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Kawasaki C2 > 1 - General Limitations > Flashcards

1 - General Limitations Flashcards

1
Q

Max taxi weight LN?

A

137,900 Kgs

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2
Q

Max Take off weight (LN)?

A

137,500 Kgs

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3
Q

Max Landing weight LN?

A

121,500 Kgs

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4
Q

Max Zero fuel weight LN?

A

109,600 Kgs

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5
Q

Minimum weight LN?

A

78,000 Kgs

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6
Q

Max taxi weight LH?

A

141,400 Kgs

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7
Q

Max Take off weight LH?

A

141,000 Kgs

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8
Q

Max landing weight LH?

A

123,000 Kgs

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9
Q

Max Zero fuel weight LH?

A

117,100 Kgs

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10
Q

Minimum weight LH?

A

78,000 Kgs

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11
Q

Max Taxi weight TLL1?

A

131,400 Kgs

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12
Q

Max take off weight TLL1?

A

131,000 Kgs

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13
Q

Max landing weight TLL1?

A

115,000 Kgs

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14
Q

Maximum zero fuel weight TLL1?

A

109,600 Kgs

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15
Q

Minimum weight TLL1?

A

80,200 Kgs

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16
Q

Maximum taxi weight TLL2?

A

115,400 Kgs

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17
Q

Maximum take off weight TLL2?

A

115,000 Kgs

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18
Q

Maximum landing weight TLL2?

A

115,000 Kgs

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19
Q

Maximum zero fuel weight TLL2?

A

97,000 Kgs

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20
Q

Minimum weight TLL2?

A

80,200 Kgs

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21
Q

Maximum taxi weight low tyre pressure?

A

120,400 Kgs

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22
Q

Maximum take off weight low tyre pressure?

A

120,000 Kgs

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23
Q

Maximum landing weight low tyre pressure?

A

120,000 Kgs

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24
Q

Maximum zero fuel weight low tyre pressure?

A

109,600 Kgs

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25
Q

Minimum weight low tyre pressure?

A

78,000 Kgs

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26
Q

What tyre pressures are considered for ‘low tyre pressure’ operations?

A

Nose landing gear 101 psi Main landing gear 111 psi

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27
Q

Maximum fuel imbalance (symmetrical tanks) at Take Off and Landing?

A
  1. 200 Kgs 1-4/2-3, 12000 Kgs L/R Inners
  2. 400 Kgs 1-4/2-3, 400 Kgs L/R Inners
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28
Q

Maximum fuel capacity?

A

48,879 Kgs

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29
Q

What is the towing weight limit for the aircraft?

A

141,400 Kgs

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30
Q

Manoeuvre limits LN1 and TLL1?

A

-1g to +2.5g

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31
Q

Manoeuvre limits LH?

A

-1g to +2.25g

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32
Q

Manoeuvre limits TLL2?

A

<14,000 ft -1g to +3g >14,000 ft -1g to +2.5g

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33
Q

Maximum operating speed LN1, TLL1, TLL2?

A

The lesser of; 300 KIAS M0.72

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34
Q

Maximum operating speed LH?

A

Whichever is the lest of; 280 KIAS M0.72

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35
Q

Limiting wind sped from ramp and door open on the ground or operating?

A

50 knots Fig B 6.2.1.1

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36
Q

What are the taxi speed limitations of the ramp & door; 1) Operation of ramp and door?

A

Max ground speed (kts) 30 Max IAS (kts) 60

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37
Q

What are the taxi speed limitations of the ramp & door; 2) Ramp/Cargo Door Open (Ramp Rods connected)?

A

Maximum ground speed 60 knots Maximum IAS 60 knots

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38
Q

What are the taxi speed limitations of the ramp & door; 3) Ramp/Cargo door open (load restrained on Ramp)?

A

Maximum ground speed (kts) 30 Maximum IAS 60 knots

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39
Q

Back up operations;

1) max weight?
2) Max OAT for back-up operations (Reversing) At or above 22kts crosswind/tailwind?
3) max duration?

A

1) 131,400 Kgs 2) At or above 22kts crosswind/tailwind ISA + 15 degrees C 3) 2 mins

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40
Q

What are the three possible Back up operations cooling processes?

A

All engine ground idle with props in-feathered for 15 mins. All engines shut down for a minimum of 2 hours Airborne activity.

41
Q

Max cross wind post mod 83838 Take off and landing?

A

30 knots including gusts

42
Q

Maximum weights for: 1) Crew seats? 2) Pax Seats? 3) Stretchers?

A

1) 110 Kgs 2) 132 Kgs 3) 100 Kgs

43
Q

Where is the prop plane area?

A

FR 30-34 Avoid pax sitting here where possible.

44
Q

Altitude Limit for APU bleed air extraction and starting on batteries?

A

25,000 ft

45
Q

APU start and ground operation temperature limits (0 feet)?

A

-55 to +55 degrees reducing with height. See RTS table Fig 3.1.1 - APU Operating envelope.

46
Q

What is the number of personnel allowed in the cockpit above 8000 ft cabin altitude?

A

Five, after that additional portable oxygen must be provided.

47
Q

What is the time limit of the passenger oxygen system?

A

17 mins

48
Q

Max weight on the crew entrance door?

A

400 Kgs

49
Q

Maximum load that can be carried on the ramp?

A

6000 Kgs

50
Q

Maximum single load that can loaded across the ramp hinge line?

A

32,000 Kgs

51
Q

Maximum design support load of the stabiliser struts?

A

32,000 Kgs

52
Q

When stabiliser struts are deployed, what is prohibited?

A

Simultaneous loading/unloading and refuelling.

53
Q

Maximum pulling angles for the cargo winch?

A

+- 30 degrees Horizontal 0 to +30 degrees vertical

54
Q

Maximum POB?

A

121 (116 pax and 5 crew) 92 POB currently with life raft DHOI

55
Q

Where can class 1 be carried?

A

Ramp only

56
Q

Speed limitations with class 1?

A

M0.65 with 842 rpm selected M0.68 in all other engine settings. 250 KIAS If one engine inop all class 1 is to be red carded.

57
Q

Max g for class 1?

A

2g

58
Q

Max altitude and temperature for class 1?

A

31,000 ft for equipment cleared to -32 degrees When curtain removed no restrictions.

59
Q

What are the permissible combinations of doors and air deflectors to open up airborne?

A

Air deflectors open, one or both PTD open. Air deflectors open, one or both PTD open cargo door open. Air deflectors open, ramp and cargo door open.

60
Q

Operation of the aircraft in the tactical fuel sequence is prohibited above what weight?

A

TLL1 Max Taxi weight 131,400 Kgs

61
Q

Distance from MDP to nose?

A

4820 mm

62
Q

Length of reference chord?

A

5.671 m

63
Q

MDP to start of LeMAC?

A

20.307 m

64
Q

Range of aircraft chord?

A

20-39.5%

65
Q

Compartment (zone) A frame location?

A

FR 21-30

66
Q

Compartment (zone) B frame location

A

FR 30-51

67
Q

Compartment (zone) C frame location?

A

FR 51-55

68
Q

Ramp frame location?

A

FR 55A - 63A

69
Q

Ramp length?

A

5.42 m

70
Q

Useable length of cargo hold?

A

17.27m

71
Q

Height of roller conveyor?

A

51 mm

72
Q

Max useable height of cargo hold fwd FR 43?

A

3.8 m

73
Q

Max useable height of cargo hold aft FR 43?

A

4.0 m

74
Q

Max useable width of cargo hold?

A

4.02 m

75
Q

Height of ramp hinge non kneeled?

A

1.67 m

76
Q

Height of ramp hinge kneeled?

A

1.321 m

77
Q

Max wind speed for strut use without calculations?

A

21 knots

78
Q

Max wind speed when using to raise the aircraft?

A

17 knots

79
Q

Max design support load of the stabiliser struts - single item of load?

A

32,000 Kgs

80
Q

Weight of single item of load when stabiliser strut loadspreaders required (Ramp grounded)?

A

23,800 Kgs

81
Q

Weight of ULD when stabiliser strut load spreader required (Ramp horizontal)?

A

16,000 Kgs

82
Q

Number of 4535 Kgs tensioners and chains onboard?

A

20

83
Q

Number of 11,340 Kgs chains and tensioners onboard?

A

20

84
Q

Max weight of aircraft when in raised mode and stabiliser strut load spreader required?

A

115,000 Kgs

85
Q

Lateral fuel imbalance symmetrical tank limit?

A

400 Kgs

86
Q

Max payload in cargo hold?

A

37,600 Kgs

87
Q

Max payload on ramp?

A

6,000 Kgs

88
Q

Max payload on the ramp when open with rods fitted?

A

6,000 Kgs

89
Q

Max payload on the ramp when open during taxi - no rods?

A

2,000 Kgs

90
Q

Ramp D ring strength (except FR 56+57 B to F)?

A

4535 Kgs

91
Q

Main floor D ring strength (and ramp FR 56+57 B to F)?

A

11,340 Kgs

92
Q

Max ramp ULD weights P1, P2, P3, P5, P6, P7?

A

3000 Kgs

93
Q

Max ramp ULD weights P4?

A

2350 Kgs

94
Q

Longitudinal separation required to avoid creating a Station Area?

A

1.5 m +

95
Q

Max axle weight in compartment A and C at 1.5 m spacing?

A

8220 Kgs

96
Q

Max axle weight in compartment B at 1.5 m spacing?

A

10,500 Kgs

97
Q

Where is the outer non-treadway area ?

A

From the sidewall to the just inboard of the outer tie down line both sides. (1.785m from aircraft centreline)

98
Q

Where is the inner non-treadway area ?

A

Just outboard of the central port and starboard (1L&1R) tie down lines. (0.572 m to 0.572 m).

99
Q

Where is the treadway area ?

A

Just inside the outboard tie down line to just outside tie down lines 2L&2R. (1.785 m to 0.572 m)

Kawasaki C2 (15 decks)

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