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P-8A Normal Procedures General Knowledge Test Prep UPDATED Exam Questions and CORRECT Answers $9.49   Add to cart

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P-8A Normal Procedures General Knowledge Test Prep UPDATED Exam Questions and CORRECT Answers

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P-8A Normal Procedures General Knowledge Test Prep UPDATED Exam Questions and CORRECT Answers Ensure coordination with the ground crew before any of the following: - Correct Answer- 1. Hydraulic system pressurization. 2. Flight control surface movement (*excludes trim*). 3. Weapons bay doo...

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  • August 24, 2024
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  • 2024/2025
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  • P-8A Normal Procedures General Knowledge
  • P-8A Normal Procedures General Knowledge
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P-8A Normal Procedures General
Knowledge Test Prep UPDATED Exam
Questions and CORRECT Answers
Ensure coordination with the ground crew before any of the following: - Correct Answer- 1.
Hydraulic system pressurization.
2. Flight control surface movement (*excludes trim*).
3. Weapons bay door open/close.
4. EO/IR extend/retract.
5. Aircraft movement.


(7.1.2 Normal Procedures Assumptions)


When applying external power or APU generator power, the standby hydraulic pump can
operate for approximately 4 seconds and may move the _____________. - Correct Answer-
Rudder and/or thrust reversers


(7.2.1 Electrical Power Up)


After _____ consecutive aborted start attempts, a fifteen minute cooling period is required for
the APU. - Correct Answer- 3


(7.2.1)


After three consecutive aborted start attempts, a _____ minute cooling period is required for
the APU. - Correct Answer- 15


(7.2.1)


During Electrical Power Up, what does it mean if the FAULT light fails to illuminate when
the TEST switch is held to FAULT/INOP? - Correct Answer- The fault monitoring system is
inoperative.

,(7.2.1)


At what point is the APU generator is ready to assume an electrical load after starting? -
Correct Answer- The APU GEN OFF light will illuminate.


(7.2.1)


Fuel in the center tank should be at least ______ lbs to supply the APU. - Correct Answer-
1000


(7.2.1 Electrical Power Up)


The APU should be operated for _____ minute/s prior to being used as a bleed air source. -
Correct Answer- 1


(7.2.1)


What temperature considerations must be made regarding PACK operation when the APU is
the sole source of bleed air during pre-flight? - Correct Answer- If OAT is 10°C or below
only one PACK should be operated when using APU bleed air for OBIGGS.


(7.2.2 OBIGGS Preflight Preparation)


Load shedding and subsequent loss of OBIGGS inerting will occur at _____%. - Correct
Answer- 92


(7.2.2 OBIGGS Preflight Preparation)


During Oxygen Mask Preflight, ensure that the mission crew oxygen pressure on the flight
deck did not decrease more than _____ psi. - Correct Answer- 100


(7.2.4.2 Oxygen Mask Preflight — Mission Crew)

, Which lights should be illuminated on the upper overhead panel during Preliminary Flight
Deck Preflight? - Correct Answer- 1. ALIGN lights
2. Landing gear indicator lights


(7.2.5)


During the fuel overheat test, the engines should not be started unless __________ is/are
displayed. - Correct Answer- "-88" in the LCD segments and a fault history code of "E8"


(7.2.5)


The stall warning test may not work. Why? - Correct Answer- The AC transfer buses need to
be powered for up to 4 minutes.


(7.2.5 Preliminary Flight Deck Preflight)


Why may the STALL WARNING TEST fail? - Correct Answer- No hydraulic power may
cause drooping of the leading edge flaps and cause an asymmetry signal.


(7.2.5 Preliminary Flight Deck Preflight)


If the STALL WARNING TEST fails due to flap asymmetry, turn on the ____ system electric
pump to retract the flaps. - Correct Answer- B


(7.2.5)


What light(s) should be illuminated in the 1st column of the lower overhead panel during the
Flight Deck Preflight? - Correct Answer- 1. Flight control LOW PRESSURE lights
2. ENG VALVE CLOSED lights (illuminated dim)
3. SPAR VALVE CLOSED lights (illuminated dim)
4. Main tank fuel pump LOW PRESSURE lights

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