Aircraft General: General Flashcards

1
Q

Description of the aircraft structure?

A
  • All metal
  • Pressurized
  • Low-wing, fully-cantilevered
  • 13° Swept-back wings
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2
Q

What are the dimensions of the aircraft?

A
  • Length: 58.4 ft.
  • Width: 47.8 ft.
  • Height: 14.1 ft.
    Rule of thumb 60/50/15
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3
Q

What part of the aircraft is pressurized?

A
  • From the pressure bulkhead to the aft pressure bulkhead
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4
Q

Personnel should maintain a minimum of how many feet when the radar is transmitting?

A
  • 9 ft.
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5
Q

Refueling must not be performed within how many feet of the antenna scan area?

A
  • 100 ft.
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6
Q

Where are the avionics located and how are they ventilated?

A
  • Nose section

- Outflow air from the pressurized section then exhausted to the wheel well

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7
Q

How many total cabin windows?

A
  • Lear 40 has 14 cabin windows

- Lear 45 has 16 cabin windows

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8
Q

What is the width of the cabin door?

A
  • 30 in.
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9
Q

What will prevent the aircraft from pressurizing if the cabin door is not closed with the locking pins engaged?

A
  • A vent flap on the door with a maximum .1 psi
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10
Q

How many pins does the cabin entry door contain?

A
  • 12 pins total
  • 8 upper door
  • 4 lower door
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11
Q

What happens when you pull the internal latch handle on the emergency exit hatch?

A
  • Extracts two spring loaded locking pins and door can be pulled inward only
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12
Q

What kind of windshield does this aircraft have and designed for?

A
  • Resistant glass and polycarbonate material

- Withstand impact of (4) birds at 330 knots

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13
Q

What is the construction of the cabin windows?

A
  • Two layers of acrylic plastic with air space in between
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14
Q

How many degrees are the wings swept?

A
  • 13°s
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15
Q

How much wing twist and dihedral?

A
  • 3°s of wing twist

- 2.5° of wing dihedral

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16
Q

How many triangles in the wing and it’s purpose?

A
  • 8 per wing

- To reenergize boundary airflow at high AOA

17
Q

How many stall strips?

A
  • 1 per wing
18
Q

How many vortilons?

A
  • 4 per wing
19
Q

How many degrees is the vertical stabilizer swept and horizontal stabilizer?

A
  • 41°s Vertical Stabilizer

- 29°s Horizontal stabilizer

20
Q

What is the purpose of the delta fins?

A
  • Provides enhanced stability
  • Prevents deep stall characteristics
  • Dampens dutch roll
  • Reduced need for yaw damper
  • Eliminates the need for a stick pusher
21
Q

How many degrees can the nose steering provide on the taxi?

A
  • 60°s at taxi speed; 70 knots decreases to 7°s
22
Q

How many static wicks are on the aircraft and how many can they be broken?

A
  • 19 Total

- 4 may be missing or broken on the inboards and on the aft vertical stabilizer fairing

23
Q

What is the purpose of the offset joints (sawtooth)?

A
  • Create vortices to reduce spanwise flow