric Ass metric Fuel wei htsFuel wei hts

FuelFuel


127/138

for Normal and Emergency conditions?for Normal and Emergency conditions?

Emergency: 600 lbsEmergency: 600 lbs

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128/138


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Name some approved types of HydraulicName some approved types of Hydraulic


129/138

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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130/138

Ice and RainIce and Rain

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Permissible Operating TimePermissible Operating Time



131/138

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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131


When must Engine and Windshield antiWhen must Engine and Windshield anti--iceice


t b t dt b t d


132/138

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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133/138

OxygenOxygen

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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


134/138

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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135/138

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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?


136/138

60 KIAS60 KIAS

reverse by what speed?reverse by what speed?

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136


Maximum reverse thrust is limited to:Maximum reverse thrust is limited to:



137/138

Maximum takeoff ower less 2% NMaximum takeoff ower less 2% N

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Additional T/R Limitations: Additional T/R Limitations:



138/138

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

Documents

Citation I-II-SII Flashcards Dallas