Numbers Flashcards
1
Q
Nose Gear Deflected Maximum Speed:
20 Degrees
A
20 KGS
2
Q
Nose Gear Deflected Maximum Speed:
60 Degrees
A
5 KGS
3
Q
Above 164,000 pounds:
Maximum Taxi Speed
A
10 KGS
4
Q
Above 164,000 pounds:
Max. Nose Gear Deflection
A
20 deg
5
Q
Maximum Tire Speeds:
Nose
A
139 KGS
6
Q
Maximum Tire Speeds:
Main
A
174 KGS
7
Q
Maneuver Load Factor Limitations:
Flaps Up in Area A (Symmetrical)
A
-1 to 3 Gs
8
Q
Maneuver Load Factor Limitations:
Flaps Up in Area A (Unsymmetrical)
A
2.33 Gs
9
Q
Maneuver Load Factor Limitations:
Flaps Up in Area C (Symmetrical)
A
2.5 Gs
10
Q
Maneuver Load Factor Limitations:
Flaps Up in Area C (Unsymmetrical)
A
2 Gs
11
Q
Maneuver Load Factor Limitations: Flaps Extended (Symmetrical)
A
2 Gs
12
Q
Maneuver Load Factor Limitations: Flaps Extended (Unsymmetrical)
A
1.5 Gs
13
Q
Engine and Propeller Limitations:
Maximum Airstart Altitude
A
25,000’
14
Q
Engine and Propeller Limitations:
Static Propeller Feathering Cycles
A
2 cycles
15
Q
Engine and Propeller Limitations:
Feathering Commands
A
4
16
Q
Relative Wind Not Within 45°:
Static Ground Runs (1-4K HP)
A
15 knots
17
Q
Relative Wind Not Within 45°:
Crosswind >15kt, T/O procedure
A
2500 HP (35 KIAS)
18
Q
UNfeathered Propeller Windmilling:
Fire Handle In > 3% NP
A
5 min
19
Q
UNfeathered Propeller Windmilling:
Fire Handle In ≤ 3% NP
A
1 hr
20
Q
Feathered Propeller Windmilling:
Fire Handle Out > 3% NP
A
2 hrs
21
Q
Feathered Propeller Windmilling:
Fire Handle Out ≤ 3% NP
A
6 hrs
22
Q
ACAWS Inhibited:
KIAS
A
70 - 140
23
Q
ACAWS Inhibited:
Alt
A
0 - 400 AGL
24
Q
Personnel Static Lines:
Tailgate Drops
A
20 per pass
25
Personnel Static Lines:
| Manually Retrieved
10 per paratroop door
26
Personnel Static Lines:
| Retriever Winch
20 per cable
27
Accommodations:
| Ground Troops
78
28
Accommodations:
| With wheel well seats
92
29
Accommodations:
| Paratroops
64
30
Accommodations:
| Litters / Attendants
70 / 6
31
Accommodations:
| CDS Bundles
16
32
Accommodations:
| Pallets
6
33
Accommodations:
| Heavy Equipment
42,000 lbs
34
Accommodations:
| Life Rafts
4 x 20 pers
35
Taxi and Takeoff Weight:
| Maximum Normal
164,000 lbs
36
Taxi and Takeoff Weight:
| Maximum Alternate
175,000 lbs
37
Landing Weight @ Rate of Sink:
| Recommended
142,000 lbs @ 540 FPM
38
Landing Weight @ Rate of Sink:
| Maximum Normal
164,000 lbs @ 300 FPM
39
Landing Weight @ Rate of Sink:
| Maximum Alternate
175,000 lbs @ 300 FPM
40
Max Fuel in Tanks for Taxi and Takeoff:
| No. 1 & 4
8310 lbs
41
Max Fuel in Tanks for Taxi and Takeoff:
| No. 2 & 3
7660 lbs
42
Max Fuel in Tanks for Taxi and Takeoff:
| AUXs (ea)
5810 lbs
43
Max Fuel in Tanks for Taxi and Takeoff:
| EXTs (ea)
8900 lbs
44
Max Fuel in Tanks for Taxi and Takeoff:
| Total Main
31,940 lbs
45
Max Fuel in Tanks for Taxi and Takeoff:
| Total Internal
43,560 lbs
46
Max Fuel in Tanks for Taxi and Takeoff:
| Total Internal Plus External
61,360 lbs
47
Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:
| No. 1 and No. 4
7323 lbs
48
Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:
| Main Tanks Total
28,000 lbs
49
Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:
| Aux Tanks Total
no restrictions
50
Max Fuel in Tanks for Landing 300-540 FPM w/ Pods:
| EXTs (ea)
<500 lbs
51
Airspeed Limitations:
| Severe Turbulence
181 KIAS
52
Airspeed Limitations:
| Inoperative Windshield Anti-Icing <10,000 Feet
187 KIAS
53
Airspeed Limitations:
| High Speed Drogue Min
185 KIAS
54
Airspeed Limitations:
| HS Drogue Extending / MAX
250 KIAS / 35,000'
55
Airspeed Limitations:
| Low Speed Drogue Min
105 KIAS
56
Airspeed Limitations:
| LS Drogue Extending
120 KIAS
57
Airspeed Limitations:
| LS Drogue Max
130 KIAS
58
APU Limitations:
| Percentage the START light extinguishes
50%
59
APU Limitations:
| Warm-up time before applying a bleed air load
1 min
60
APU Limitations:
| Warm-up time before applying a bleed air load (≤-26°C)
4 min
61
APU Limitations:
| Starter Duty cycle times
1 min on / 4 min off
62
APU Limitations:
| Maximum continuous EGT (overtemp)
680 deg C (710 deg C for 3 sec)
63
APU Limitations:
| Cool down time without a bleed air load
1 min
64
Fuel Limitations -- Maximum weight difference between:
| Symmetrical main tanks
1000 lbs
65
Fuel Limitations -- Maximum weight difference between:
| Left and right wings
1500 lbs
66
Autopilot Engagement Limitations:
| Minimum altitude during an ILS/IPRA
200' (100' CAT II)
67
Autopilot Engagement Limitations:
| Maximum gross weight
155,000 lbs
68
Autopilot Engagement Limitations:
| Maximum airspeed
Vh
69
Autopilot Engagement Limitations:
| Min. non-approach operations altitude
500'
70
Engine Start Limitations:
| Maximum MGT prior to start
175 deg C
71
Engine Start Limitations:
| Minimum bleed air pressure
22 psi
72
Engine Start Limitations:
| Before attempting ground restarts, wait ___ seconds after NG reaches 0.
30 sec
73
Engine Start Limitations:
Starter duty cycle is __ sec on, __ sec off
for __ cycles, then a __ min cooling time.
70 sec on, 60 sec off
| 5 cycles, 20 min cooling
74
Engine Start Limitations:
| NG must be indicated within __ sec after actuation of the ENGINE START switch to START.
10 sec
75
Engine Start Limitations:
| An indication of increasing eng oil press must be noted within __ sec of gas generator (NG) rotation.
15 sec
76
Engine Start Limitations:
| An indication of increasing gearbox oil press must be noted w/in __ sec of propeller rotation.
15 sec
77
Miscellaneous Limitations:
| LSGI should be selected for __ min prior to eng shutdown to allow engine temp to stabilize.
2 min
78
Miscellaneous Limitations:
| Replace a battery if the voltage is less than:
22 VDC
79
Miscellaneous Limitations:
| The minimum battery voltage allowed for takeoff is:
24 VDC
80
Miscellaneous Limitations:
| Check HP w/in ___ of takeoff prediction NLT __ secs after power levers reach TAKEOFF.
w/in 200 HP w/in 5 sec
81
Miscellaneous Limitations:
| Before Starting Engines checklist, ensure radar altimeter reads between __ and __ feet
1 and -3 ft
82
Miscellaneous Limitations:
| The maximum altimeter error to the elevation of a known checkpoint is +/- __ feet
40 ft
83
Miscellaneous Limitations:
| When accomplishing the propeller controls cycle, the oil temperature must be:
45 deg C
84
Flap Retraction:
| Less than 100K pounds (start)
135 KIAS
85
Flap Retraction:
| 100-140K (start & end)
135 KIAS / FUSS
86
Flap Retraction:
| Greater than 140K (start & end)
Vobs + 5 / FUSS, 10% in 5 kt increments
87
Minimum Runway Length for Landing:
| 100% Flaps
5000'
88
Minimum Runway Length for Landing:
| 0% or 50% Flaps
6000'
89
```
Minimum Runway Length for Landing:
Max Effort (marked zone)
```
Ground Roll + 500'
90
```
Minimum Runway Length for Landing:
Max Effort (unmarked zone)
```
Ground Roll + 1000'
91
Minimum Runway Width:
60'
92
Minimum Taxiway Width:
30'
93
Minimum Runway for Takeoff:
| Normal
Critical Field Length
94
Minimum Runway for Takeoff:
| AMAX
AMFLMETO
95
Minimum Runway for Takeoff:
| MAX
MFLMETO
96
Minimum Runway Length for Landing:
| Normal
Landing Distance
97
Minimum Runway Length for Landing:
| Training
3000' (or Landing Distance, whichever is greater)
98
A "Dash One" Preflight is good for ___ hours, provided the aircraft is _____.
72 hours provided the aircraft is sealed
99
CAT II:
| Min HAT
100'
100
CAT II:
| Min RVR
1200
101
CAT II:
| Max Crosswind
10 kts
102
```
CAT II:
Max Crosswind (Training with min wx)
```
15 kts (with 200, 1/2)
103
Max # of people on Flight Deck:
9
