C-17 PIQ EOC Exam | Most Recent Exam 2026 Actual
Complete Real Exam Questions And Correct Answers
(Verified Answers) Already Graded A+ | Guaranteed
Success!! Newest Exam
When performing the Electrical Fire and Smoke checklist,
a) pause after each step which depowers a portion of the aircraft
b) do each step in rapid succession
c) wear asbestos gloves at all times
d) never pull out any circuit breakers
a) pause after each step which depowers a portion of the aircraft
The engine-driven hydraulic pumps provide continuous hydraulic pressure
of _______ psi.
a) 4,000
b) 4,200
c) 4,500
d) 5,000
a) 4,000
, The engine-driven hydraulic pumps are located in the
a) respective engine accessory gear box
b) right aft gear pod
c) wheel wells
d) cargo compartment
a) respective engine accessory gear box
The normal pressure for the passenger oxygen system is
a) 150-350 psi
b) 200-375 psi
c) 250-430 psi
d) 285-430 psi
d) 285-430 psi
,There is/are ___________ engine driven hydraulic pump(s) per system, located
on and driven by their respective engine accessory gearbox.
a) one
b) two
c) three
d) four
b) two
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 3 engine loss.
a) auxiliary
b) transfer
c) primary
d) secondary
b) transfer
, The RAT, located in the forward right main gear pod, develops enough
hydraulic pressure to control the aircraft for
a) takeoff and refueling
b) emergency refueling
c) LAPES delivery
d) all engine-out emergency
d) all engine-out emergency
During ground operations, you have been using hydraulic system 1 without
any engines running. The MASTER CAUTION light comes on as well as the
HYD cue light and a LOW in the Sys 1 Aux pump switch light. You should
conclude that you have
a) low temperature in system 1
b) asymmetric slats
c) overpressure condition in system 1
d) failure of the AUX pump 1
d) failure of the AUX pump 1
Complete Real Exam Questions And Correct Answers
(Verified Answers) Already Graded A+ | Guaranteed
Success!! Newest Exam
When performing the Electrical Fire and Smoke checklist,
a) pause after each step which depowers a portion of the aircraft
b) do each step in rapid succession
c) wear asbestos gloves at all times
d) never pull out any circuit breakers
a) pause after each step which depowers a portion of the aircraft
The engine-driven hydraulic pumps provide continuous hydraulic pressure
of _______ psi.
a) 4,000
b) 4,200
c) 4,500
d) 5,000
a) 4,000
, The engine-driven hydraulic pumps are located in the
a) respective engine accessory gear box
b) right aft gear pod
c) wheel wells
d) cargo compartment
a) respective engine accessory gear box
The normal pressure for the passenger oxygen system is
a) 150-350 psi
b) 200-375 psi
c) 250-430 psi
d) 285-430 psi
d) 285-430 psi
,There is/are ___________ engine driven hydraulic pump(s) per system, located
on and driven by their respective engine accessory gearbox.
a) one
b) two
c) three
d) four
b) two
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 3 engine loss.
a) auxiliary
b) transfer
c) primary
d) secondary
b) transfer
, The RAT, located in the forward right main gear pod, develops enough
hydraulic pressure to control the aircraft for
a) takeoff and refueling
b) emergency refueling
c) LAPES delivery
d) all engine-out emergency
d) all engine-out emergency
During ground operations, you have been using hydraulic system 1 without
any engines running. The MASTER CAUTION light comes on as well as the
HYD cue light and a LOW in the Sys 1 Aux pump switch light. You should
conclude that you have
a) low temperature in system 1
b) asymmetric slats
c) overpressure condition in system 1
d) failure of the AUX pump 1
d) failure of the AUX pump 1
