Ch 8

Question 1

(Before Starting Engines)

Before ENG operation, ensure all _______________________

Answer 1

main rotor tie-downs are removed

WARNING

Question 2

(Before Starting Engines)

While fully restrained at appropriate ________________, I must be able to manipulate all ______________________________________.

Answer 2

Design Eye Position

flight controls, propulsion, fuel, fire t-handles

(WARNING)

Question 3

(Before Starting Engines)

Do not grasp _____________ on glare shield to adjust seats or may cause damage.

Answer 3

foam pad

CAUTION

Question 4

(COCKPIT EQUIPMENT CHECKS)
(2. APU Control Switch – ON /// “APU-CLEAR”:)

If APU ACCUM LOW does not appear, Pull ____________________ on accumulator manifold until APU reaches __________________.

Answer 4

manual override lever

self-sustaining speed

(NOTE)

Question 5

(COCKPIT EQUIPMENT CHECKS)
(2. APU Control Switch – ON /// “APU-CLEAR”:)

If APU fails, __________________, Note BITE indications.

Answer 5

do not turn off BATT switch

NOTE

Question 6

(COCKPIT EQUIPMENT CHECKS)
(3. GENERATORS APU SWITCH-ON /// “STAB/TACAN CLEAR”:)

STAB will ______________ due to AC power being applied (Senses zero A/S and in AUTO MODE).

Answer 6

slew full down

WARNING

Question 7

(COCKPIT EQUIPMENT CHECKS)
(3. GENERATORS APU SWITCH-ON /// “STAB/TACAN CLEAR”:)

Due to potential_______________, ensure no one is within __’ of the TACAN antennae when power is applied to the A/C.

Answer 7

radiation hazard

3

(WARNING)

Question 8

(COCKPIT EQUIPMENT CHECKS)
(3.2. EDECU- Check signal Val code 25%)

Verify 25% on Q indicator for 701D to verify _______________ installed.

Answer 8

DAS plug

NOTE

Question 9

(COCKPIT EQUIPMENT CHECKS)
(3.2. EDECU- Check signal Val code 25%)

EDECU _____________ may be verified on FMS status page.

Answer 9

configuration

NOTE

Question 10

(COCKPIT EQUIPMENT CHECKS)
(3.2. EDECU- Check signal Val code 25%)

Code displayed after AC power application at a rate of __ seconds on and __ seconds off during startup, and __ seconds after both ENG’s are shutdown w/AC power applied

Answer 10

4

2

30

(NOTE)

Question 11

(COCKPIT EQUIPMENT CHECKS)
(8. MASTER WARNING PANEL – Check # 1 ENG OUT, # 2 ENG OUT, LOW ROTOR RPM segment lights are illuminated.)

If segment light does not appear, pull __________________ to reset bulb.

Answer 11

¼ inch then push back in

Question 12

(COCKPIT EQUIPMENT CHECKS)
(13. Press FCC FAILURE RESET switches.)

EGI’s must be in _____________ phase before faults will reset.

Answer 12

ORIENT

NOTE

Question 13

(COCKPIT EQUIPMENT CHECKS)
(16. Flight Controls- Check first helicopter flight of the day.)

Perform control sweeps (Cyclic) to see if _______________ is in the way (Restrictions).

Answer 13

aviator worn gear

WARNING

Question 14

(COCKPIT EQUIPMENT CHECKS)
(16. Flight Controls- Check first helicopter flight of the day.)

Limit force applied to pedals only to contact a system stop with ___________________ to prevent flight control bearing/bolt noises.

Answer 14

SAS/BOOST-off

Question 15

(COCKPIT EQUIPMENT CHECKS)
(16. Flight Controls- Check first helicopter flight of the day.)

If hydraulic access door is open, ensure ___________ are not over nose to prevent contact with WSPS.

Answer 15

rotor blades

CAUTION

Question 16

(COCKPIT EQUIPMENT CHECKS)
(Stabilator- Check.)

If any part of check fails _________ the A/C.

Answer 16

do not fly

WARNING