C17 CBT Flashcards
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
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.
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
When in the vicinity of an operating APU, you should wear
.Ear protection
.Eye protection
.Protective clothing
.Hard hat
Ear protection
Which switch is used for a normal APU start
.START CONTR switch
.MODE SEL switch
START CONTR switch
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.
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
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
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
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
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
During APU start and operation, the exhaust does not represent a personal hazard.
.True
.False
False
How close to the fire should you position the hand held fire extinguisher?
.12 feet
.8 feet
.4 feet
.2 feet
8 feet
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
The transmission lines for the FEDS are arranged so that any ________ initiator(s) can fire all four hatches.
.one
.two
.three
.four
One
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
Ramp blowdown may not function if the weight on the ramp exceeds _______ pounds.
.20,000
.20,750
.25,000
.40,000
20,750
How many fire extinguishers are located on the aircraft?
.four
.six
.eight
.nine
Nine
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.
When CBrC1F2 decomposes, It can be hazardous. It can be recognised by its_________odour.
.very sweet
.sharp, acrid
.rotten eggs
.pleasant
Sharp, acrid
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
How many Emergency Escape Breathing Devices are on the C-17?
. 7
.6
.5
.4
6
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
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.
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
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
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.
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
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
Of the eight ground egress exits on the c-17, how many are equipped with escape ropes?
.3
.4
.5
.6
6
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
Do not use external power with the battery switch OFF.
.true
.false
True
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
80
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
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
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
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)
The normal operating configuration for the electrical system is ____________ mode.
.split-isolated mode
.isolated
.parallel
.split-parallel
Split parallel
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
When using the DC electrical system, the _________ configuration is the normal mode for operation.
.split parallel
.conversion
.isolated
.parallel
Split parallel
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
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.
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
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
Which generator buses are the normal sources of power for the battery chargers?
.2&3
.1&2
.1&4
.2&4
1&4
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
As a minimum, aircraft batteries can supply emergency power up to _________ minutes
30
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
A mishap that has a fatality or permanent total disability is a class __________ mishap
.A
.B
.C
.D
A
All vehicles must approach parked aircraft with the vehicles _______ toward the aircraft
.front end
.right side
.back end
.operators side
Operators side
When working on or around aircraft, _______ will not be worn
.earplugs
.contact lenses
.gloves
.rings
Rings
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
The speed limit for vehicles within 25 feet of the aircraft is ______ MPH
.5
.10
.15
.20
5
Smoking is not permitted on the flight line except in designated areas and never closer than _______ feet to the aircraft.
.25
.50
.75
.100
50
When in the vicinity of an operating APU, ________ protection should be worn.
.eye
.ear
.head
.foot
Ear
The speed limit for the aircraft parking ramp is ________ MPH
.10
.15
.20
.25
15
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
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
The warning and caution annunciation panel
.displays visual warning, caution, and advisory messages for various systems throughout the aircraft.
.automatically prioritises messages as received
.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
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
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
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
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
An improperly secured ladder poses a threat to
.Loadmaster
.Pilot
.copilot
.personnel seated underneath the ladder.
personnel seated underneath the ladder
When the troop door is checked, ensure the door is closed and locked and the DOOR NOT LOCKED annunciator is illuminated
.true
.false
False
The oxygen shutoff valve at the forward loadmaster station will be closed only for an emergency action or for flight.
.True
.False
False
An electrical shock is possible when installing/removing a defective hot cup if the cup timer is powered
.True
.False
True
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
Stowage of equipment on the aft bulkhead of the cargo door is prohibited
.true
.false
TRUE
An unsecure IV post may rapidly slide from the stanchion during _______ and strike personnel seated in sidewall seats
.Landing
.Approach
.Takeoff
.Taxi
Takeoff
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
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
When the STAB STRUT ACTUATORS circuit breaker is pulled, the STRUT DOOR light on the DOOR?STATUS panel will illuminate
.True
.False
False
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
Which lights are controlled from the forward Loadmaster station?
.Cargo compartment
.Galley
.Lavatory
.Ramp and Door
Cargo compartment
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
The nacelle scanning lights are located on the upper surface of each wingtip
.True
.False
False
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
The stowage compartment and ________ light switches are located on the crew entry light panel
.galley panel
.stairway
.forward loadmaster station
.forward aisle
forward aisle
Two rotating beacons are called _____ lights
.anti collision
.landing/taxi
.runway turn off
.wingtip landing
Anti-collision
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
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
The emergency evacuation lighting is enabled in all positions of the MODE SELECT switch
.True
.False
True
The OXYGEN CONTROL panel backlights are inhibited in the SECURE mode
.True
.False
True
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
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
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
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
The primrary source of oxygen for the crew system is ________ liquid oxygen converter(s)
. One 25Litre
.One 75Litre
.Two 25Litre
.Two 75Litre
one 25Litre
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
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
The oxygen control panel for the passenger/auxiliary oxygen system is located at the _______ loadmaster station
.forward
.instructor
.aft left
.aft right
forward
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
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.
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
The normal pressure for the passenger oxygen system is
.150-300psi
.200-375psi
.250-430psi
.285-430psi
285-430psi
The passenger oxygen system contains one ______ litre converter and one _______ litre auxiliary converter.
.75;75
.75;25
.25;75
.25;25
75;75
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
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.
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.
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
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
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.
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
The engine-driven hydraulic pumps provide continuous hydraulic pressure of _______ Psi
.4000
.4,200
.4,500
.5,000
4,000
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
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
The manifold fail annunciation and ilimunation of the MANIFOLD FAIL light indicates a failure of what system
.Hydraulic
.Bleed air
.Electrical
.Fuel
Bleed air
pressing the AVIONICS COOL ORIDE switchlight to OPEN drives the avionics augmentation valve and the avionics cooling outflow valves open.
.True
.False
True
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
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
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
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
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.
Because avionics cooling is critical prompt corrective action is required.
.True
.False
True
When flying through contaminated airspace, the air used for avionics cooling will be
.shut off
.purified
.contaminated
.circulated through all compartments
contaminated
The isolation valve divides the manifold into the left and right side.
.True
.False
True
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
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
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
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
A thin coating of frost is permitted on the fuselage, provided _______ are visible.
.Crew chiefs
.antennas
.lights
.lettering/paint lines
lettering/paint lines
If an engine has been cold soaked for an extended period, white smoke may appear during start.
.True
.False
True
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
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
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
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
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
visible moisture includes
.rain
.snow
.sleet or ice crystals
.all of the above
all of the above
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
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
Hydraulic transfer pump inadequate pressure output may occur at ambient temperatures colder than
.20C
.20F
.0F
.0F
0F
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
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
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
Pallets are solid aluminium pallets with tie down rings
.True
.False
False
The maximum single pallet weight for cargo secured with nets and stacked over 96” shall not exceed 8,000 pounds
.True
.False
True
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
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
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
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.
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
The 463L pallets are loaded with the 88” dimension laterally in the logistic restraint rail system
.True
.False
True
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
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
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
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.
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
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
How many pallets can be carried on the cargo compartment floor?
.4
.7
.14
.18
14
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?
.1
.2
.4
.6
4
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
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?
.1
.2
.3
.4
2
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
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
- 0
- 5
- 0
- 0
1.5
The minimum restraint criteria for vertical is ______Gs.
- 0
- 5
- 0
- 0
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
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
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
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
no
no
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
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
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?
81
82
83
84
81
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
TO 1C-17A-5-2
The maximum ramp gross weight is
440200
442200
582000
586000
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
60
88
96
108
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
24
30
48
60
30
Palletised cargo weighing 10000 pounds secured with side and top nets cannot exceed ___ inches in height from the surface of the pallet
60
88
96
100
96
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
D
E
F
G
E
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
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
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
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
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.
5
10
15
20
15
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
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
24
36
48
72
72
If a specific fault code is not available, the general fault code is usually
- 00
- 11
- 000
- 111
-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
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.
25
35
45
50
25
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
pilot
Unless cargo size and location require otherwise, always offload cargo before passengers
true
false
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
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
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?
- 1
- 5
- 6
- 9
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?
- 2
- 5
- 8
- 6
36.2
What is MAC on the c17?
- 7
- 5
- 5
- 6
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
quadruple line
winch cable used with aircraft snatch blocks have a maximum diameter of ______ inch.
1/8
3/8
1/5
1
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
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
overrides the remote winch control
replace winch cable if ______ or more broken wires per strand inch
3
4
6
7
4
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
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
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
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
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
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
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
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
E8
E7
E6
E5
E5
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
35-80
what is the maximum number of human remains transfer cases that could be loaded on a 463L pallet
9
10
11
12
12
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
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
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
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
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
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
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
- 2
- 5
- 8
- 6
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
68
70
72
74
74
