This Quiz will help prepare you for any up comming Test for the C-17A Engine Run Test
Pushed In
Pulled Out
Pulled Out and Rotated
Rotated in any direction
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Person A
Person B
Person C
Pro-Super
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True
False
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True
False
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Pseudo hyper valve system
Engine OBIGGS system
Hydraulic drain system
Cowl anti-ice system
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MAX
FWD IDLE
EPR OF THE DAY
3 UP AND ALL THE WAY OUT
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If the handles stay foward, the brakes are set
Person C Visually checks the brakes
Pressure indicator reads 1500 psi
Brakes indicate SET on MFD 4
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True
False
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True
False
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Engine 1 is used to start engine 4 secondary
FWD aircraft air is primary, APU is secondary
APU is primary, external pneumatic is secondary
Engine 1, and 4 are primary and engine 2 and 3 secondary
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Pilot or co-pilot sliding window
Maintenance ditching hatch
APU access doors
Nose radome
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Use both when you run engines
Use B system on humid days
Use A system on rainy days
Alternate use of A & B
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Flux capacitor heater
Perform a battle start
Press all four start switches
Both A and B ignition systems
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Lights
Anti-Ice
Headsets
None of these
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Person A
Person B
Person C
Person D
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True
False
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Two Minutes
Two Seconds
One Hour
One Minute
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True
False
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Three
One
Four
Two
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WAP cue switchlight
Flowline test switchlight
ANN/DIGT test switchlight
BRT/DIM test switchlight
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Fuel flow and Revolutions per Min
Fuel Flow and Exhaust Gas Temperature
Exhaust Gas Temperature and Revolutions Per Minute
Total Pressure Inlet And Total Temperature Inlet
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True
False
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Start Control Switch
Override
Generator Switch
Fuel boost pump switch
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True
False
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100 A Degrees
130 A Degrees
150 A Degrees
190 A Degrees
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True
False
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3800-4200 psi
3900-4300 psi
3950-4350 psi
4000-4400 psi
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Position A/C (Acft) to meet wind limits
Wait for the wind to go away
Call MOC for guidance
Reschedule engine run
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Person A
Person B
Person C
Person D
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True
False
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Overtemperature condition
Overspeed condition
Insufficient fuel flow
Loss of weight on wheels indication
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True
False
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Perform engine run with fire department standing by
Proceed with engine run, investigate afterwards
Investigate prior to running engines
Never run that engine again
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Borescope equipment
Inlet cushion pad
Exhaust cover
Inlet cover
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Left side accessory compartment door aft side
Right side only accessory compartment door
Left side accessory compartment door forward
Both left and right side accessory compartment
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With fire detection system loop A inoperative
With fire detection system loop B inoperative
With fire detection system loop A and loop B inoperative
None of these
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APU loop A and loop B lights come on, center
Master warning press to reset lights on glare shield
Fire light on APU panel comes on, WAP display
All of the above
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4
3
2
1
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97-101%
95-99%
94-98%
96-100%
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OFF/Raised
On/Depressed
ARM
OVERRIDE
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Cross
TIE
On
OFF
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True
False
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Notify person A of any vehicular or aircraft
Keep all personnel and equipment clear of aircraft
Do not allow anyone to enter the aircraft with out
All answers are the scanners responsibility
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Ignition switch
APU power switch
Fuel solenoid switch
Engine shutoff switch
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170 A Degrees
180 A Degrees
190 A Degrees
200 A Degrees
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Notify fire department and give aircraft number
Notify job control and give engine serial number
Notify ground control and give aircraft tail number
Notify fire department and give aircraft make
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True
False
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NLG downlock links
Nose fire bottle handle
NLG steering bypass valve handle
MLG steering bypass valve handle
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