Aircraft General Flashcards

1
Q

The danger area surrounding the radar is

A

100’ for large metallic objects and 9’ for personnel

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2
Q

The windshields are constructed of

A

A 2 ply layer with the outer glass and the inner polycarbonate material for structural integrity

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3
Q

A coating is applied to the windshield to provide

A

Rain repellency

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4
Q

In the event of the outer glass pane of the windshield shatters, structural integrity is provided by

A

The inner polycarbonate pane

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5
Q

The checklist for outer windshield shattering is found

A

Amber section of the QRH. QRH A-13

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6
Q

During taxi, if the wing clears an object, the ( ) will also clear it.

A

Tail. PTM 1-21

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7
Q

There are ( ) vortilons attached to the underside of each wing

A
  1. PTM 1-19
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8
Q

There are ( ) triangles attached to the inboard leading edge of each wing.

A
  1. PTM 1-18
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9
Q

Which static wicks can be missing and why?

A

Inboard because the outboard dissipate more static electricity. PTM 1-22

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10
Q

The VHF 1 antenna is located ( ) and the VHF 2 antenna is located ( ).

A

1 on the bottom of the aircraft.

2 on the top of the aircraft. PTM 1-23

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11
Q

Maximum structural takeoff weight is

A

21,500

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12
Q

Max landing weight is

A

19,200

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13
Q

MMO and VMO are

A

.81 MACH and 330 kts

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14
Q

Max ramp weight is

A

21,750

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15
Q

The emergency exit can be locked by

A

Inserting the security pin into the locking mechanism. PTM 1-15

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16
Q

The purpose of the vent on the upper main entry door is to

A

Relieve residual cabin pressure after landing and prevent the aircraft from pressurizing if the door is open. PTM 1-12

17
Q

There are 2 APU cooling fans. They are located

A

1 in the tailcone access door and 1 aft of the aft baggage door. PTM 1-17

18
Q

Illumination of the amber EXTERNAL DOORS CAS msg could mean

A

Either or both the baggage door or tailcone access door is open. PTM 1-17

19
Q

( ) or ( ) must be selected on the MFD for takeoff and landing.

A

SUMRY or FLT. AFM 1-10

20
Q

Max weight of the baggage compartment

A

500 lbs. PTM 1-17

21
Q

Minimum extension of the nose strut while on the ground.

A

1.5 inches

22
Q

Which probes heat up on the ground when Probe Heat is turned on?

A

All of them except the Total Air Temp Probe

23
Q

How many static wicks are there?

A

19

11 on the tail
4 on each wing

24
Q

General dimensions

A

58’ long
48’ wingspan
14’ tall

25
Q

Which service bulletin is the engine upgrade?

A

SB 45-72-1