1 - STANEVAL EKQ Flashcards

(118 cards)

1
Q

Length of reference chord?

A

5.671 m

WBM

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2
Q

MDP to start of LeMAC?

A

20.307 m

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3
Q

Range of aircraft chord?

A

20-39.5%

Weight dependant

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4
Q

Useable length of cargo hold?

A

17.27m

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5
Q

Ramp length?

A

5.42 m

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6
Q

Max useable height of cargo hold fwd FR 43?

A

3.8 m

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7
Q

Max useable height of cargo hold aft FR 43?

A

4.0 m

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8
Q

Max useable width of cargo hold?

A

4.02 m

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9
Q

Max taxi weight LH?

A

141,400 Kgs

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10
Q

Max Take off weight LH?

A

141,000 Kgs

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11
Q

Max landing weight LH?

A

123,000 Kgs

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12
Q

Max Zero fuel weight LH?

A

117,100 Kgs

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13
Q

Minimum weight LH?

A

78,000 Kgs

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14
Q

Max taxi weight LN?

A

137,900 Kgs

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15
Q

Max Take off weight (LN)?

A

137,500 Kgs

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16
Q

Max Landing weight LN?

A

121,500 Kgs

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17
Q

Max Zero fuel weight LN?

A

109,600 Kgs

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18
Q

Minimum weight LN?

A

78,000 Kgs

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19
Q

Max Taxi weight TLL1?

A

131,400 Kgs

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20
Q

Max take off weight TLL1?

A

131,000 Kgs

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21
Q

Max landing weight TLL1?

A

115,000 Kgs

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22
Q

Maximum zero fuel weight TLL1?

A

109,600 Kgs

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23
Q

Minimum weight TLL1?

A

80,200 Kgs

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24
Q

Maximum taxi weight TLL2?

A

115,400 Kgs

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25
Maximum take off weight TLL2?
115,000 Kgs
26
Maximum landing weight TLL2?
115,000 Kgs
27
Maximum zero fuel weight TLL2?
97,000 Kgs
28
Minimum weight TLL2?
80,200 Kgs
29
Maximum taxi weight low tyre pressure?
120,400 Kgs
30
Maximum take off weight low tyre pressure?
120,000 Kgs
31
Maximum landing weight low tyre pressure?
120,000 Kgs
32
Maximum zero fuel weight low tyre pressure?
109,600 Kgs
33
Minimum weight low tyre pressure?
78,000 Kgs
34
What tyre pressures are considered for ‘low tyre pressure’ operations?
Nose landing gear 101 psi Main landing gear 111 psi
35
Maximum fuel imbalance (symmetrical tanks) at T/O and Landing?
1. 200 kgs 1-4/2-3. 1200 kgs L/R Inners. 2. 400 kgs 1-4/2-3. 400 kgs L/R Inners.
36
Maximum fuel capacity (Normal Capacity)?
48, 879 Kgs RTS
37
Max payload in cargo hold?
37,600 Kgs
38
Max payload on ramp?
6,000 Kgs
39
Main floor D ring strength (and ramp FR 56+57 B to F)?
11,340 Kgs
40
Ramp D ring strength (except FR 56+57 B to F)?
4535 Kgs
41
Max ramp ULD weights P1, P2, P3, P5, P6, P7?
3000 Kgs
42
Max ramp ULD weights P4?
2350 Kgs
43
What is the towing weight limit for the aircraft?
141,400 Kgs
44
Manoeuvre limits for LN1 and TLL1?
-1g to +2.5g RTS/FCOM
45
Manoeuvre limits LH?
-1g to +2.25g
46
Manoeuvre limits TLL2?
\<14,000 ft -1g to +3g \>14,000 ft -1g to +2.5g
47
Maximum operating speed LN1, TLL1, TLL2?
The lesser of; 300 KIAS M0.72
48
Maximum operating speed LH?
Whichever is the lest of; 280 KIAS M0.72
49
Limiting wind sped from ramp and door open on the ground or operating?
50 knots Fig B 6.2.1.1
50
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
51
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
52
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
53
Back up operations; 1) max weight? 2) OAT? 3)ISA? 4) max pressure Alt? 5) max duration?
1) 131,400 Kgs 2) 39 degrees 3) ISA +15 4) 3000ft 5) 2 mins
54
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.
55
Max cross wind post mod 83838 Take off and landing?
30 knots including gusts
56
Maximum weights for: 1) Crew seats? 2) Pax Seats? 3) Stretchers?
1) 110 Kgs 2) 132 Kgs 3) 100 Kgs
57
Where is the prop plane area?
FR 30-34 Avoid pax sitting here where possible.
58
Altitude Limit for APU bleed air extraction and starting on batteries?
25,000 ft
59
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.
60
What is the number of personnel allowed in the cockpit above 8000 ft cabin altitude?
Five, after that additional portable oxygen must be provided.
61
What is the time limit of the passenger oxygen system?
17 mins
62
Max weight on the crew entrance door?
400 Kgs
63
Maximum load that can be carried on the ramp?
6000 Kgs
64
Maximum single load that can loaded across the ramp hinge line?
32,000 Kgs
65
Maximum design support load of the stabiliser struts?
32,000 Kgs
66
When stabiliser struts are deployed, what is prohibited?
Simultaneous loading/unloading and refuelling.
67
Maximum pulling angles for the cargo winch?
+\- 30 degrees Horizontal 0 to +30 degrees vertical
68
Maximum POB?
121 (116 pax and 5 crew) 92 POB currently with life raft DHOI
69
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.
70
Where can class 1 be carried?
Ramp only
71
Max g for class 1?
2g
72
Max altitude and temperature for class 1?
31,000 ft for equipment cleared to -32 degrees When curtain removed no restrictions.
73
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.
74
Operation of the aircraft in the tactical fuel sequence is prohibited above what weight?
TLL1 Max Taxi weight 131,400 Kgs
75
Distance from MDP to nose?
4820 mm
76
Compartment (zone) A frame location?
FR 21-30
77
Compartment (zone) B frame location
FR 30-51
78
Compartment (zone) C frame location?
FR 51-55
79
Ramp frame location?
FR 55A - 63A
80
Height of roller conveyor?
51 mm
81
Height of ramp hinge non kneeled?
1.67 m
82
Height of ramp hinge kneeled?
1.321 m
83
Max wind speed for strut use without calculations?
21 knots
84
Max wind speed when using to raise the aircraft?
17 knots
85
Max design support load of the stabiliser struts - single item of load?
32,000 Kgs
86
Weight of single item of load when stabiliser strut loadspreaders required (Ramp grounded)?
23,800 Kgs
87
Weight of ULD when stabiliser strut load spreader required (Ramp horizontal)?
16,000 Kgs
88
Number of 4535 Kgs tensioners and chains onboard?
20
89
Number of 11,340 Kgs chains and tensioners onboard?
20
90
Number of 4535kg ratchet strops onboard?
20
91
Max weight of aircraft when in raised mode and stabiliser strut load spreader required?
115,000 Kgs
92
Max payload on the ramp when open with rods fitted?
6,000 Kgs
93
Max payload on the ramp when open during taxi - no rods?
2,000 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)
100
Max Sidewall seat fit?
54 (52 with SAK fitted)
101
Max Seat Fit?
116 (54+62)
102
Max Stretcher Fit?
66 stretchers plus 26 attendant seats
103
Maximum Aircraft Occupancy?
121
104
Max passenger number if CED or REE not available?
37 (Crew member and loadmaster seats not included)
105
Max passenger number if PTDs not available?
106
Max pallet fit cargo compartment?
7
107
Max pallet fit on the ramp?
2
108
463L Pallet weight?
122 Kilograms DAP 101A-1101-1
109
Load capacity of 463L Pallet?
4535 Kilograms DAP 101A-1101-1
110
Maximum height of the load CofG of 463L Pallet? Maximum load height? Number of rings on the 108in side? Number of rings on the 88in side?
48 inches 96 inches 6 5 DAP 101A-1101-1
111
Shape of the 4535kg net? Which side has a red marker row? How many corner lashing lines? Maximum floor area dimensions? Max height when floor area less than 100in x 80in? Max weight when floor area less than 100in x 80in? When is a net is to be removed from service and not used?
Cruciform 88 inch side 4 Yellow, 4 red 120 inches by 80 inches Not higher than the lesser floor dimension. 2250 kilograms if more than two hooks attached to a floor point The TIMEX date cannot be established. TIMEX limit reached 10 years old from manufacture
112
Winch cable length?
75 metres LMOM
113
Normal max vehicle weight for single line haul? Normal max vehicle weight for double line haul? Normal max vehicle weight for triple line haul?
10 ton (Depending on wheel base/knleeling) 20 ton (Depending on wheel base/kneeling 29.8 ton (Depending on wheel base) LMOM
114
Winch max cable angle?
30 degrees LMOM
115
Winch Ancillaries consist of?
Pulleys, Ramp hinge protectors, LAAs LMOM
116
The winch cable will be rendered u/s if?
Broken wires ( 2 over 58mm, 4 over 285mm, 8m over all) Waviness (1mm above flat surface) Local increase in cable diameter (5% increase on 9.5 mm). LMOM
117
The Winch is controlled from?
LMWS, LMCP, RCUs LMOM
118
How many RCU connection points are there in the cargo hold?
1 x FR 21-22 Port 1 x FR36-37 Port 2 x FR54-55 Both sides 2 x FR 61-63 Both sides Total 6 LMOM