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HH-60 APU System Numbers, UH60 Hydraulic Systems, Fuel System, uh-6 apart Verified Exam Questions and Answers Latest update 2026/2027

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HH-60 APU System Numbers, UH60 Hydraulic Systems, Fuel System, uh-6 apart Verified Exam Questions and Answers Latest update 2026/2027

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HH-60 APU System Numbers, UH60 Hydraulic Systems, Fuel System,
uh-6 apart Verified Exam Questions and Answers Latest update
2026/2027

Question:
1. Number of reasons for the ESU to shutdown the APU

Answer:



Question:
2. APU OIL TEMP HI caution light

Answer:
149 C

Question:
3. Fuel pump output pressure

Answer:
5 psi

Question:
4. Fuel consumption rate

Answer:
150 pph

Question:
5. Accumulator pressure required to start

Answer:
2800 psi

Question:
6. Single accumulator recharge time

Answer:
90 sec

,Question:
7. Dual accumulator recharge time

Answer:
180 sec

Question:
8. #1 and #2 hydraulic pumps are driven by what?

Answer:
#1 and #2 transmissoin accessory gearbox modules, respectively.

Question:
9. How much pressure do #1 and #2 hydraulic pumps operate
on when main rotor is turning?

Answer:
3000 psi

Question:
10. What powers the backup hydraulic pump?

Answer:
a 115 VAC electric motor

Question:
11. Is AC power required for the backup pump to operate?

Answer:
yes

Question:
12. Each hydraulic pump pressure, volume pump.

Answer:
constant pressure, variable volume is a

Question:
13. At what PSID will the dydraulic pumps' filter indicator buttons pop?

Answer:
70 PSID, plus or minus 10

, Question:
14. At what PSID will the return filter bypass activate?

Answer:
100 PSID, plus or minus 10

Question:
15. What would happen if there was no return filter bypass?

Answer:
hydraulic fluid would be blocked in the return lines with a resulting hydrostatic lock, which would
lock up the flight controls

Question:
16.
What does the #1 hydraulic pump pressurize?

Answer:
#1 primary servos and the #1 tail rotor servo

Question:
17. What does the #2 #2 primary servos and the pilot assist hydraulic pump pressurize?

Answer:



Question:
18. What are the components of the pilot assist area?

Answer:
pitch SAS actuator roll SAS actuator yaw SAS actuator pitch boost servo collective and yaw boost
servo pitch trim assembly

Question:
19. For the pitch trim 3000 PSI to 1000 PSI servo, a pressure reducer in the pilot assist module reduces
the PSI pump pressure to

Answer:
PSI?

Question:
20. Can the backup pump supply pressure to the #1 and #2 hydraulic pumps simultaneously?

Answer:
yes

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