C17 CBT Flashcards by Tenille Abbott

To enable an alert start, set the APU control switches to:

. MODE SEL to ALERT START CONTROL TO START

.AUTO SHITDOWN ORIDE ON and OFF/ARM to ARM

.MODE SEL to ALERT and START CONTR to RUN

.OFF/ARM to ARM and START CONTR to START

MODE SEL to ALERT and START CONTR to RUN

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Where is the external power door located?

.On the left side of the aircraft aft of the nose

.On the right side of the aircraft aft of the nose

.on the right wheel pod

.on the left wheel pod

On the right side of the aircraft aft of the nose.

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The AUTO SHT DN ORIDE switchlight will override all automatic shutdowns except?

.Fire and over speed

.fire and high EGT

.high EGT and over speed

.low oil press and high EGT

Fire and Overspeed

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When in the vicinity of an operating APU, you should wear

.Ear protection

.Eye protection

.Protective clothing

.Hard hat

Ear protection

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Which switch is used for a normal APU start

.START CONTR switch

.MODE SEL switch

START CONTR switch

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In addition to the MASTER CAUTION and the APU cue light, the indication you receive for above normal EGT reading is.

.HIGH light

.HOT light

.EGT HIGH on WAP

.EGT HOT on WAP

HOT light.

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You are in the cargo compartment and the APU is running. Suddenly, you hear the APU warning horn. What does the horn indicate?

.APU fuel Low

.APU overspeed

.APU fire

.APU auto shutdown

APU Fire

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The APU OIL indication on the WAP may mean the APU

.Oil needs changing

.Oil filter is bypassed

.Oil pressure or quantity is abnormal

.Generator voltage is low.

Oil pressure or quantity is abnormal

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An APU fire will be indicated on which of the following panels?

.APU Control, AFT left loadmaster and single point refuelling

.APU control, aft loadmaster and electrical control

.Aft loadmaster, FWD loadmaster and APU control

.Aft loadmaster, fwd loadmaster and single point refuelling

APU control, aft left loadmaster and single point refuelling

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What is used for emergency operations to allow restart of the APU after an automatic shutdown has occurred to provide bleed air pressure for an engine start?

. Push the AUTO SHIT DN ORIDE

.Select ALERT on MODE SEL

.Move START CONTR to START

.Turn on No. 3 boost pump

Push the AUTO SHT DN ORIDE

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The AVAIL light will not illuminate unless the power cart shows the following under no-load condition.

. Volts 110 to 122, Frequency 350 +/- 12.

.Volts 112-122, Frequency 400 +/- 12

.Volts 110 to 124, Frequency 350 +/- 10

.Volts 112-124, Frequency 400 +/- 10

Volts 112-122, Frequency 400 +/- 12

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During APU start and operation, the exhaust does not represent a personal hazard.

.True

.False

False

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How close to the fire should you position the hand held fire extinguisher?

.12 feet

.8 feet

.4 feet

.2 feet

8 feet

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Which of the following are the correct warning signals for ditching situations?

.one sustained ring to signal the crew to prepare and six short rings to brace for impact

.one sustained ring to signal the crew to prepare and three short rings to brace for impact

.three short rings to signal the crew to prepare and one sustained ring to brace for impact

.six short rings to to signal the crew to prepare and one sustained ring to brace for impact

Six short rings to signal the crew to prepare and one sustained ring to brace for impact

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The transmission lines for the FEDS are arranged so that any ________ initiator(s) can fire all four hatches.

.one

.two

.three

.four

One

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The system that incorporates a pyrotechnic that burns openings in the aircrafts structure is called ____________ system.

.automated egress

.flotation equipment deployment

.ramp blowdown

.bailout

Flotation equipment deployment

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Ramp blowdown may not function if the weight on the ramp exceeds _______ pounds.

.20,000

.20,750

.25,000

.40,000

20,750

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How many fire extinguishers are located on the aircraft?

.four

.six

.eight

.nine

Nine

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If Passengers are onboard the aircraft and ground evacuation is necessary, it is your responsibility to

.Notify the passengers of the situation and direct the evacuation.

.Immediately open the ramp and door and inform the passengers to evacuate.

.Passout headset so the pilot can inform the passages of procedures to be followed.

.Act as if nothing is wrong, using situational awareness to make up an excuse to get the passengers off the aircraft.

Notify the passengers of the situation and direct the evacuation.

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When CBrC1F2 decomposes, It can be hazardous. It can be recognised by its_________odour.

.very sweet

.sharp, acrid

.rotten eggs

.pleasant

Sharp, acrid

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Flotation equipment deployment system manual initiators are located.

.Above the crew entry and trapdoors.

.at the forward loadmaster station.

.in the crew rest area.

.At each FEDS exit and externally at the forward left wing root

At each FEDS exit and externally at the forward left wing root

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How many Emergency Escape Breathing Devices are on the C-17?

. 7

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Portable fire extinguishers are located in which areas?

. Crew rest area, cargo compartment, fwd lm area

. Cockpit, crew rest area, cargo compartment

. Cockpit, lavatory, cargo compartment

. Crew rest area, cockpit, Galley

Cockpit, crew rest area, cargo compartment

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Which of the following are cockpit ground egress areas?

.clear view sliding windows, emergency ejection hatches

.clear view sliding windows, overhead maint ditching hatch.

.Crew entry door, emergency escape hatches

.crew entry door, overhead maint ditching hatch

Clear up sliding windows, maint ditching hatch.

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Do not activate the FEDS hatches prior to the aircraft coming to rest as the

.fuselage may break apart

.Life rafts may be lost

.Ladders may be lost

.hatches may jam

Life rafts may be lost

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If the wiring to the cockpit emergency locator switch is severed or shorted during a crash, the emergency locator transmitter will

.shut off temporarily

.still operate normally

.operate for five minutes

.not operate

Still operate normally

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The flotation equipment deployment system may be electronically armed. To ACTIVATE the system, the crew member must

.pull the quick release pin and turn the handle ninety degrees.

.pull down on the handle to release the quick release pin and turn the handle ninety degrees.

.pull the quick release pin, turn the handle ninety degrees, then pul downward.

.pull down on the handle, then turn ninety degrees.

Pull the quick release pin, turn the handle ninety degrees then pull downward.

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Where are the crash axes located?

.crew rest area and cargo compartment

.cockpit and cargo

.cockpit only

.cargo compartment only

Crew rest area and cargo compartment

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Control panels for ramp blowdown are located at the

.forward and aft loadmaster station

.aft left and right loadmaster stations

.forward and aft loadmaster stations

.forward loadmaster station and right troop door

Forward and aft loadmaster station

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Of the eight ground egress exits on the c-17, how many are equipped with escape ropes?

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Failure to fully install safety switch pins or place CMDS WOW MAINT ORIDE switch to normal could result in unintended jettison of payloads

.true

.false

True

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Do not use external power with the battery switch OFF.

.true

.false

True

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If the external power unit is not rated at __________ KVA or above, it is not capable of supporting the large initial electrical load requirements of the AUX hydraulic pumps

.60

.70

.80

.90

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To preclude damage to the slat seals, the APU should not be started or operated with the slats in ___________ position. If the APU must be started with the slats___________, they should be retracted as soon as possible.

.retracted,extended

.extended, Extended

.reset, retracted

.off, extended

Extended, extended

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OBIGGS II To prevent fuselage fire, electrical power shall be applied to the aircraft prior to connecting an external high pressure pneumatic air source.

.true

.false

True

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Aircraft batteries can be fully recharged by the battery charges in

.30 min

.45 min

.1 hour 30 min

.1 hour 45 min

1 hour 30 min

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Generator no.2 is inoperative. Which component allows AC from generator 1 to power generator bus no.2?

.AC transfer bus

.AC cross tie(s)

.Generator power relay

.Generator bus tie(s)

Generator bus tie(s)

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The normal operating configuration for the electrical system is ____________ mode.

.split-isolated mode

.isolated

.parallel

.split-parallel

Split parallel

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Circuit breaker location on the various circuit breaker panels is identified

.by vertical and horizontal references

.in alphabetical order as listed in TO 1C-17A-1

.in numerical order as listed in TO 1C-17A-1

.by system load requirements

By vertical and horizontal references

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When using the DC electrical system, the _________ configuration is the normal mode for operation.

.split parallel

.conversion

.isolated

.parallel

Split parallel

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Circuit breakers will open if

.the amount of electricity in the circuit breaker is more than the circuit breaker can tolerate

.the pilot touches the wrong switch on the electrical panel

.the pilot and co pilot not flying turn on the same switch at the same time

.the AC X TIE switch is placed in the AUTO position too soon after you establish aircraft power

The amount of electricity in the circuit breaker is more than the circuit breaker can handle

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The transformer/rectifiers perform the function of

.providing power for APU start

.converting DC power to AC power

.providing emergency power for the DC buses

.converting AC power to DC power

Converting AC power to DC power.

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Which of the following buses is always powered even if the battery switch is off?

.emergency power bus

.battery direct bus

.AC transfer bus

.DC transfer bus

Battery direct bus

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The APU and EPU supply electrical power to the _________ of the aircraft, respectively

.right and left sides

.left and right sides

.forward and aft sides

.aft and forward sides

Left and right sides

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Which generator buses are the normal sources of power for the battery chargers?

.2&3

.1&2

.1&4

.2&4

1&4

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Which electrical system component is used to join the left and right sides of the aircraft so the the AC electrical system operates in parallel mode?

.AC cross tie

.Inverters

.Emergency power relay

AC transfer bus

AC cross tie

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As a minimum, aircraft batteries can supply emergency power up to _________ minutes

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Which position of the avionics bus switch(AV BUS) enable automatic load shedding when the aircraft is on the ground with inadequate cooling?

.ORIDE

.OFF

.AUTO

.OPEN

AUTO

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A mishap that has a fatality or permanent total disability is a class __________ mishap

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All vehicles must approach parked aircraft with the vehicles _______ toward the aircraft

.front end

.right side

.back end

.operators side

Operators side

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When working on or around aircraft, _______ will not be worn

.earplugs

.contact lenses

.gloves

.rings

Rings

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The _________ will be used to record any mishap that occurs during flight or the mission

.AMC form 97

. AF form 457

.AF form 651

.AF form 761

AMC form 97

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The speed limit for vehicles within 25 feet of the aircraft is ______ MPH

.10

.15

.20

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Smoking is not permitted on the flight line except in designated areas and never closer than _______ feet to the aircraft.

.25

.50

.75

.100

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When in the vicinity of an operating APU, ________ protection should be worn.

.eye

.ear

.head

.foot

Ear

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The speed limit for the aircraft parking ramp is ________ MPH

.10

.15

.20

.25

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Vehicles are not allowed within ______ feet of a parked aircraft except when the aircraft is being serviced, loaded or off-loaded .

.10

.25

.50

.75

10feet

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At what power setting are the engines capable of developing enough inlet duct suction to cause fatal injuries to a person too close to the inlet?

. low

.medium

.high

.all of the above

All of the above

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The warning and caution annunciation panel

.displays visual warning, caution, and advisory messages for various systems throughout the aircraft.

.automatically prioritises messages as received

.provides aural and visual warnings of potentially dangerous flight conditions that could lead to a collision with the ground

.allows acknowledgment of advisory warning messages by pressing the reset button

Displays visual warning, caution, and advisory messages for various systems throughout the aircraft

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Before caution messages can be manually scrolled, new caution messages must first be acknowledged by pressing the

.SCROLL push button

.GROUND PROX light

.AURAL SILENCE button

.MASTER CAUTION light

MASTER CAUTION LIGHT

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The two panels at the forward loadmaster station that provide warning and caution information are the DOOR/STATUS panel and the

.alt warning horn panel

.fire extinguisher panel

.cargo compartment lights panel

.cargo smoke detection panel

Cargo smoke detection panel

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If both WCCs fail or the WAP fails, the ________ illuminates
.MASTER WARNING light

.MASTER CAUTION light

.WACS fail light

.head-up display

WACs fail light

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Which type of message on the warning and caution annunciation panel indicates a hazardous condition that requires immediate corrective action?

.advisory

.caution

.warning

.cue

WARNING

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An improperly secured ladder poses a threat to

.Loadmaster

.Pilot

.copilot

.personnel seated underneath the ladder.

personnel seated underneath the ladder

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When the troop door is checked, ensure the door is closed and locked and the DOOR NOT LOCKED annunciator is illuminated

.true

.false

False

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The oxygen shutoff valve at the forward loadmaster station will be closed only for an emergency action or for flight.

.True

.False

False

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An electrical shock is possible when installing/removing a defective hot cup if the cup timer is powered

.True

.False

True

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The ______ cargo compartment lights will not function if the CARGO OVERHEAD ORIDE light switch is in the WHITE position at LACP-LS or if the LIGHT SELECT switch at the LFCP is in the white position,

.White

.Red

.Exit

.Subdued

RED

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Stowage of equipment on the aft bulkhead of the cargo door is prohibited

.true

.false

TRUE

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An unsecure IV post may rapidly slide from the stanchion during _______ and strike personnel seated in sidewall seats

.Landing

.Approach

.Takeoff

.Taxi

Takeoff

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When the RAMP BLOWDN EMERG LIGHTS are tested, which lights should illuminate?

.All emergency lights in the cargo compartment

.All EXIT signs

.All emergency lights and exit signs aft of the troop doors and the two exit signs at FS1345

.All ramp and door lights

All emergency lights and exit signs aft of the troop doors and the two exit signs at FS1345

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To prevent deployment of FEDS, ensure the

.Switch cover is closed, initiator handle is turned to open, and the safety pin has been removed.

.Switch cover is open, initiator handle is turned to open, and the safety pin is in place.

.Switch cover is open, initiator handle is turned to lock, and the safety pin is in place.

.Switch cover is closed, initiator handle is turned to lock,
and the safety in is in place

Switch cover is closed, initiator handle is turned to lock,

and the safety in is in place

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When the STAB STRUT ACTUATORS circuit breaker is pulled, the STRUT DOOR light on the DOOR?STATUS panel will illuminate

.True

.False

False

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Which control provides general illumination of the flight deck area?

.Dome light

.Flow line PWR switch

.NVG/T-STORM switch

.OVERHEAD PANEL switches

DOME light

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Which lights are controlled from the forward Loadmaster station?

.Cargo compartment

.Galley

.Lavatory

.Ramp and Door

Cargo compartment

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Controls for the lights that illuminate the flight deck floor are located on the ________ light control panel

.Crew rest area

.centre pedestal

.stairway

.forward loadmaster station

centre pedestal

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The nacelle scanning lights are located on the upper surface of each wingtip

.True

.False

False

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Combat lighting features are enabled through the _________ on the cockpit overhead panel and the forward loadmaster control panel

.Anti-collision lights

.MODE SELECT Switches

.EMERG light switches

IR CARGO overhead switch

MODE SELECT Switches

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The stowage compartment and ________ light switches are located on the crew entry light panel

.galley panel

.stairway

.forward loadmaster station

.forward aisle

forward aisle

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Two rotating beacons are called _____ lights

.anti collision

.landing/taxi

.runway turn off

.wingtip landing

Anti-collision

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with the MODE SELECT switch in IR, the aircraft may not be visible during ground operations at night unless using night vision devices

.True

.False

True

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Shutdown the aircraft electrical system with either emergency light switch in the ON or ARM position, will cause the emergency lights to remain illuminated and could cause depletion of the emergency batteries.

.True

.False

True

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The emergency evacuation lighting is enabled in all positions of the MODE SELECT switch

.True

.False

True

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The OXYGEN CONTROL panel backlights are inhibited in the SECURE mode

.True

.False

True

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Infrared light sources are invisible to the unaided eye. To prevent eye damage, avoid extended unprotected direct viewing of operating exterior infrared lights from closer than 6 feet.

.True

.False

True

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What two sets of lights provide the maximum amount of lighting to the ramp area?

.Exterior/ interior

.Service, jump station

.Cargo door, staging lights

.Cargo door, formation

cargo door, staging lights

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Staging lights are controlled from the

.Cockpit overhead panel

.forward loadmaster station

.cargo ramp and door panel

.aft left loadmaster station

aft left loadmaster station

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The FLUORESCENT light switch on the forward loadmaster panel is inhibited when the MODE SELECT switch is in NVG or SECURE mode.

.True

.False

True

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The primrary source of oxygen for the crew system is ________ liquid oxygen converter(s)

. One 25Litre

.One 75Litre

.Two 25Litre

.Two 75Litre

one 25Litre

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After turning the regulator supply lever to off during the oxygen mask pre flight, if the user can continue to breathe normally without resistance, it means that the oxygen

.Regulator is defective

.Converter is leaking

.Mask is too tight

.Regulator is working properly

Regulator is defective

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Sufficient oxygen must be on board before takeoff to fly

.The planned mission at 25,000ft, unpressurised.

.The mission from ETP to original destination at cruise altitude using 100% oxygen at FL250

.From ETP to the next suitable recovery base using 100% oxygen at FL250

.The mission from departure to destination to the alternate airfield

from ETP to the next suitable recovery base using 100% oxygen at FL250

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The oxygen control panel for the passenger/auxiliary oxygen system is located at the _______ loadmaster station

.forward

.instructor

.aft left

.aft right

forward

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when positive pressure is required, the oxygen mask must be well fitted to the face to prevent rapid depletion of the oxygen supply.

.True

.False

True

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IF the aircraft loses cabin pressure, the aircraft commander will descend

.immediately to below 8,500ft MSL

.immediately to below 10,000ft MSL

.to an altitude not above FL180 and notify AMC ground station

.to the lowest practical altitude, preferably below 18,000ft MSL, but below FL250

To the lowest practical altitude, preferably below 18,000ft MSL, but below FL250.

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During normal operation, the oxygen regulator levers will be positioned as follows:

.SUPPLY lever - ON, DILUTER lever 100%, EMERGENCY lever - Normal.

.SUPPLY lever - ON, DILUTER lever - Normal, EMERGENCY lever - Normal.

.SUPPLY lever - OFF, DLIUTER lever - NORMAL, EMERGENCY lever - Normal.

.SUPPLY lever - OFF, DILUTER lever - 100%, EMERGENCY lever - Normal.

SUPPLY lever - on, DILUTER lever - 100%, EMERGENCY lever - Normal

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The normal pressure for the passenger oxygen system is

.150-300psi

.200-375psi

.250-430psi

.285-430psi

285-430psi

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The passenger oxygen system contains one ______ litre converter and one _______ litre auxiliary converter.

.75;75

.75;25

.25;75

.25;25

75;75

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When stowing the quick-don masks, if the end of the strap is inside the clamp or facing away from the crew position, the mask will be easier to remove from the hanger.

.true

.false

false

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If the mask assembly is stored improperly, the suspension assembly will unfold and

.transfer communications capability from the headset to the oxygen mask microphone.

.disable any oxygen use.

.allow oxygen to leak from the mask.

.cause a dangerous spark near 100% flowing oxygen.

.transfer communications capability from the headset to the oxygen mask microphone.

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The CREW OXY LOW warning illumination on the WAP indicates the oxygen

. quantity remaining is less than 5 litres or supply pressure is below 60psi +/- 5psi

.quantity remaining is less than 7.5 litres or supply pressure is below 75psi +/- 5 psi

.pressure is below 75psi

.pressure is above 80psi

quantity is less than 5 litres or pressure is below 60psi +/- 5psi.

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The oxygen cross feed switch is used to

.connect the auxiliary system to the passenger system

.isolate the passenger oxygen converter

.isolate the crew oxygen converter

.connect the crew and passenger oxygen system

connect the crew and passenger oxygen system

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There is/are ______ engine driven hydraulic pumps(s) per system, located on and driven by their respective engine accessory gearbox.

.one

.two

.three

.four

four

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The RAT, located in the forward right main gear pod, develops enough hydraulic pressure to control the aircraft for

.Takeoff and refuelling

.Emergency refueling

.LAPES delivery

.All enigne-out emergency

All engine-out emergency.

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A warning appears on the WAP when the hydraulic reservoir temperature first exceeds

.100 degrees c

.121 degrees c

.125 degress c

.155 degrees c

121 degrees c

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The engine-driven hydraulic pumps provide continuous hydraulic pressure of _______ Psi

.4000

.4,200

.4,500

.5,000

4,000

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The primary purpose of the ______ pump is to assist in landing gear retraction or cargo door/ramp closing in the event of No. 2 or No. 3 engine loss.

.auxiliary

.transfer

.primary

.secondary

transfer

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The engine-driven hydraulic pumps are located in the

.respective engine accessory gearbox

right aft gear pod

.wheel wells

.cargo compartment

respective engine accessory gearbox

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The manifold fail annunciation and ilimunation of the MANIFOLD FAIL light indicates a failure of what system

.Hydraulic

.Bleed air

.Electrical

.Fuel

Bleed air

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pressing the AVIONICS COOL ORIDE switchlight to OPEN drives the avionics augmentation valve and the avionics cooling outflow valves open.

.True

.False

True

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If the AVIONICS OVERHEAT caution persists after completing the procedures, __________ until maintenance can correct the system.

.evacuate the aircraft.

.open avionics compartment doors

.turn off electrical power

.distribute hearing protection devices.

turn off electrical power

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on the Loss of Pressurisation checklist, Loadmaster’s report - CHECK COMPLETED indicates

.the loadmaster is seated with seatbelt fastened

.the loadmaster is cleared off oxygen

.all passengers are on oxygen

.passengers are safe to move around

all passengers are on oxygen

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Once annunciated during ascent, the WAP message CABIN PRESS LOW and CAWS alert CABIN ALTITUDE may continue to display/annunciate until a cabin altitude as low as ______ ft is achieved.

.8000

.7000

.6000

.5000

8,000

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if passenger oxygen masks are deployed using the DROP switchlight below 12,500ft cabin altitude, or the DROP switchlight was pressed more than once, each emergency oxygen regulator SURGE mode lever/three position toggle switch must be positioned to ________ to provide passenger oxygen.

.AUTO/AUTO

.MANUAL OFF

.MANUAL ON

.MANUAL OVER

MANUAL ON

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During the smoke, fire or fumes checklist, what could be used to aid in filtering fumes if EPOS is not available?

.Having passengers place their hands over their face

.Use of wet towels/cloth over the passengers oxygen mask

.Moving passengers to the aft part of the plane

.Turning on the exhaust fans.

use of wet towel/cloth over the passenger oxygen masks.

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Because avionics cooling is critical prompt corrective action is required.

.True

.False

True

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When flying through contaminated airspace, the air used for avionics cooling will be

.shut off

.purified

.contaminated

.circulated through all compartments

contaminated

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The isolation valve divides the manifold into the left and right side.

.True

.False

True

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Each ramp heater control cycles its heater on at a ramp temperature of _____ degrees f and off at _______ degrees f.

.30;50

.35;45

.30;45

.35;50

35;50

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Where is the outflow valve?

.Lower left side of fuselage

.upper left side of fuselage

.lower right side of fuselage

.upper right side of fuselage

lower right side of fuselage

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When the CARGO FLR HTR switch is in the AUTO position, the heater strips automatically activate if the cargo floor temperature drops below 65 degrees fahrenheit.

.True

.False

True

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Which aircraft components require a close visual inspection and must be clear of frost, ice and snow?

.Fuselage and wings

.Landing gear, control surfaces

.External door controls, gear doors

.All of the above

All of the above

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A thin coating of frost is permitted on the fuselage, provided _______ are visible.

.Crew chiefs

.antennas

.lights

.lettering/paint lines

lettering/paint lines

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If an engine has been cold soaked for an extended period, white smoke may appear during start.

.True

.False

True

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If icing conditions are expected during the descent, engine anti-ice, wing anti-ice, and windshield anti-ice will be turned on at least _____ feet above the expected icing level in order to provide adequate warm-up time.

.5,000

.10,000

.15,000

.20,000

10,000

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Because of the time required to charge the _______ accumulators, system No.2 will remain at approximately 1,000 to 2,500 psi until the accumulators are filled.

.flap

.cargo door

.brake

.landing gear

brake

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Frost on the ______ may reduce aircraft stall margin and lift so that a safe takeoff may not be possible.

.upper wings

.lower wings

.fuselage

.engine nacelles

upper wings

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If frost, icing, or snow conditions are encountered after the aircraft is inspected and considered clean, a _____ will be accomplished by the flight crew.

.before takeoff check

.full stop taxi back

.pre takeoff check

.line up

pre takeoff check

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When a heavy accumulation of snow is present, deicing procedures shall begin at the ______ prior to moving to the forward section of the aircraft

.wheel well and landing gear

.wing

.nose

.tail of the aircraft and rear fuselage

tail of the aircraft and rear fuselage

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visible moisture includes

.rain

.snow

.sleet or ice crystals

.all of the above

all of the above

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After the cabin has stabilised above -40f, the crew, passenger and auxiliary oxygen systems may be

.serviced

.purged

.re pressurised

.too cold to use

re pressurised

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If required to be accomplished, the pre takeoff contamination check must be accomplished from outside the aircraft within five minutes of prior to take off.

.True

.False

True

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Hydraulic transfer pump inadequate pressure output may occur at ambient temperatures colder than

.20C

.20F

.0F

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What is the size of a standard 463L pallet?

.54 x 88 x 2 1/4 inches

.54 x 88 x 2 1/2 inches

.108 x 88 x 2 1/4 inches

.108 x 88 x 2 1/2 inches

108 x 88 x 2 1/4 inches

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An aluminium rail with indentations and tie down rings extends along the outer perimeter of a pallet. what is the capacity of each tie down ring?

.2,500 pounds

.5,000 pounds

.7,500 pounds

.10,000 pounds

7,500 pounds

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Pallet coupling devices are used to secure

.metal cargo containers to the pallet tie down rings

.two or more pallets together

.two or more side nets together

.metal cargo containers to the restraint rails

two or more pallets together

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Pallets are solid aluminium pallets with tie down rings

.True

.False

False

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The maximum single pallet weight for cargo secured with nets and stacked over 96” shall not exceed 8,000 pounds

.True

.False

True

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Which panel allows you to simultaneously lock or release all logistic restraint locks on the cargo floor and ramp>

.Aft logistic pallets control panel

.Logistic lock gang release panel

.Left logistic pallet position panel

.right logistic pallet position panel

Logistic lock gang release panel

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Which logistic pallet positions have two pairs of locks?

.1,7,8 and 9

.1,8 and 9

.1 through 7

.2 through 6

2 through 6

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Where are the quad teeter rollers located?

.Forward edge of the ramp

.aft end of the ramp

.aft edge of the cargo floor

.forward edge of the ramp toes

aft end of the ramp

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What is the function of the gang lock back up panel?

.Enables you to operate the right sidewall control panels.

.Allows operation in case the logistic lock gang control switches fail.

.Ensure that none of the locks will be released.

.Allows you to check all annunciators on the right sidewall control panel.

Allows operation in case the logistic lock gang control switches fail.

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When not in use, the ramp toe roller conveyers are stowed

.forward of the right troop door

.aft of each troop door

.on the reverse side of the ramp toes

.on the cargo door

on the cargo door

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The 463L pallets are loaded with the 88” dimension laterally in the logistic restraint rail system

.True

.False

True

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What type of roller conveyer is placed 1” above the floor and is spaced 10” apart?

.Ramp toe

.Bi-directional

.single teeter

.Quad teeter

Bi-directional

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The lock annunciator for pallet position seven is blinking on and off. What does this mean?

.The locks are in transition

.the locks have been activated

the locks have been de-activated

the lock lights need replacing

the locks are in transition

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Which type of roller conveyers allows you to rotate and move pallets laterally on the ramp for entry into the logistic rail system?

.Omni-directional

.Bi-directional

.single teeter

.quad teeter

Omni-directional

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Where are the single teeter rollers located?

.Forward and aft of the ramp

.Aft end of the cargo floor and forward and aft ends of the ramp

.Forward end of the cargo floor and forward end of the ramp

.Aft end of the cargo floor and forward end of the ramp

Aft end of the cargo floor and forward and aft ends of the ramp.

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To which of the following pallet positions does the logistic rail system provide permanent vertical restraint?

. 1 through 9

. 7 through 9

. 1 through 6 and part of 7

.part of 7 and all of 8 and 9

1 through 6 and part of 7

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In which of the pallet positions are the retractable vertical restraint lips located?

.1 through 9

.7 through 9

.1 through 6 and part of 7

.part of 7 and all of 8 and 9

part of 7 and all of 8 and 9

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How many pallets can be carried on the cargo compartment floor?

.14

.18

What is the function of the pallet end stops?

.Prevents cargo from travelling past the forward end of the cargo compartment restraint rails

.Allows you to rotate pallets when loading them into the logistics rail system

.protects the inboard ramp restraint rails during loading operations

.Aids in intial positioning of a pallet while on and off loading pallets

Prevents cargo from travelling past the forward end of the cargo compartment restraint rails.

When the retractable vertical restrain lip is retracted, the annunciator at the forward loadmaster station illuminates

. in the horizontal position

.in the vertical position

. “L”

.the pallet position

In the horizontal position

How many pallet end stops are there in the logistic rail system?

Which component of the logistic rail system is designed to ease the movement of palletised cargo across the cargo floor, ramp and ramp toes?

.Roller conveyors

.Restraint rails

.pallet end stops

.ramp toe guide rails

Roller conveyors

Restraint rails are located on the left right sides of the cargo floor but not on the ramp.

.True

.False

Flase

Use caution when positioning pallets over ____ inches tall into pallet position No.1 of the ADS rail system.

.100

.96

.88

.78

Set the L LOCK SELECT and R LOCK SELECT switches on SAFE for normal air land operations to ensure the locks will not be released.

.True

.False

True

What is the purpose of the ANN/DIG TEST button on the right sidewall control panel?

.Allows you to check the annunciator lights and LED readouts on the right sidewall control panel to make sure they are working.

.Allows you to check the annunciator lights and LED readouts on all control panels on the C-17.

.Allows you to check the annunciator lights and LED readouts on the right sidewall control panel as well as the forward loadmaster station.

.Allows you to check the annunciator lights and LED readouts on the aft left loadmaster station

Allows you to check the annunciator lights and LED readouts on the right sidewall control panel to make sure they are working.

Which of the following is a function of the ADS retractable vertical restraint lips?

.Aids the initial position of a pallet while on/off loading palletised cargo.

.Provides for vertical restraint on the last rail segment on the cargo floor and the segments on the cargo ramp

.Protects the inboard ramp restraint rails during loading operations.

.Prevents pallets from going any further into the C-17 during loading operations.

Provides for vertical restraint on the last rail segment on the cargo floor and the segments on the cargo ramp.

Where are the controls located for the retractable ADS vertical restraint lips on the left side of the ramp?

.Left sidewall control panel

.Right sidewall control panel

.Aft right loadmaster station

.Aft left loadmaster station

Aft right loadmaster station

What is the minimum number of right variable restraint locks for each pallet (weighing 7,801lbs or more) loaded into the ADS rail system?

Which of the following statements in NOT a characteristic of the ADS restraint rails?

.Capable of carrying 11 standard 463L pallets

. Provides restraint to palletised cargo

. Guides palletised cargo throughout the cargo compartment during loading and offloading

.Hsndles pallets with the 88-inch dimension facing forward

Handles pallets with the 88-inch dimension facing forward.

How much restraint do the left pallet locks provide to a pallet loaded into the ADS rail system?

.14,800lbs forward; 7,500 aft

.14,800lbs forward; 15,533lbs aft

.15,533lbs forward; 14,800lbs aft

.20,000lbs forward; 10,000 aft

14,800lbs forward; 15,533lbs aft

The ADS pallet locks located on the ramp are individually controlled from the

.forward loadmaster station

.aft left loadmaster station

.aft right loadmaster station

.right sidewall control panel

aft right loadmaster station

Why is it necessary to turn the sidewall panel control switch to off after the locks have been locked into the ADS rail system?

.To operate LOCK and RELEASE switches on the sidewall control panels.

.To keep switches on the sidewall control panels from being accidentally activated.

.To gang lock all right variable restraint locks on the cargo compartment floor.

To gang lock all pallet locks in the ADS rail system

To keep switches on the sidewall control panels from being accidentally activated.

Where is the ADS restraint rail system located?

.The entire centre length of the cargo compartment floor and ramp.

.The entire centre length of the cargo compartment floor, but not the ramp.

.The left side of the cargo compartment floor as well as the left and right sides of the ramp.

.The right side of the cargo compartment floor as well as the left and right sides of the ramp.

The entire centre length of the cargo compartment floor and ramp.

What is the function of the ADS LOCK STATUS sub panel?

.To select specific right variable restraint locks to gang lock or release.

.To select specific pallet locks for gang lock or release.

.To gang lock or release the ADS locks

.To monitor the status of the ADS locks.

To monitor the status of the ADS locks.

Which of the following actions is taken if the cargo/ADS ISO valve fails to open when the DOOR SYS ARM switchlight is ARMED?

.Reset the circuit breakers.

.Manually open the cargo door and ramp.

.Turn the No.2 AUX pump on and open/close the cargo door and ramp using the individual switches.

.Call the pilots and request DOOR SYS ARM switchlight on the pilots ADS panel be positioned to SYS ARM.

Turn the No.2 AUX pump on and open/close the cargo door and ramp using the individual switches.

The first step in using electrical operations to open the cargo door and ramp with the aircraft on the ground, is to

.pull ADSC and ISO circuit breakers.

move the door switch to open and hold.

.install ADS links.

.establish electrical and hydraulic power.

establish electrical and hydraulic power.

Use AUX system No.1 to establish hydraulic power when using the DOOR/RAMP switch to operate the cargo door and ramp system on the ground.

.True

.False

False

What supports the ramp when lowered to the ground for drive in loading?

.Long ADS links

.Ramp actuators

.Ground support pad

.Stabiliser struts.

Ground support pads

When the cargo door and ramp are open; they provide access to the cargo compartment; closed the form a protective seal to pressurise the aircraft.

.True

.False

True

Which component provides automatic sequencing of the cargo door, ramp, and ramp toes operation?

.Aerial Delivery System Controller.

.Loadmaster forward control panel.

.Pilots ADS control panel

.Stabiliser strut manifold

Aerial delivery system controller

Where are the stabiliser struts located?

.Each side of the fuselage bottom just forward of the ramp at station 1160.

.Just aft of the ramp hinge area.

.Along the outboard edge of the ramp.

.Forward wall of each main landing gear wheel well

Each side of the fuselage bottom just forward of the ramp at station 1160.

The ramp toes can be connected to the ramp in which of the following positions?

.High and Low

.Extended and retracted

.5 degrees and 3.8 degrees

.ground level and horizontal

High and Low

To prevent damage to equipment, ensure _______ in the ramp manual unlock mechanisms, arm assemblies are removed prior to opening the ramp.

.ramp toes

.ditching locks

.ADS links

.quick release pins

quick release pins

Which of the following statements is a function of the cargo door?

.Stows aircraft equipment.

.serves as a loading platform

.allows adjustment position between closed and open

.provides additional storage for selected types of special cargo.

Stows aircraft equipment.

Ensure the _________ is clear prior to extending the stabiliser struts.

.strut door

.cargo door

.ground bearing pad

.ground area

ground area

To prevent damage to the aircraft and prevent injury to personnel

.Ensure the quick release pins in the ramp manual unlock mechanisms are installed.

.Ensure personnel remain well clear of the cargo door, ramp, and ramp toes during open/close operations.

.Ensure ADS links and plugs are installed

.Raise the ramp toes to the pre-load position.

Ensure personnel remain well clear of the cargo door, ramp and toes during open/close operations.

When the control handle is in the EXTEND position and the handle is released, the spring loaded handle will return to the STRUT HOLD position.

.True

.False

True

The DEPLOYED light on the annunciator panel will illuminate only after

.one strut has reached the vertical position

.both struts have reached the vertical position

.the strut doors have opened

.one of the struts has begun to extend

both struts have reached the vertical position

If no further flight activity is scheduled and maintenance is not required

.Instal the nose landing gear downlock safety pins, shut down external power source, remove power cord from aircraft, and open all exits.

.install the main landing gear pins, shut down external power source, remove power cord from aircraft, and close all exits.

.install the nose landing gear downlock safety pins, start external power source, and close all exits.

.Install nose landing gear downlock safety pins, shut down external power source, remove power cord from aircraft and close all exits.

install nose landing gear downlock safety pins, shut down external power, remove external power cord from aircraft and open all exits.

If no further flight activity is scheduled, set all forward and aft loadmaster panel switches to off or inactive status.

.true

.false

true

The loadmaster ensures personnel are clear of all gear access areas prior to stating CHOCKS INSTALLED.

.True

.False

True

Attaching straps or chins around a cargo unit to two adjacent tie down fittings

.decreases the effective value of the strap or chain

.provides restraint in four directions: vertical, forward, lateral and aft.

.doubles the effective value of the strap or chain.

halves the effective value of the strap or chain

doubles the effective value of the strap or chain

When figuring restraint, what is the ratio multiplied by when installing a 10,000lb device and chain to a cargo attachment point with a rating of 7,500lbs?

.2,500lbs

.7,500lbs

.10,000lbs

.17,500lbs

7,500lbs

After installing two symmetrical 25,000 pound tie downs on a unit of cargo, you measure and record the following:
Chain length: 75"
Longitudinal: 60"
Lateral length: 20"
vertical length: 24"
How much vertical restraint is provided?

16,000lbs
20,000lbs
32,000lbs
40,000lbs

16,000lbs

After installing four 25,000 pound chains (2 fwd 2 aft) on a vehicle, you measure and record the following:
Chain length: 75”
Longitudinal: 60
Lateral length: 20”
vertical length: 24”
How much lateral restraint per chain is provided?

6,500lbs
6,665lbs
13,000lbs
13,330lbs

13,330lbs

What plan angle is between the chain and a line which runs fore and aft in the cargo compartment through the attachment point?

Vertical

Lateral

Horizontal

Longitudinal

Damage may occur if cargo tiedown that spans from the main floor to the ramp is not _________ or sufficiently slackened.

added

tightened

removed

loosened

removed

After installing two symmetrical 25,000 pound tie downs on a unit of cargo, you measure and record the following:
Chain length: 75”
Longitudinal: 60”
Lateral length: 20”
Vertical length :24”
how much longitudinal restraint is provided per chain?

6,667lbs
8,000lbs
10,000lbs
20,000lbs

20,000lbs

The minimum restrain criteria for aft or lateral is _____Gs

1.5

The minimum restraint criteria for vertical is ______Gs.

2.0

To ensure proper restraint is provided, cargo tie downs should be attached

Asymmetrically in pairs

symmetrically in pairs

only when the aircraft is flying

loosely to soft pieces of cargo

symmetrically in pairs

Damaged hazardous material to be loaded will be

Accepted if damage is minimal

accepted as is

refused

repaired and shipped

refused

During tactical and contingency procedures, when may DOT-5L jerri cans be used to transport vehicle fuel?

When the jerri cans are loaded and secured in the bed of an approved vehicle

when the total combined fuel quantity does not exceed three times the capacity of the items fuel tank

when drained to the greatest extent possible

when each jerri can is at least 1/2 full but no more than 3/4 full

when drained to the greatest extent possible

Shipments of hazardous materials for military airlift may be certified by

any trained technical specialist

any individual designated by the installation or activity commander

a technician trained IAW AFMAN 24-204 and designated in writing by the commander

a technician trained IAW AFMAN 24-204 only

a technician trained IAW AFMAN 24-204 and designated in writing by the commander

If hazardous materials such as biological agents must be jettisoned, what is the minimum distance required from shore of the jettison?

10 miles

12 miles

25 miles

50 miles

12 miles

Do not transport hazardous cargo aboard aeromedical flights. The field commander may allow casualties on hazardous cargo flights in extreme circumstances that may result in potential loss of life.

true

false

true

A single shippers declaration for dangerous goods will be used for multiple like items shipped under one TCN

true

false

true

For safety reasons, aircraft carrying certain materials such as DoD class or division 1.1 and 1.2 explosives are normally parked in areas isolated from non- associated personnel and facilities.

true

false

true

For safety reasons, aircraft carrying certain materials such as DoD class or Division 1.1 and 1.2 explosives are normally parked in areas isolated from non-associated personnel and facilities.

True

False

True

For safety reasons, aircraft carrying certain materials such as DoD class or Division 1.1 and 1.2 explosives are normally parked in areas isolated from non-associated personnel and facilities.

True

When using the segregation table for hazardous materials to determine the compatibility of hazardous items for air shipment , what does an ‘O’ at the intersection of two classes on the chart indicate.

The items are ok to ship together

The items may be shipped together but must be separated by 88 inches in all directions

The items must be positioned in an open area of the cargo floor

The items may be shipped together if in the opinion of the aircraft commander they do not present a significant risk.

The items may be shipped together but must be separated by 88 inches in all directions

Labelling requirements for hazardous materials do not apply during tactical and contingency procedures

True

False

The cargo compartment has a constant loadable width of _____ inches at approximately 2 inches above the floor

181

216

298

347

216

Suppose you are loading a vehicle with a 235 inch wheelbase, an overhang of 90 inches and a ground clearance of 20 inches. considering ground contact, what is the maximum ramp hinge height for the item to be safely loaded without shoring?

cannot be loaded without shoring

70 inches

68 inches

66 inches

70 inches

If a truck being driven on has a ground clearance of 15 inches and a rear overhang of 100 inches, how far forward from FS1165 must the rear wheels be moved so that the ramp can be safely closed?

89 inches to FS 1076

44 inches to FS 1121

24 inches to FS 1141

16 inches to FS 1149

When are spotters required, as far as height, when loading cargo forward if FS937

148 inches

138 inches

128 inches

118 inches

148 inches

Compartment E has a maximum single axle floor limitation of___________ pounds

15000

22000

27000

36000

Can this vehicle be loaded into compartment D?

Articulating track
weight 24,500 lbs 
10 wheels 
pad area 18 square inches 
9.5 feet track length 
18 inch track width

yes

Consider two axles parked side-by-side in cargo compartment E. If axle weighs 19,000lbs, the maximum weight of axle B is _____ pounds.

18,000

20,000

20,500

21,000

20,500

Can a non-articulated (rigid) suspension vehicle be loaded across area B if it weighs 62,000 lbs and has an 18 inch wide track?

yes

What is the PIW for a non-articulating track vehicle that weighs 72,000lbs and has a 16 inch track width?

2,250 PIW

2,750 PIW

3,000 PIW

3,250 PIW

2,250 PIW

calculate PLF (lbs per linear foot)

weight 24,500
10 wheels 
18 square inch pad area
9.5ft track length 
18 inch track width

2,579 PLF

calculate psi of pad area

weight 24,500
10 wheels 
18 square inch pad area
9.5ft track length 
18 inch track width

137 psi

what is the maximum allowable weight that can be loaded in compartment F?
30,000

35,000

72,000

170,900

35,000

What is the PIW for a non-articulating track vehicle that weighs 72,000lbs and has a 16 inch track width?

2,250 PIW

2,750 PIW

3,000 PIW

3,250 PIW

2,250 PIW

max centreline axle weight in compartment D?

20,000

22,000

25,000

27,000

When are bogie axles considered side by side?

when the axle spacing is less than 42 inches

when all axle centroids are within 8 feet of each other

when the single axle limits do not apply

when the axle is parked next to a tracked vehicle

when all axle centroids are within 8 feet of each other.

The PIW limitation for both inflight and on/offloading for this tyre is

axle with two tyres weighs 13,000lbs
inflation pressure 110psi
tyre pad dimensions 10 in x 9 in.

840/1186

What is the PIW?

weight 24,500
10 wheels 
18 square inch pad area
9.5ft track length 
18 inch track width

137 PIW

Given the information on the right, compute the wheel weight.

weight 24,500
10 wheels 
18 square inch pad area
9.5ft track length 
18 inch track width

2,450lbs

The tyre contact PSI is?
axle with two tyres weighs 13,000lbs
inflation pressure 110psi
tyre pad dimensions 10 in x 9 in.

73 psi

The PIW limitation for both inflight and on/offloading for this tyre is

axle with two tyres weighs 13,000lbs
inflation pressure 110psi
tyre pad dimensions 10 in x 9 in.

840/1186

How many classes of hazardous materials have been established under the United Nations system?

Nine

Eight

Seven

Six

Nine

The _____ weight is determined by the operating weight plus the total cargo weight

Zero fuel

Total aircraft

Takeoff

Landing

Zero Fuel

The supplemental weight and balance handbook contains which of the following technical orders?

TO C-17A-1

TO 1C-17A-5-2

TO 1-1B-50

TO 1C-17A-9

TO 1C-17A-5-2

Which configuration allows for 11 pallets to be loaded using the ADS rail system and 54 seats along the sides of the cargo compartment?

C-1

C-2

CP-1

P-1

C-1

When you add total passenger/cargo weight and moments (Ref 15) to the operating weight and moments (Ref 9) you will have determined which of the following weights?

Zero Fuel

Total Aircraft

Takeoff

Landing

Zero Fuel

When you add operating weight (Ref 9) and Takeoff fuel (Ref 10) you have determined which of the following weights?

Takeoff

Zero Fuel

Total Aircraft

Landing

Total Aircraft

The three allowable gross weights that are entered in the limitations block on DD form 365-4 are found in which publication?

TO 1C-17A-1

TO 1C-17A-9

MCI 11-204

AFI 11-2C-17, Vol 3

Which of the following publications contains two tables which list the equipment that is stowed on the C-17?

AFI 11-2C-17, Vol 3, Addenda A

AMCI 11-208

TO 1C-17A-5-2

TO 1C-17A-1-2

AFI 11-2C-17, Vol 3, Addenda A

This tyre require parking shoring?

axle with two tyres weighs 13,000lbs
inflation pressure 110psi
tyre pad dimensions 10 in x 9 in.

false

this tyre can be airlifted without shoring?

2 airless tyres axle weight 6000lbs
tyre pad 6.5in w x 8in long.

true

Regardless of where the units are placed in the aircraft, vehicles may be transported with fuel in the tanks not to exceed ________ full unless the item is being transported under authority of AFMAN 24-204, chapter 3.

one quarter

one half

two thirds

three quarters

one half

A trailer has forward support weight of 500 pounds and a rear axle weight of 2200lb, wheelbase is 99in. What is the CG?

wheeled items weighing _______ pounds or more shall be marked with individual axle weights.

2000

3500

5000

7500

2000

What is the rear axle weight of a vehicle that weighs 6200lbs, the centre of gravity from the front axle is 85in, and the wheelbase is 110

4591

4691

4791

4891

4791

Using the fuel moment w/o ER table in TO 1C-C17A-5-2 compute the moments for takeoff fuel weight of 98000 pounds. Both outboard tanks contain 24000 pounds and both inboard tanks contain 25000 pounds.

7800

8724

8832

8840

8832

To compute operating weight compute the weight of the aircraft

properly configured and ready to fly without fuel

plus trapped fuel and some miscellaneous equipment

properly configured and ready to fly without fuel or cargo

properly configured and ready to fly plus cargo and fuel

properly configured and ready to fly without fuel or cargo

Permissible centre of gravity ranges for takeoff and landing are found in which publication

AMCI 11-208

AFI 11-2C-17 Vol 3

TO 1C-17A-9

TO 1C-17A-5-2

The maximum ramp gross weight is

440200

442200

582000

586000

Which of the following publications contain basic cargo compartment configurations used in completing DD form 365-4

TO 1C-17A-1

TO 1C-17A-5-2

AFI 11-2C-17, Vol 3, Addenda A

AMCI 11-208

AFI 11-2C-17, Vol 3, Addenda A

Pallet trains joined on the ____ inch side require you to use the ADS rail system

108

What should be placed in positions where they can be easily jettisoned

Vehicles

Pallets with hazardous cargo

Pallet trains

Mail pallets

Pallets with hazardous cargo

When carrying passengers maintain a ___ inch space between palletised cargo restrained with nets or straps and the nearest occupied seat forward of the cargo

Palletised cargo weighing 10000 pounds secured with side and top nets cannot exceed ___ inches in height from the surface of the pallet

100

Each bi directional roller has a load capacity of ___ pounds

1000

1500

2000

2500

2000

Refer to the floor limitations chart to TO 1C-17A-9. Which cargo compartment is capable of carrying the entire capacity

After sequencing your cargo load, the next step in determining whether or not this sequence will work is to compute

takeoff gross weight

zero fuel gross weight

takeoff CG

combined load CG

You compute the combined load CG by dividing

the operating weight by the operating moment

the total payload moment by the total payload weight

the operating moment by the operating weight

the total payload weight by the total payload moment

the total payload moment by the total payload weight

Where are the pallet identifiers attached on 463L pallets loaded with cargo

only on the 88 inch side

only on the 108 inch side

on the 88 inch and the 108 inch side

on the 108 inch side and top

on the 88 inch and the 108 inch side

The loadmaster must ensure the area is free of obstacles prior to closing the door and ramp.

True

False

True

What should be worn when configuring logistics rails to prevent injury

goggles

gloves

ear plugs

headset

gloves

On/off loading cargo is permissible during refuelling operations with reference to 1C-17A-2-10JG-30-1

True

False

True

Restraint locks shall not be used as pallet/platform stops

True

False

True

Failure to position the winch MODE switch in the OFF position could result in

cargo winch failure

inadvertent movement of the retriever winch

operation of the no 3 hyd system

inadvertent movement of the winch cable

Prior to offload operations, the loadmaster should brief the loading crew members on duties to be accomplished and hand signals to be used

True

False

True

FAW 4250
RAW 3860
RAA 206 in
CoG?

98in

FAW 12100
IAW 9300
RAW 9300
IAA 190in 
RAA 250in

CoG?

133in

In certain instances, units which are susceptible to fuel spills or leakage can be carried if they are drained and capped?

True

False

True

Under certain conditions, on/offloading cargo is permissible during fuelling operations

true

flase

true

When vehicles/items are loaded onto the ramp for flight, the _______ must be toward the higher end of the closed ramp

fuel filler cap/spout

fuel lines and tank

engine manifolds

exhaust pipe

fuel filler cap/spout

Why must exhaust fans be used when loading vehicles?

to prevent buildup of carbon monoxide fumes

to reduce aircraft fire hazard

to prevent overheating of the cargo compartment

to provide emergency exiting

to prevent build up of carbon monoxide in the cargo compartment

When cargo is positioned on the ramp for flight, ensure the cargo is restrained in at least one direction prior to raising the ramp.

True

False

false

DOT-5L jerricans may only be shipped drained

true

false

true

If more than one layer of shoring is required during the offload, the vehicle will be winched off the aircraft

true

false

true

What can be used to help eliminate fumes when loading vehicles?

portable electric fans

cryogenic vents

aircraft air conditioning

oxygen scrubber

aircraft air conditioning system

Inspect the backside of the axles and structures for the presence of hydraulic lines or electrical cables before attaching ________ around these hidden areas.

loading aids

shoring equip

safety nets

tiedown chains

What should be used to load vehicles if slippery ramp conditions exist?

K Loader

cargo winch

forklift

personnel

cargo winch

The M-149A2 ______ are certified for airlift with liquid in the tanks

fuel trailer

POL trailer

water trailer

halon trailer

water trailer

connection of low temperature exhaust to a _______ contaminated with oil or grease may cause an explosion

rubber hose

muffler

baffle

vent

When the aircraft has been cocked, it should be closed and sealed.

true

false

true

The alert start procedures provide for engine start and ready the aircraft for launch within _____ minutes after aircrew arrives at the aircraft.

For buddy start, the donor aircraft should use engine No. _____ to provide the pneumatic source

1 or 4

2 or 4

2 or 3

1 or 2

While the aircraft remains in a sealed condition, the FCC and SCEFC preflight test remains valid for _____ hours or until alert launch

If a specific fault code is not available, the general fault code is usually

-00

The fault code listing provides the flight crew a concise description of the fault for entry into aircraft forms

true

false

true

The maintenance tasks the aircrews are authorised to perform are listed in

AFI 11-202

AFI 11-217

AFI 11-2C-17, VOL. 3, CHAP 17

AFI 11-2C-17, VOL 3, CHAP 12

When would a crew member be required to perform maintenance support tasks?

When required for mission accomplishment

Crew members are always required to perform maint. tasks

crew member never perform maint. tasks

maint. pers. perform main. tasks at home stn only.

when required for mission accomplishment

personnel exiting via the ramp will proceed aft of the aircraft at least _____ feet before turning and 200 feet before stopping.

Uring on/offloading, if a thrust reverser will not extend, consideration should be given to ______ the affected engine

idling

shutting down

restarting

checking

shutting down

Engines will be placed into reverse idle prior to the _____ giving clearence for on/offloading operation.

aerial port pers.

CRG pers.

LOADM

pilot

Unless cargo size and location require otherwise, always offload cargo before passengers

true

false

The ________ will be stowed and the ramp will be raised to at least the coplanor position before taxiing

ramp rollers

winch

sidewall seats

stab struts

After the aircraft is slowed to taxi speed, you may remove all vehicle tie downs except

two on opposite sides

one forward and one aft

one forward and two aft

one side and one aft

one forward and one aft

DD form 365-4, weight and balance, is not required when

loading passengers only

load is loaded exactly according to load plan

downloading to an empty aircraft

only carrying a through load

downloading to an empty aircraft

When engines are running, you may not onload or offload through the crew entry door and cargo ramp door at the same time unless both doors are supervised by a c17A qualified crew member.

true

false

true

With exception of small arms ammunition, hazardous division 1.4, do not ERO _______ unless authorised by mission directive

mail

explosive cargo

ground troops

passengers

explosive cargo

The operational stop checklist used when performing ERO procedures is found in

TO 1C-17A-9

AMCI 11-217

LOADM reference manual

TO-1C-17A-1

TO-1C-17A-1If a combat offload is to be accomplished before offloading vehicles, do not remove ________ until after the combat off load is complete.

restraint

headphones

oxygen mask

goggles

Using the load shift formula, compute the following
load 80,000lbs, CG change in inches if 20,000lbs are moved from station 500 to station 600

25 inches

30 inches

48 inches

52 inches

25 inches

In general, you should always plan to position the heaviest unit(s)

on the ramp

near the desired load CG

near the front cargo compartment

near the rear of the cargo compartment

near the desired load CG

According to the CG envelope graph W/O ER in TO-1c-17a-5-2, what are the forward and aft CG stations for 140,000lbs

FS 400 and FS1100

FS550 and FS 1050

FS700 and FS1000

FS800 and FS 920

FS 800 and FS920

Using the load shift formula, compute the following: With a total cargo weight of 90,000lbs, how much weight must be moved from FS800 to FS720 to move the load CG 40 inches?

32,000

40,000

45,000

51,000

45,000

What is LEMAC on the C-17?

793.6

If an aircraft has a zero fuel weight of 326,220 and a zero fuel moment of 29,539 what is ZFW MAC?

36.2

What is MAC on the c17?

309.5

With a ZFW of 400,000 and a ZFW MAC of 39.0 an aircraft is within the ZFW envelope limitations?

true

false

true

If the total weight of a load is 96,221lbs and the total load moment is 7,957, what is the load CG?

750

782

827

872

827

Personnel will wear _____ when handling the winch cable

ear pro

gloves

knee pads

eye pro

gloves

Using table 4E-1 in TO 1C-17A-9, compute the correct cable configuration to load a 32,000lb load on skids on a non-skid surface up a 3.8 degree incline

single line

double line

triple line

quadruple line

winch cable used with aircraft snatch blocks have a maximum diameter of ______ inch.

1/8

3/8

1/5

3/8

The rotary knob on the winch control panel controls both direction and speed at which the winch will operate

true

false

true

Ensure the winch cable sheave is in alignment with the ________, properly routed through the __________ and will not interfere with other items.

cargo ramp; steering yoke

cargo ramp; snatch blocks

devices; tie down chains

cable pull; snatch blocks

When winching a load on a level surface, a triple line configuration will provide ______ pounds of cable pull

15,000

22,500

30,000

40,000

22,500

The ORIDE switch on the cargo winch control panel

establishes electrical power

establishes hydraulic power

overrides the winch control panel

overrides the remote winch control

replace winch cable if ______ or more broken wires per strand inch

If there is a delay while winching cargo up the ramp/ramp toes, use ________ to secure the item.

wheel chocks

the winch cable

chain type devices

the parking brakes

chain type tie downs

A 28,000 pound load on dry shoring can be winched up a 3.8 degree incline with a double line configuration.

true

false

Less cable pull is needed to winch cargo on a level surface as opposed to an inclined surface.

true

false

true

Using Table 4E-1 in TO 1C-17A-9, compute the cable configuration needed to load a 56,000 pound vehicle rolling on tracks up a 15 degree ramp angle.

single

double

triple

quadruple

triple

A skidded item of cargo being pulled across the cargo ramp is an example of _________ friction.

parking

rolling

rotating

sliding

Internal winching utilises the

RWC or winch control panels

external winching source

self-winching source

vehicle winching source

RWC or winch control panels

The cargo winch is powered

electrically

hydraulically

manually

pneumatically

hydraulically

When in operating position, the cable guide sheave allows the cable to extend ______ above the floor

.5 in

0 in
5 in
0 in

1.0 in

Which of the following components is used to select and set remote cargo winch controller operating frequencies

Receiver/Transmitter radio

cargo winch control panel

intercommunication system panel

aircraft high frequency radio

Receiver/Transmitter radio

When operating the cargo winch in the low speed and using a single line cable configuration, the winch is limited to ___________ pounds of pull.

5000

5500

7000

7500

The remote cargo winch controller is stored

in the cargo door storage compartment

at the forward loadmaster station

at the left aft loadmaster station

on the sure-comm rack

An item of cargo weighing 68,000lb with hard rubber wheels would require a _______-line configuration in order to be winched up a 15-degree angle

double

triple

quadruple

quintuple

quadruple

When moving the loading vehicle in which direction should the driver turn the wheel

the drivers left or right

the direction of cargo ramp toes

the opposite direction of guides extended hand

the direction of guides extended hand

Top nets may be used to totally restrain low profile cargo not exceeding ____ pounds

1500

2000

2500

3000

2500

Damage to the aircraft ramp will occur if ____ are not configured the same for both sides

ADS links/plugs

guide rails

ramp toes

roller conveyors

ADS links/plugs

Suppose a concentrated load weighs 5670 pounds and is supported on 4 skids, each 4 inches wide by 10 inches long. The skids are more than 12 inches apart. According to the figure ‘concentrated floor loads - calculations’ sheet what is the max PIW for this load

708

670

624

595

624

Rough runway surfaces may damage the cargo ramp during combat offload operations, to prevent this damage,

the loadmaster will offload only one pallet at a time

the loadmaster will raise the ramp slightly

the aircraft commander will reduce forward taxi speed

the aircraft commander will request a marshaller to direct the taxi

the aircraft commander will reduce forward taxi speed

When conditions warrant, the ____ may authorise combat offloading

PIC

Loadmaster

MAJCOM/A3/DO or DIRMOBFOR

ABCCC

MAJCOM/A3/DO or DIRMOBFOR

The combat entry checklist can be found in

AFI 11-218

AFI 11-401

AFI 11-2C-17, Vol 3

TO 1C-17A-1 and TO 1C-17A-1CL-2

Ensure roller conveyors are configured as appropriate for intended offload. As a minimum _____ immediately forward of all combat offload pallets will be raised/extended.

the buffer stop assembly

rails, rollers and two pairs of locks

rollers and one pair of locks

rails and rollers only

rails, rollers and two pairs of locks

Without approval of MAJCOM/A3/DO, excluding hazardous division 1.4 ____ shall not be combat offloaded unless rigged for airdrop

vehicles

explosives and ammunition

animals/fowl

personnel

explosives and ammunition

The combat exit checklist is initiated by the loadmaster

True

False

Registered mail may contain up to and include ____ material

top secret

secret

radioactive

in bond

secret

If approved by the aircraft commander, an enlisted crew member at the rank of ____ or above can be a courier

What should happen if you find damaged classified shipments

Annotate discrepancy on manifest

refuse shipment at originating destination

carry cargo and let next destination know about problem

let aircraft commander make a decision on what to do

refuse shipment at originating destination

Normally human remains will be placed at the front of the cargo compartment, but if this is not possible, human remains may be loaded towards the rear of the aircraft in the C-17 because

cases can be moved from one side to the other in the event jettisoning is required

cases can be moved from forward to aft in the event jettisoning is required

cases are easier to unload when they are in the aft section of the cargo compartment

they must be loaded aft to satisfy the ‘head higher than feet’ requirement

cases can be moved from one side to the other in the event jettisoning is required

Whole blood must be maintained at a temperature of ____ degrees fahrenheit

32-80

32-70

34-90

35-80

what is the maximum number of human remains transfer cases that could be loaded on a 463L pallet

During unscheduled stops crew members may place courier material in temporary custody of

any squadron commander

army personnel

US military guards

maintenance supervisor

US military guards

The special handling data/certification form is the

DD form 1873-1

DD form 1387-2

AF form 175

AF form 120

DD form 1387-2

who may sign for classified shipments and take custody of them?

only US military and US civillians with appropriate security clearance

pilot not flying

any air freight personnel

aircraft crew chief

only US military and US civillians with appropriate security clearance

what is used to provide a complete record of all cargo or mail aboard the aircraft on a flight or mission

AF form 127

DD form 1387-2

cargo manifest

label

cargo manifest

when checking oil quantity verify on the MFD that each engine has a minimum of

20 quarts

15 quarts

12 quarts

10 quarts

20 quarts

minimum unpressurised reservoir quantity for safe auxiliary pump operation are ___ quarts for system no 2 and ___ quarts for systems no 1, 3 and 4

8/15

16/12

12/16

18/12

16/12

during icing conditions remove the inlet covers as soon as possible after arriving at the aircraft

true

false

the maximum vertical height of load to be jettisoned is ____ inches measured from the top of the pallet/platform

110

115

118

120

118

During the tailpipe fire procedures it may become necessary to use a ground fire extinguisher. this should be accomplished

immediately

as a last resort

only by fire department personnel

only by maintenance personnel

as a last resort

do NOT approach or stand near a known or suspected hydraulic leak area if the system is pressurised. Fluid under high pressure is extremely dangerous and will cause serious personnel injury if it

penetrates the skin

gets on your flight suit

makes your boots slippery

gets in your hair

penetrates the skin

during ground operations you have been using had system no 2 without any engines running. The hydraulic QTY LOW light illuminates. You should conclude that you have

low temperature in system 2

asymmetric slats

failure of ADSC isolation valve

loss of fluid in system 2

when the loadmaster states ‘locks released’ this is a signal for the pilot to

increase the deck angle to ensure pallet/platform/container movement

decrease the deck angle to ensure pallet/platform/container movement

maintain straight and level flight

close the cargo door and ramp

increase the deck angle to ensure pallet/platform/container movement

Engine running ground operations with a pylon fuel leak may result in an engine fire and damage to the aircraft if the fire handle for the associated engine is not pulled

true

false

true

A controllability check should be confirmed if CG cannot be maintained within limits

true

false

true

nonpalletized wheeled vehicles should not be jettisoned under emergency conditions

true

false

true

Above 20000 feet, fuel ___ may cause engine flameout due to loss of fuel pressure

dump

transfer

crossfeed

venting

dump

The loadmaster will don and connect a restraint harness or parachute prior to opening the troop doors or the cargo door and ramp from the aft loadmaster station

true

false

true

The ____ checklist MUST always be accomplished if smoke is filling the pressurised portion of the aircraft

electrical fire and smoke

fuselage fire and smoke

fumes suppression

smoke/fumes in the aircraft

Do not shift cargo in flight except when necessary to maintain aircraft control

true

false

true

The MASTER CAUTION, LOOP cue and APU LOOP A lights are on. The APU LOOP A is turned off and LOOB B is tested. All LOOP B switchlights illuminate indicating LOOP B works. What does this mean?

APU is on fire and should be shut down

LOOP B is faulty and should be selected to the OFF position

the system has malfunction and is unreliable

Loop A is faulty and no fire exists

If the MASTER CAUTION light, the loop cue on the WAP and a single amber LOOP light illuminates, it could be an indication of a

fire warning, but not a loop malfunction

loop malfunction or a fire warning

loop malfunction, but not a fire indication

loop malfunction during loop testing

loop malfunction or a fire warning

Time and conditions permitting, circuit breaker actions should be performed by the loadmaster or by a qualified crew member

true

false

true

If you receive an unsafe gear indication, but visual inspection confirms the gear to be down and locked, the unsafe indication may be disregarded

true

false

true

the lowering both main landing gear on one side, which gear is lowered first?

aft gear

forward gear

both at the same time

no order specified

forward gear

what actions should be performed if brakes overheat during a high energy rejected takeoff

set parking brakes and evacuate aircraft

keep aircraft on runway, set parking brake, notify ground crew, check nose wheels, approach overheated brakes from the side

edit the aircraft, check nose wheels, and approach the brakes from the side to inspect the damage

taxi the aircraft clear of the runway, notify tower of emergency, do not set parking brakes, chock nose wheels, monitor brake temp

If the stab strut doors are open and/or the stab struts are deployed, a landing can be safely made

true

false

true

The possibility of engine or system failures should be considered for each takeoff. The pilot flying should thoroughly brief the crew regarding go/no go criteria

true

false

true

If a gear malfunction occurs while lowering the gear, recycle the gear

true

false

During the ground evacuation (engines not running) procedure, if flammable and/or explosive materials are onboard these items should be offloaded first to prevent spread of the fire and/or onboard explosions

true

false

true

For any gear malfunction, visually inspect the affected gear to confirm damage or proper alignment of red fluorescent band on down lock links

true

false

true

Proximity sensors can be affected by local Electromagnetic interference (EMI) when equipment located near the sensor experiences a failure

true

false

true

If the MASTER CAUTION and ENTRY DOOR on the door annunciator panel light illuminate, and your aircraft is in the local traffic pattern

prepare for emergency landing

prepare for bailout

complete the door warning (in flight) checklist

complete the loss of pressurisation checklist

complete the door warning (in flight) checklist

During the ground evacuation (engines not running) procedure, if conditions permit, shut down the APU, external power and battery systems

true

false

true

The aircraft should be scanned before starting any emergency decent requiring airspeed increase

true

false

true

what is the ramp toes contact ratio of a vehicle if it has an overhang of 90 inches and ground clearance of 19 inches

4.8

what is the maximum allowable in flight ramp loadable height of a vehicle when its highest point is positioned at FS 1260

150 inches

140 inches

130 inches

120 inches

140 inches

Determine the maximum ramp hinge height for a vehicle loaded inboard of x = + 82, with a projection of 100 inches, a 350 inch wheelbase and a height of 140 inches

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