Powertrain and Rotor Systems Flashcards

1
Q

The ________ accessory module has a low oil pressure switch and chip detector.

A

Left

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2
Q

The main transmission is made up of ____ modules.

A

Five

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3
Q

Each accessory module drives both ________ and ________ .

A

Main generator, Hydraulic pump

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4
Q

Oil pressure should remain steady in the __ to __ psi range to ensure that when fluctuations occur, they remain in the acceptable range.

A

45 to 60

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5
Q

What caution appears if a chip detector fails the PBIT?
CHIP IBIT FAIL

A
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6
Q

The fuzz burn-off feature is deactivated when oil temperature reaches ___°C.?

A

140

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7
Q
  1. The intermediate and tail gear box may run at cruise flight for ___ minutes, with loss of all oil.
A

30

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8
Q
  1. When gear box oil temperature reaches 140°C, the _____ _____ feature de-activates.
A

Fuzz Burn

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9
Q

What is the maximum NR for normal shutdown operations of the rotor brake?

A

NR below 40%, 150–180 psi applied, in not less than 12 seconds

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10
Q
  1. With rotor brake applied, what is the contingency which allows you to move the PCLs from idle to fly?
A

idle inter-lock lever

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11
Q

Operating an engine against the gust lock __ _______ on rotor brake equipped helicopters.

A

is prohibited

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12
Q

The rotor brake solenoid prevents movement of the ______ _____ ______ from idle to fly.

A

Engine power levers

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13
Q

One advantage of the wide chord blades is _________________.

A

increased maneuverability

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14
Q

The three control inputs connecting the primary servos to the main rotor swashplate are the _______, ___, and _______ control rods.

A

Forward, Aft, and Lateral

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15
Q

. The tail rotor provides approximately _____ lift.

A

2.5%

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16
Q

The tail rotor is mounted on the right side of the tail pylon, and canted _____
upward.

17
Q

Decreasing NR may be accompanied by a drop in transmission oil pressure of _____ psi or more.

18
Q

The severity of vibrations can usually be minimized by __________________.

A

reducing airspeed