1 - General Limitations Flashcards

(99 cards)

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
Minimum weight low tyre pressure?
78,000 Kgs
26
What tyre pressures are considered for ‘low tyre pressure’ operations?
Nose landing gear 101 psi Main landing gear 111 psi
27
Maximum fuel imbalance (symmetrical tanks) at Take Off and Landing?
1. 200 Kgs 1-4/2-3, 12000 Kgs L/R Inners 2. 400 Kgs 1-4/2-3, 400 Kgs L/R Inners
28
Maximum fuel capacity?
48,879 Kgs
29
What is the towing weight limit for the aircraft?
141,400 Kgs
30
Manoeuvre limits LN1 and TLL1?
-1g to +2.5g
31
Manoeuvre limits LH?
-1g to +2.25g
32
Manoeuvre limits TLL2?
\<14,000 ft -1g to +3g \>14,000 ft -1g to +2.5g
33
Maximum operating speed LN1, TLL1, TLL2?
The lesser of; 300 KIAS M0.72
34
Maximum operating speed LH?
Whichever is the lest of; 280 KIAS M0.72
35
Limiting wind sped from ramp and door open on the ground or operating?
50 knots Fig B 6.2.1.1
36
What are the taxi speed limitations of the ramp & door; 1) Operation of ramp and door?
Max ground speed (kts) 30 Max IAS (kts) 60
37
What are the taxi speed limitations of the ramp & door; 2) Ramp/Cargo Door Open (Ramp Rods connected)?
Maximum ground speed 60 knots Maximum IAS 60 knots
38
What are the taxi speed limitations of the ramp & door; 3) Ramp/Cargo door open (load restrained on Ramp)?
Maximum ground speed (kts) 30 Maximum IAS 60 knots
39
Back up operations; 1) max weight? 2) Max OAT for back-up operations (Reversing) At or above 22kts crosswind/tailwind? 3) max duration?
1) 131,400 Kgs 2) At or above 22kts crosswind/tailwind ISA + 15 degrees C 3) 2 mins
40
What are the three possible Back up operations cooling processes?
All engine ground idle with props in-feathered for 15 mins. All engines shut down for a minimum of 2 hours Airborne activity.
41
Max cross wind post mod 83838 Take off and landing?
30 knots including gusts
42
Maximum weights for: 1) Crew seats? 2) Pax Seats? 3) Stretchers?
1) 110 Kgs 2) 132 Kgs 3) 100 Kgs
43
Where is the prop plane area?
FR 30-34 Avoid pax sitting here where possible.
44
Altitude Limit for APU bleed air extraction and starting on batteries?
25,000 ft
45
APU start and ground operation temperature limits (0 feet)?
-55 to +55 degrees reducing with height. See RTS table Fig 3.1.1 - APU Operating envelope.
46
What is the number of personnel allowed in the cockpit above 8000 ft cabin altitude?
Five, after that additional portable oxygen must be provided.
47
What is the time limit of the passenger oxygen system?
17 mins
48
Max weight on the crew entrance door?
400 Kgs
49
Maximum load that can be carried on the ramp?
6000 Kgs
50
Maximum single load that can loaded across the ramp hinge line?
32,000 Kgs
51
Maximum design support load of the stabiliser struts?
32,000 Kgs
52
When stabiliser struts are deployed, what is prohibited?
Simultaneous loading/unloading and refuelling.
53
Maximum pulling angles for the cargo winch?
+\- 30 degrees Horizontal 0 to +30 degrees vertical
54
Maximum POB?
121 (116 pax and 5 crew) 92 POB currently with life raft DHOI
55
Where can class 1 be carried?
Ramp only
56
Speed limitations with class 1?
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
Max g for class 1?
2g
58
Max altitude and temperature for class 1?
31,000 ft for equipment cleared to -32 degrees When curtain removed no restrictions.
59
What are the permissible combinations of doors and air deflectors to open up airborne?
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
Operation of the aircraft in the tactical fuel sequence is prohibited above what weight?
TLL1 Max Taxi weight 131,400 Kgs
61
Distance from MDP to nose?
4820 mm
62
Length of reference chord?
5.671 m
63
MDP to start of LeMAC?
20.307 m
64
Range of aircraft chord?
20-39.5%
65
Compartment (zone) A frame location?
FR 21-30
66
Compartment (zone) B frame location
FR 30-51
67
Compartment (zone) C frame location?
FR 51-55
68
Ramp frame location?
FR 55A - 63A
69
Ramp length?
5.42 m
70
Useable length of cargo hold?
17.27m
71
Height of roller conveyor?
51 mm
72
Max useable height of cargo hold fwd FR 43?
3.8 m
73
Max useable height of cargo hold aft FR 43?
4.0 m
74
Max useable width of cargo hold?
4.02 m
75
Height of ramp hinge non kneeled?
1.67 m
76
Height of ramp hinge kneeled?
1.321 m
77
Max wind speed for strut use without calculations?
21 knots
78
Max wind speed when using to raise the aircraft?
17 knots
79
Max design support load of the stabiliser struts - single item of load?
32,000 Kgs
80
Weight of single item of load when stabiliser strut loadspreaders required (Ramp grounded)?
23,800 Kgs
81
Weight of ULD when stabiliser strut load spreader required (Ramp horizontal)?
16,000 Kgs
82
Number of 4535 Kgs tensioners and chains onboard?
20
83
Number of 11,340 Kgs chains and tensioners onboard?
20
84
Max weight of aircraft when in raised mode and stabiliser strut load spreader required?
115,000 Kgs
85
Lateral fuel imbalance symmetrical tank limit?
400 Kgs
86
Max payload in cargo hold?
37,600 Kgs
87
Max payload on ramp?
6,000 Kgs
88
Max payload on the ramp when open with rods fitted?
6,000 Kgs
89
Max payload on the ramp when open during taxi - no rods?
2,000 Kgs
90
Ramp D ring strength (except FR 56+57 B to F)?
4535 Kgs
91
Main floor D ring strength (and ramp FR 56+57 B to F)?
11,340 Kgs
92
Max ramp ULD weights P1, P2, P3, P5, P6, P7?
3000 Kgs
93
Max ramp ULD weights P4?
2350 Kgs
94
Longitudinal separation required to avoid creating a Station Area?
1.5 m +
95
Max axle weight in compartment A and C at 1.5 m spacing?
8220 Kgs
96
Max axle weight in compartment B at 1.5 m spacing?
10,500 Kgs
97
Where is the outer non-treadway area ?
From the sidewall to the just inboard of the outer tie down line both sides. (1.785m from aircraft centreline)
98
Where is the inner non-treadway area ?
Just outboard of the central port and starboard (1L&1R) tie down lines. (0.572 m to 0.572 m).
99
Where is the treadway area ?
Just inside the outboard tie down line to just outside tie down lines 2L&2R. (1.785 m to 0.572 m)