HMH-462 December EP Quiz

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1 point

The ACC GB OIL HOT caution light will go on when the oil temperature is over:

107 degrees C.

121 degrees C.

145 degrees C.

170 degrees C.

1 point

Which subsystems are not are not isolated by the isolation valve? (Check all that apply)

Flight Control

Cargo Door and Ramp

Landing Gear

APP Accumulator Recharge

Main Wheel Power Brakes

1 point

The Longitudinal Bias Actuator, in series with the cyclic pitch flight controls, extends and retracts with airspeed to provide the pilot with a positive longitudinal cyclic gradient.

True

False

1 point

Fail Operational means that the mode is important enough that it will conitnue to operate with a single failure. Which modes of operation are Fail Operational? (Choose all that apply)

Stability Augmentation System (SAS)

Turn Coordination

Control Desensitizers (DSEN)

Hover Augmentation/Gust Alleviation

1 point

With the utility hydraulic system not pressurized, the wheel brakes are capable of holding the helicopter, loaded to the design gross weight, on a 10 degree slope. With hydraulic pressure the helicopter is held on a ______ degree slope.

1 point

External Cargo Jettison

*1. Area-Clear if possible *2. Cargo release-Activated

*1. Cargo release-Activated

*1. Avoid Populated Areas *2. Cargo release-Activated

*1. Area-Clear if possible *2. Avoid Populated Areas *3. Cargo release-Activated

1 point

If you receive an ENG OIL PRESS LOW caution light reduce the power of the affected engine to minimum needed for immediate requirements and then transition to single- or dual-engine operating procedures as quickly as possible.

True

False

1 point

Warning: Failure to reduce airspeed below ____ KIAS when securing the No. 2 engine increases the hot exhaust backflow component and likelihood of a subsequent engine compartment fire.

100

120

1 point

Tail rotor drive system failure is usually preceded by: (Choose all that apply)

excessive vibration

noise in the tail section

10.

1 point

Note: A PYLON UNSAFE FOR FLIGHT caution light may be accompanied by loss of AFCS servos.

True

False

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