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KA-400 > 400 Aircraft General > Flashcards

400 Aircraft General Flashcards

1
Q

Approximate Flight range

A

7,000nm

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2
Q

400BCF Max Weights

A

Taxi - 873
T.O. - 870
Inflight w/ Flaps - 670
Landing flaps 25/30 - 652
Zero Fuel - 610

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3
Q

400F Max Weights

A

Taxi - 878
T.O. - 875
Inflight w/ Flaps - 670
Landing flaps 25/30 - 652
Zero Fuel - 610

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4
Q

Max operating altitude

A

45,100’

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5
Q

Max takeoff and landing latitude

A

10,000’

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6
Q

Max field Elevation

A

9,500’

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7
Q

Max Runway slope

A

+/- 2%

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8
Q

Max speed in RVSM

A

.90 Mach

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9
Q

What can HP ground air be used for?

A

Engine start and a/c PACKs

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10
Q

Overhead panel sections

A

AFT - Mx Panel
Center - Circuit Breaker Panel
FWD - Overhead Panel

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11
Q

What control cabin pressurization?

A

Two outflow valves in the back of the cabin

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12
Q

What control pressurization in normal operation?

A

Automatically with takeoff and landing F.E. and cruise date from the FMC

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13
Q

What Ice and Rain protection does the 400 have?

A

Window heat
Probe heat
Wing anti-ice
Nacelle anti-ice

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14
Q

When can wing anti-ice be operated?

A

Only during flight

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15
Q

When can nacelle anti-ice be operated?

A

Ground or in flight

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16
Q

What else is turned on while the nacelle anti-ice is on?

A

The engine igniters

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17
Q

How many pitot-static probes are there?

A

4

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18
Q

How many AOA probes are there?

A

2

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19
Q

How many TAT probes are there?

A

2

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20
Q

How are the windshields heated?

A

Forward Electrically heated with interior anti fog and exterior anti ice
Side - electrically heated with interior anti fog only

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21
Q

What are the hydraulic load assignments?

A

Heavy load (Landing gear, brakes, flaps, etc.)
1 and 4
Primary flight control 2 and 3
With redundancy built in

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22
Q

System 1 HYD Load

A

Center AP
Left in/out Aileron
Upper Rudder
Inbd TE flap
NW/Body Steering
Alt Brakes
Left on/in Elevator

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23
Q

System 2 HYD Load

A

Right AP
Left Out Aileron
Right IN Aileron
Spoilers 2,3,10,11
Low YD
Low Rudder
Alt Brakes
Elevator feel
Stab trim
Left INBD Elevator

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24
Q

System 3 HYD Load

A

Left AP
Left INBD Aileron
Right Out Aileron
Spoilers 1,4,9,12
Upper YD
Upper Rudder
Alt Brakes
Elevator feel
Stab trim
Right INBD elevator

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25
Q

System 4 HYD Load

A

Right INBD Aileron
Right Out Aileron
Spoilers 5,6,7,8
Lower Rudder
OUT TE Flap
Wing gear
Normal Brakes
Right INBD/Out Elevator

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26
Q

Landing gear

A

4 Mains, 2 body and 2 center
1 Nose

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27
Q

Ground Steering

A

Nose gear and Body gear
Wing gear does not steer

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28
Q

Wheel brakes

A

Wheel braking on all main gear with Normal and alternate braking. Both systems provide anti-skid.

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29
Q

AUTO Brake Settings

A

RTO - T.O.
2,3,4, MAX - Landing

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30
Q

Fuel Tanks

A

Center Wing Tank
4 Main Tanks
2 Reserve Tanks

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31
Q

Center Wing tank capacity

A

115,008 lbs
52,167kg

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32
Q

Main Tanks 1 & 4 Capacity

A

29,295 lbs
13,288 lbs

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33
Q

Main Tanks 2 & 3 Capacity

A

84,065 lbs
38,131.5 kg

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34
Q

Reserve Tanks Capacity

A

8,858 lbs
4,018 kg

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35
Q

How is fuel normally delivered?

A

Under pressure

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36
Q

What are the AC pumps in the fuel system?

A

2 AC boost pumps in each main tank
2 Overide Jettison pumps in Main 2 & 3
2 Overide Jettison pumps in CWT

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37
Q

Explain the fuel Crossfeed system.

A

4 Crossfeed valves to allow fuel delivery from the CWT or any Main to ANY engine or the APU.
All normally closed.

38
Q

Where does the APU normally get fuel?

A
  • Main tank 2
  • w/ AC power fuel is supplied by main pump 2 aft. Main 3 aft operates to prevent tank to tank transfer and provides fuel if main 2 fails.
  • w/o AC power a dedicated DC pump in main 2 provides fuel.
39
Q

APU Operation limits

A

Can only be used up to 20,000’.
Can only supply bleed air in flight, no electrical power.
Can not be started in the air.

40
Q

APU generators

A

2 APU generators can completely power the airplane on the ground

41
Q

APU Bleed air

A

Can power the pneumatic system.
Ground: Power all A/C packs except during engine start.
Air: Can power 1 pack up to 15,000’

42
Q

Where is APU operation displayed?

A

On the STATUS page.

43
Q

Where are the APU ground panel?

A

In the Right Body Gear Wheel well.

44
Q

The Air Conditioning System has _____ Packs.

A

3

45
Q

T/F: The Autobrake system is selected to RTO for takeoff.

A

True

46
Q

Thrust rating of each engine.

A

57,900 lbs Takeoff Thrust

47
Q

What kind of Engines does the airplane have?

A

Dual Rotor Axial Flow Turbofans
High Compression and Bypass ratio

48
Q

What in the engine drives the accessory box?

A

N2 rotor

49
Q

How is the Thrust reverse operated on the GE engines?

A

Pneumatically with bleed air from the associated engine.

50
Q

What is the EEC?

A

Electronic Engine Controller, monitors TL position to automatically control engines and provides limit protections.

51
Q

What fire systems are on the airplane?

A

Detection and extinguishing system for the Engines, APU, Cargo, and LAVs.
Detection only in the Main gear wheel wells

52
Q

How Fire Extinguishing bottles are there?

A

2 per wing for engines
1 for APU
6 for forward and AFT cargo

53
Q

What happens when the Main Deck Cargo Fire Arm switch is pressed?

A

Turns off two packs and stop airflow to all cargo compartments.

54
Q

What happens when the CARGO DPRESS/DISCH switch?

A

Opens the Outflow vales to initiate a controlled cabin depressurization.

55
Q

What is the fire detection system in the flight deck crew compartment?

A

Aural warning if smoke is detected and automatic extinguisher in the waste container.

56
Q

How are the primary flight controls operated?

A

From the hydraulic systems

57
Q

What is the primary pitch control?

A

4 elevator surfaces

58
Q

What is the secondary pitch control?

A

The horizontal Stabilizer

59
Q

What provides roll control?

A

Inboard and outboard ailerons and 10 of 12 spoilers

60
Q

Which spoilers act as speed brakes?

A

4 inboard on each wing

61
Q

Which spoilers act as ground spoilers?

A

All 6 on each wing

62
Q

How are LE flaps normally powered?

A

Pneumatically from the bleed air ducts

63
Q

How are TE flaps normally powered?

A

By the hydraulic system
1- Inboard
4 - Outboard

64
Q

What is the secondary mode for the flaps?

A

Electric drive to move the flaps

65
Q

What are normal sources of AC power?

A

4 IDGs and the APU generators

66
Q

When can the autopilot be used?

A

After takeoff to Autoland with full-roll out capabilities.

67
Q

T/F The main gear wheel wells have a fire extinguisher?

A

False

68
Q

Aircraft Wing span

A

211’,5’’ (64.4m)
Varies based on fuel in the wing tanks

69
Q

Wing tip height

A

16’ 9’’ (5.11m)

70
Q

Winglet Height

A

22’ (6.71m)

71
Q

Span of the Horizontal Stab

A

72’ 9’’ (22.2m)

72
Q

Height of the Horizontal Stab

A

27’ (8.23m)

73
Q

Overall Length

A

231’ 10’’ (70.7m)

74
Q

Distance from Nose to Nose gear

A

25’ (7.6m)

75
Q

Distance from Nose gear to body gear

A

89’ 5.5’’ (27.26m)

76
Q

Distance between body gear

A

12’ 7’’ (3.8m)

77
Q

Distance between wing gear

A

41’ 4’’ (12.5m)

78
Q

Height of the fuselage

A

32’ 5.5’’ (9.89m)

79
Q

Height of the tail

A

62’ 6.5’’ (19.06m)

80
Q

Wing tip radius

A

159’ (48.9m)

81
Q

Minimum pavement width for 180 turn

A

153’ requires normal nose and body steering

82
Q

At take off power, the hazard distance of winds up to 100 mph extends to almost _____ ft/ ______ m from the back of the engine.

A

500 , 150

83
Q

Where is the Fire Panel Located?

A

Overhead panel

84
Q

Where are the rudder trim control located

A

The Aisle Stand

85
Q

How many main deck entry doors are there? How many are active?

A

10 total, only 2 activated

86
Q

How many cargo doors are there?

A

5
Lower forward, aft, and cargo. Side cargo and nose cargo.

87
Q

Which doors have slides on the aircraft?

A

Upper Deck Doors only.

88
Q

When both Left side Main Deck Doors are NOT closed and latched the EICAS message(s) __________ display(s).

A

DOOR ENTRY L

89
Q

Where are the emergency escape devices stowed?

A

Adjacent to the flight deck overhead hatch

90
Q

Power to operate the left side cargo door is supplied by the _______________.

A

Main Deck Cargo Handling Bus

91
Q

All Main Deck Door ENTRY door Controls are located ____________.

A

On the door

92
Q

What type of window damage can cause Arcing to occur?

A

Moisture Ingress

KA-400 (33 decks)

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