Test Review Flashcards

(37 cards)

1
Q

The minimum clearance of the main rotor is normally 8ft whilst the Nr is at what speed?

A

107% Nr

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2
Q

What is the Amperage of the starter/generator?

A

200 amps

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3
Q

The pilots compartment secondary lights (glare shield) consists of..?

A

Six recessed lights in glare shield

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4
Q

What is the ENG OUT audio alert?

A

ALTERNATING tone

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5
Q

Where does the wheel brake system get its hydraulic pressure from?

A

Toe-operated brake cylinders

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6
Q

What automatically changes tail rotor blade angle as the collective pitch is changed?

A

Collective to yaw coupling

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7
Q

Control movements from the collective and cyclic are transmitted via the…?

A

Mixing Unit

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8
Q

The principle data for Pitch, roll and magnetic heading are provided via..?

A

AHRS

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9
Q

The rate-of-tuen display will be replaced by an expanded localizer display when..?

A

Coupled to an ILS/LOC frequency

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10
Q

What is some of the ducted are form the heating/vent system used for across the windscreen?

A

Defogging

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11
Q

Flight director coupling is not possible if:

A

Only one AP is engaged

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12
Q

To engage ATT mode for an autopilot system…

A

Cyclic Stick Trim must be ON

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13
Q

Maximum water contact speed with FLOT system inflated is…?

A

33kts

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14
Q

The FLOT system is actuated electrically by the pilot at speeds up to…?

A

75kts

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15
Q

What type of gearboxes are the IGB and TGB?

A

Splash-lubricated

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16
Q

When metals chips are detected in the oil sump of_______, a caution light goes on.

A

Any of the main, tail or intermediate gearboxes

17
Q

What permits the blades to flap, lead/lag and rotate?

A

Elastomeric bearings

18
Q

Tail rotor blade flap and pitch change are provided by:

A

Deflection of the flexible composite spars

19
Q

Engine operation with cowling open or unlatched is:

20
Q

The minimum airspeed for IFR flight (Vmini) is____KIAS

21
Q

The N1 5-minute takeoff power is____%N1

22
Q

The CATA landing profile is___kts and rate of descent no more than:

23
Q

With surface w/v 180/5 and departing RW 21 (210deg) what is the head wind component?

24
Q

How do you initiate a CatA takeoff after established in the 5ft hover?

A

Increase collective pitch to achieve 10% torque above hover torque

25
HOGE weight at 3000ft PA, +20°C, the 4% Pwr Margin is_____lbs
11,100lbs
26
The RFM ____Section includes cruise, endurance and climb information to enable pilots to compute fuel requirements
Supplemental Performance Data
27
The flight director should be decoupled when operating below _____KIAS.
60kts
28
After failure of a single symbol generator the _____switch allows continued use of all displays by providing duplicate displays from the remaining symbol generator
SG REV
29
Withe useable fuel per tank 80lbs or less, avoid sustained nose-down pitch attitudes in excess of ____ degrees.
30
The primary source of electrical power to the DECU during startup, idle, and shutdown is…?
DC ESS bus
31
DECU faults are categorised into which 3 groups?
- MINOR - DEGRADED - MAJOR
32
During a confirmed engine fire, prior to pulling the T-handle aft you should_____?
Establish safe OEI flight
33
In the event of an engine compartment fire, extinguishing agent is selected by?
Moving FIRE EXT to MAN or RESERVE after the T-Handle is pulled aft
34
The WINDSHIELD WIPER switch has position marked:
OFF-SLOW-FAST
35
Hot_____ is used for anti-ice protection of the air sleeve between the bell mouth and the engine air intake
Compressor discharge air
36
Electrical interlocks between the first and second stage hydraulic systems:
Prevent one system form being shut-off unless there is at least 1600psi in the opposite system
37
Full pressure is available to the flight control servos at about _____%
10%