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CBT > General > Flashcards

General Flashcards

1
Q

The ATR 72 main dimensions are:

A 
Length - 27.166 m/ 89 ft 1.5 in
Span    - 27.050 m/ 88 ft 9 in
Height  - 7.72 m (CG 25%)
             - 7.67 m (CG 14%)
             - 7.52 m (CG 37%)
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2
Q

Distance between main LG wheels:

A

4.1 m

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3
Q

Propeller diameter and clearance from the fuselage:

A

3.96 m diameter and 0.82 m clearance

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4
Q

The ATR 72 passenger capacity:

A

68 pax

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5
Q

The plane is certified in the Transport Category, JAR 25 and ICAO Annex 16 for:

A
  • VFR and IFR
  • Flight in icing conditions
  • Reverse thrust taxi (single or twin engine)
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6
Q

Minimum flight crew and maximum operating altitude ?

A

2 pilots and 25000 ft

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7
Q

Height and width of the fuselage

A

Height - 1.910 m
Width (diameter) - 2.865 m outside
- 2.570 m inside
- 2.263 m inside (floor level)

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8
Q

Distance between engines:

A

8.1 m

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9
Q

Distance between main and nose LG

A

10.79 m

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10
Q

What is the crosswind limit for operating the cargo door

A

45 KT

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11
Q

The risk for a tip up exists when:

A

from seven persons and up, moving near the rear part of an off load aircraft

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12
Q

MTOW

A

22800 KG

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13
Q

MLW

A

22350 KG

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14
Q

MZFW

A

20800 KG

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15
Q

Maximum Taxi Weight

A

22970 KG

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16
Q

Maximum Fuel Load and the usable fuel quantity in each tank

A

5000 KG and 2500 KG in each tank

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17
Q

Conditions for Hotel Mode

A

RH engine running + propeller brake on + gust lock on + condition levers at feather

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18
Q

Hotel Mode works with the

A

LP and HP stages

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19
Q

Entry door + dimensions

A
  • outward opening
  • non plug type
  • 72 cm wide (without hand-rails) / 1.75 m high
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20
Q

Non-plug type door

A

They rely on the strength of the locking mechanism to keep the door shut, whereas a plug door relies on the pressure differential to keep it shut

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21
Q

Service door + dimensions

A
  • outward opening
  • non plug type
  • 69 cm wide / 1.27 m high
22
Q

Cargo door + dimensions

A
  • outward opening
  • non plug type
  • 1.30 m wide / 1.57 m high
23
Q

Cockpit communication door. Location + dimensions

A
  • below the captain’s side window

- 17.5 cm wide / 15 cm high

24
Q

Forward compartment door. About

A

Located in the fwd section of the nose LG, gives external access tot the avionics compartment behind the main instrument panel

25
Q

Aft avionics door. About

A

Gives access to the rear unpressurized area of the aircraft (beyond the aft bulk compartment)

26
Q

Cockpit emergency exit hatch

A
  • provided for evacuation of the flight compartment
  • the escape rope is located in a compartment on top of the electric rack, RH side
  • located between FR(frame) 9 and FR 12
27
Q

Emergency exit doors

A
  • Type III
  • 2 doors, on the LH and RH sides
  • between FR 18 and FR 19 and STR(stringer) 6 and STR 12
28
Q

If used as emergency exit doors, the main and the service doors are what type

A

Type I

29
Q

When is the doors opening inhibited and how

A

When delta p > 6 PSI. Through vent doors

30
Q

Number of doors and their location

A
  1. main
  2. service
  3. emergency LH
  4. emergency RH
  5. cargo door
  6. cockpit communication door
  7. forward communication door
  8. aft avionics compartment door
  9. cockpit emergency exit hatch
31
Q

When are the lights (cockpit) OFF

A

normal operation

32
Q

Light: AMBER

A

Caution. Does not require immediate action. Time for taking action will be left to the crew’s discretion.

33
Q

Light: RED

A

Warning. Configuration or failure requires immediate action

34
Q

Light: GREEN

A

Normal operation

35
Q

Light: WHITE

A

Control position indication

36
Q

Light: BLUE

A

Normal transient configuration

37
Q

Lighting controlled from the cockpit:

A
  • cockpit
  • cabin signs
  • emergency
  • exterior
38
Q

Lighting controlled from the cabin:

A
  • cabin
  • emergency
  • aft cargo compartment
39
Q

Lighting controlled from exterior panels:

A
  • FWD cargo compartment
  • main & nose LG wells
  • FWD & AFT avionics compartments
  • refueling panel
40
Q

How can you illuminate the aircraft when you enter it and for how long

A

Through a switch located on the RH at the main entrance which provides 2 minutes illumination of two emergency lights and the cockpit entrance light. Another switch located at the cockpit entrance panel provides the same functions.
EXTRA: as soon as the passenger door is open, GND HANDLING BUS is available (entrance light power supply)

41
Q

Exterior lights include:

A

A. Navigation lights: red left (port side, 110 degrees), green right (starboard, 110), white tail (140 degrees)
B. Taxi/take off lights
C. Landing lights
D. Wing scan lights
E. Beacon anti-collision lights: top & bottom (white flashing)
F. Strobe lights: wings & tail (white flashing)
G. Logo lights
H. Emergency lights

42
Q

What is the voltage for emergency illumination of the EXIT signs on the ceiling and the EXTERIOR lights

A

6 VDC

43
Q

What are the sources for the emergency illumination

A
  • DC STBY BUS via a voltage divider

- 6V integral batteries with a 10 minutes capacity, charged from the DC STBY BUS

44
Q

When the emergency lighting system activates, it is supplied from….or

A

from the DC STBY BUS, or if this source fails, automatically from the batteries

45
Q

With aircraft batteries supply only (2 min), the lighting is restricted to:

A
  • RH dome light, with the possibility of switching it off
  • LH three lights below the glareshield
  • Overhead panel light illuminating the pedestal
46
Q

How is the lighting with the DC NORMAL BUS activated

A
  • six lights below the glareshield

- one light overhead, illuminating the pedestal

47
Q

where is the ice evidence probe located and when does it illuminate

A

located on the Captain’s side, it illuminates when the NAV lights are switched on

48
Q

Emergency lighting switch: ARM

A

The normal switch position during flight. The emergency lighting is automatically actuated as soon as both DC generators are lost, or when DC STBY BUS voltage is

49
Q

Emergency lighting switch: ON

A

The emergency lighting comes on whether or not the power supply voltage is 28 V. The 6 V emergency batteries will be discharged only when the onboard network voltage decreases below 18 V. Batteries are charged if power supply voltage is 28 V.

50
Q

Emergency lighting switch: DISARM

A

Normal position when the aircraft is on ground. The emergency lighting is off whether or not the power supply voltage is 28 V. The DISARM caution light located on overhead panel comes on if 28 V power supply is available on aircraft network.

CBT (2 decks)

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