Aircraft Configuration Flashcards

1
Q

Aluminum panels are used in some locations for E3 protection while____has been bonded to composite material panels in other locations

A

Aluminum mesh

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2
Q

Which components are located in the avionics compartment?

A

Number one and number two slab
Number one and number two EGI
Number two FCC
Esis battery

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3
Q

How much ground clearance does the landing light in searchlight have when extended

A

Less than 1 ft

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4
Q

Why does storing items blow the seat? Increase the probability in severity of injury in the event of a crash

A

The seats are designed to stroke downward during a crash

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5
Q

The vlea can be adjusted. From___pounds to___pounds

A

130 to 250

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6
Q

What provides a means of manually selecting alternate data sources for the pilot and copilot mfds?

A

Reversionary switch panels

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7
Q

What is the purpose of the I-Event switch?

A

To capture and record intermittent event data

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8
Q

Where is the ESIS display located?

A

The upper center of the instrument panel

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9
Q

What is the purpose of the auxiliary fuel management panel

A

It contains all controls for operating the CEFS

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10
Q

How is the tail wheel locked in the trail position from the cockpit

A

By activating the unlock/lock switch on the parking brake/ tail wheel control panel

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11
Q

What are the three positions of the backup hydraulic pump switch?

A

On auto off

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12
Q

The___safeguards the battery system and the DC electrical system from shorts in the applicable bus

A

Battery circuit breaker panels

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13
Q

The ICS consists of___control panels located throughout the aircraft

A

5 ICS control panels

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14
Q

___Mode provides for hands off and foot off voice activated keying of the ICS intercom or the pvt intercom

A

VOX

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15
Q

Illumination of the___indicates that the digital link between the ICS panel and the ICU has been broken

A

ICU light

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16
Q

What are the four engine power control lever positions?

A

Off idle fly lockout

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17
Q

How is cockpit ventilation controlled

A

Vent blower switch

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18
Q

When either___is pulled DC power actuates the fire extinguisher logic module to select the compartment to which the fire extinguisher agent is to be directed

A

Engine fire T-handle

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19
Q

The two-stage main strut is designed to absorb a landing rate of up to ___ ft per second

A

39 fps (11 Gs)

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20
Q

For flights over 6 hours, the engine oil level should be___

A

Full

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21
Q

The___provides pneumatic power for main engine start and cabin heating and electrical power for ground operation and in-flight emergency

A

APU

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22
Q

The main transmission has a built-in___forward tilt

A

3 deg

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23
Q

What changes the direction of drive transmits torque and reduces shaft speed from the main module to the tail rotor gearbox?

A

Intermediate gearbox (IGB)

24
Q

The tail wheel swivels___on a yoke assembly when unlocked

A

360 deg

25
Q

The bottom trailing edge of the___has an aerodynamically shaped fairing with a 7° camber

A

Tail pylon

26
Q

The stabilator is a variable angle of incidence stabilator that enhances___handling qualities

A

Pitch

27
Q

How to adjust (VLEA)

A

Lever to the right of the seat

28
Q

Range for the VLEA

A

130 to 250 lbs

29
Q

How to control avionics in M
model?

A

FMS

30
Q

Where is the esis located?

A

Nose of the aircraft

31
Q

Purpose of backup Arc 231

A

Emergency in case FMS is not available

32
Q

Accessory module provides mounting and drive for

A

Hydraulic pump and main generator

33
Q

Stabilator purpose

A

Enhance pitch

34
Q

Apu accumulator pressure

A

2800 PSI

35
Q

Landing gear absorption

A

39 fps or 11.3 Gs

36
Q

Embedded global positioning/inertial navigation system (EGI) location

A

Nose of aircraft

37
Q

Where is the FCC number 2 located and what does it do?

A

Nose compartment and controls trim electronically

38
Q

How is the main transmission mounted?

A

3° forward tilt

39
Q

How is the tail rotor mounted and what does it provide?

A

20° cant with 2.5% overall lift provided

40
Q

What are the three positions of the backup hyd pump?

A

On off auto

41
Q

What are the four positions of the engine power control Levers

A

Off idle fly lockout

42
Q

What is E3 protection?

A

Electromagnetic environmental effect

43
Q

What is the significance of high-speed machining

A

Increases durability and lifespan
Provides a single piece of metal machine to shape
The cabin tub structure

44
Q

How many sealed lead acid batteries (SLAB)?

A

2

45
Q

What does EGI stand for and what does it provide?

A

Embedded global positioning/inertial navigation system (EGI)

Position, heading, attitude, turn rate/velocity
PHATV

46
Q

How many bezel keys are on the mfds?

A

24 (6 x 4 sides)

47
Q

How many mfds?

A

4 (1-4 from left/co-pilot seat)

48
Q

What are avionics controlled by?

A

Fms

49
Q

What does the flight/mission display system consist of?

A

MFDs, reversionary switch panels and MFSCs

50
Q

The outboard number one and number four mfds default to the ___ upon power up

A

PFD

51
Q

The reversionary switch panels allow the pilot to

A

Select an alternate data source

52
Q

The PFD___annunciations are displayed as yellow parameter label with a double-headed yellow arrow above

A

Miscompare

53
Q

Selection of the MFD display in various sub modes are accomplished using each mfds

A

24 bezel keys 6 per side

54
Q

The radar altimeter can read up to

A

1500 ft

55
Q

Two places to see storm scope

A

Nav display Arc and full