C-5M Study at Training Flashcards
1
Q
AIRPLANE WEIGHT LIMITS:
Maximum Ramp
A
840,000 lbs
2
Q
AIRPLANE WEIGHT LIMITS:
Maximum Takeoff
A
840,000 lbs
3
Q
AIRPLANE WEIGHT LIMITS:
Maximum Inflight
A
840,000 lbs
4
Q
AIRPLANE WEIGHT LIMITS:
Maximum Landing
A
840,000 lbs
5
Q
AIRPLANE WEIGHT LIMITS:
Maximum Fuel
A
332,500 lbs
6
Q
AIRPLANE WEIGHT LIMITS:
Maximum Zero Fuel (ZFW)
A
686,190 lbs
7
Q
AIRPLANE WEIGHT LIMITS:
Normal Landing
A
635,850 lbs
8
Q
AIRPLANE WEIGHT LIMITS:
Normal Landing Fuel
A
142,600 lbs
9
Q
AIRPLANE WEIGHT LIMITS:
Heavyweight
A
635,850 lbs
10
Q
PITCH AND BANK:
Normal Pitch on Rotation
A
8-10 degrees
11
Q
PITCH AND BANK:
Max Pitch on Rotation
A
13 degrees
12
Q
PITCH AND BANK:
Pitch Attitude (Windshear Recovery)
A
15-18 degrees
13
Q
PITCH AND BANK:
Max Pitch (Rapid Descent)
A
15 degrees
14
Q
PITCH AND BANK:
Max Pitch (Below 200 Feet)
A
10 degrees
15
Q
PITCH AND BANK:
Max Bank (Below 200 Feet)
A
15 degrees
16
Q
PITCH AND BANK:
Max Bank (Below 50 Feet)
A
5 degrees
17
Q
AOA:
Clean, Holding
A
4.5 degrees
18
Q
AOA:
Vapp 100% Flaps
A
6.9 degrees
19
Q
AOA:
Vapp 40% Flaps
A
7.8 degrees
20
Q
AOA:
Vapp No Flap
A
7.2 degrees
21
Q
AOA:
Vapp 100% Flaps and Slats Up
A
5 degrees
22
Q
AOA:
Vstall Flaps Up
A
13-14 degrees
23
Q
AOA:
Vstall Flaps Down
A
17-19 degrees
24
Q
Oxygen Pressure:
Static (No Flow)
A
275-450 PSIG
25
Oxygen Pressure:
Stabilized (Flow)
275-400 PSIG
26
ICING:
On the Ground: If ice buildups are noted or suspected, momentarily advance the engines to greater than ___ percent N1 every ___ minutes.
70 percent N1 every 5 minutes
27
ICING:
Inflight: Avoid prolonged operation at thrust settings below ___ percent N1.
70 percent N1
28
ICING:
Inflight: If prolonged operation cannot be avoided, advance each engine individually for ___ seconds to at least ___ percent N1 every ___ minutes when flying above ________ feet and every ___ minutes when flying below _______ feet.
10-30 seconds / 70 percent / 10 minutes / 15,000 feet / 6 minutes / 15,000 feet
29
ENGINE EGT LIMITS:
MTO Below 15,000 feet
5 minutes / 960 degrees
30
ENGINE EGT LIMITS:
Maximum Continuous
925 degrees
31
ENGINE EGT LIMITS:
Starting: Ground
750 degrees
32
ENGINE EGT LIMITS:
Starting: Flight
960 degrees
33
ENGINE EGT LIMITS:
Maximum Reverse
960 degrees
34
CG LIMITS
19-41 %
35
MAX NLG STEERING ANGLE:
< or = to 732,500 pounds, Asymetric thrust and braking
60 degrees
36
MAX NLG STEERING ANGLE:
> 732,500 pounds, Symetric thrust and braking
60 degrees
37
MAX NLG STEERING ANGLE:
> 732,500 pounds, Asymetric thrust OR braking - Castered ____ , Fixed ___
Castered 60 degrees, Fixed 45 degrees
38
MAX NLG STEERING ANGLE:
> 732,500 pounds, Asymetric thrust AND braking - Castered ____ , Fixed ___
Castered 45 degrees, Fixed 30 degrees
39
STARTER DUTY LIMITATIONS -
DUTY CYCLE:
___ Minutes On, ___ Minutes Off
___ Minutes On, ___ Minutes Off
___ Minutes On, ___ Minutes Off (Continuous)
5 Minutes On, 2 Minutes Off
5 Minutes On, 2 Minutes Off
5 Minutes On, 10 Minutes Off (Continuous)
40
HYDRAULIC PRESSURE:
Normal
3,000 +/- 150 PSI
41
HYDRAULIC PRESSURE:
Overpressure
3,400 PSI
42
HYDRAULIC PRESSURE:
Min for NLG Emergency Extension
2,500 PSI
43
HYRDAULIC PRESSURE:
Min for 1 Full Brake Application
1,000 PSI
44
MAXIMUM SPEEDS:
Clean Recommended
350 KCAS / .825 M
45
MAXIMUM SPEEDS:
Rapid Descent
350 KCAS / .825 M
46
MAXIMUM SPEEDS:
Emergency Descent
350 KCAS / .85 M
47
MAXIMUM SPEEDS:
Landing Light Extended
300 KCAS / .825 M
48
MAXIMUM SPEEDS:
Yaw Aug Faulted / INOP
300 KCAS / .825 M
49
MAXIMUM SPEEDS:
Max Taxi > 732,500 lbs
30 kts
50
MAXIMUM SPEEDS:
Max Taxi > 772,000 lbs
20 kts
51
THRUST REVERSERS (INFLIGHT):
Max to Deploy Inboard TR
300 KCAS / .825 M
52
THRUST REVERSERS (INFLIGHT):
Max w/Inboard TR Extended
350 KCAS / .825 M
53
THRUST REVERSERS (INFLIGHT):
Max to Stow Inboard TR
250 KCAS / .77 M
54
THRUST REVERSERS (INFLIGHT):
Min with Inboard TR Extended
215 KCAS
55
THRUST REVERSERS (On the Ground):
TR Levers to Reverse Idle at
60 KCAS
56
THRUST REVERSERS (On the Ground):
If Rev Thrust Idle is exceed below _____, an engine & TR System inspection is required.
50 KCAS
57
Landing Gear Extension
250 KCAS / .60 M
58
Landing Gear Operation
250 KCAS / .60 M
59
Landing Gear Recommended
200 KCAS
60
TAKEOFF & LANDING:
Vapp Increase for Ice on Wing/Tail
5 KCAS
61
TAKEOFF & LANDING:
Min Touchdown Speed Vapp minus
6 kt
62
TAKEOFF & LANDING:
Landing ( < or = Normal Landing Weights)
540 ft/min
63
TAKEOFF & LANDING:
Landing ( > Normal Landing Weights)
360 ft/min
64
AIRSTART:
EEC Prevents Start Engagement Above ______
30% N2
65
AIRSTART:
Most Favorable Conditions:
N2 at or greater than _____,
Altitudes below ________
15% N2 / 20,000 feet
66
EMERGENCY:
RAT - Max Extension
350 KCAS / .825 M
67
EMERGENCY:
RAT - Max Retraction
180 KCAS / .45 M
68
EMERGENCY:
RAT - Minimum for Hydraulics > or = 15,000 feet
190 KCAS
69
EMERGENCY:
RAT - Minimum for Hydraulics < 15,000 feet
175 KCAS
70
EMERGENCY:
Minimum for Flight Instruments
155 KCAS
71
EMERGENCY:
Main Tank Low (If fuel mismanagement has occurred)
280 KCAS / .825 M
72
EMERGENCY:
Main Sump Low
280 KCAS / .825 M
73
EMERGENCY:
3 Engine Enroute Climb:
> 600,000 lbs. ____________
< or = 600,000 lbs _____________
270 KCAS / .65 M
| 250 KCAS / .65 M
74
EMERGENCY:
2 Engine Enroute Climb:
> 600,000 lbs. ____________
< or = 600,000 lbs _____________
250 KCAS / .50 M
| 230 KCAS / .50 M
75
EMERGENCY:
Drift down (2 or 3 Engine)
250 KCAS / .45 M
76
TURBULENCE:
CLEAN (Severe Turbulence)
280 KCAS / .825 M
77
TURBULENCE:
Recommended Penetration
240 KCAS / .74 M
78
FLAPS & SLATS:
40% Flaps (Slats Ext / Retract)
215 KCAS / .45 M
79
FLAPS & SLATS:
62.5% Flaps
195 KCAS / .45 M
80
FLAPS & SLATS:
Landing Flaps
180 KCAS / .45 M
81
FLAPS & SLATS:
62.5% Flaps (No Slats)
185 KCAS / .45 M
82
FLAPS & SLATS:
Landing Flaps (No Slats)
175 KCAS / .45 M
83
FLAPS & SLATS:
Slats Extended (No Flaps)
215 KCAS / .45 M
84
AIR REFUELING:
AR Door Open
350 KCAS / .825 M
85
AIR REFUELING:
Normal Rendezvous
300 KCAS / .72 M
86
AIR REFUELING:
Rendezvous Outside 3 NM
325 KCAS
87
AIR REFUELING:
KC-135 at 1/2 NM
270 KCAS / .65 M
88
AIR REFUELING:
KC-135 Contact
252 KCAS / .62 M
89
AIR REFUELING:
KC-135 Max Refueling
265 KCAS / .64 M
90
AIR REFUELING:
KC-10 at 1/2 NM
290 KCAS / .70 M
91
AIR REFUELING:
KC-10 Contact
275 KCAS / .66 M
92
AIR REFUELING:
KC-10 Max Refueling
300 KCAS / .77 M
93
OXYGEN SYSTEM:
Cabin Press Low CWA
10,000 feet
94
OXYGEN SYSTEM:
Oxygen Warning Activation
12,500 - 14,000 feet
95
OXYGEN SYSTEM:
Auto Reset of Oxygen Warning System
11,500 feet
96
ENGINE ANTI-ICE:
Use anti-ice on the ground when visible moisture is present and the temperature is below ____
8 degrees Celsius
97
LANDING GEAR EMERGENCY:
MLG may not rotate at air speeds > ______ with hydraulic pressure available.
185 KCAS
98
LANDING GEAR EMERGENCY:
MLG will not rotate at air speeds > ______ with accumulator pressure only.
170 KCAS
99
LANDING GEAR EMERGENCY:
Max Brake Applications with Fully Charged Accumulator
3 times
100
ENGINE SUCTION FEED LIMITS:
During Climb with JP8 -
Outboard Engines ___________
Inboard Engines. ___________
32,000 feet
| 40,000 feet
101
DOORS:
Max Wind to Open Visor
35 kts
102
DOORS:
Max Winds with Visor Open
70 kts
103
DOORS:
Max WInds to Open Aft Doors
35 kts
104
DOORS:
Max Winds with Aft Doors Open
70 kts
105
ALDCS INOP:
Light Turbulence
300 KCAS / .825 M
106
ALDCS INOP:
Moderate / Severe Turbulence
300 KCAS / .825 M
107
LANDING LIGHTS:
On the ground when less than fully extended do no operate for more than _____ minutes.
25 minutes
108
TAKEOFF & LANDING:
Rudder Effective for Direction Control
80 KCAS
109
TAKEOFF & LANDING:
Max Vrot / Vapp Increase for Gusts
10 KCAS
110
TAKEOFF & LANDING:
Max Vrot Increase for Gusts, XW, & Ice
15 KCAS
111
TAKEOFF & LANDING:
After flap retraction, do not exceed ____ bank until accelerating to minimum of _______________ .
10 degrees / Vmfr + 15 KCAS
112
TAXI:
Min Taxiway Width
75 feet
113
TAXI:
Min Runway Width
147 feet
114
TAXI:
Min Width for 180 degrees MRT (CASTERED):
(FIXED):
```
150 feet (Castered)
228 feet (Fixed)
```
115
TAXI:
Max from Edge for 180 degree MRT
4 feet
116
TAXI:
Wingsapn
222.9 feet
117
TAXI:
Turn Anti-Skid Off When Taxiing Below ______
20 kts
118
TAXI:
If stopped in turn w/aft MLG Castered, limit NLG to no more than _______ from stopped position.
30 degrees
119
TAXI:
If stopped and all MLG at zero degrees, the NLG may be turned _______ prior to forward motion.
45 degrees
120
ENGINE CROSSWIND / TAILWIND:
Below 6000 feet:
From ____ to ____ Tailwind limited to _________
10 kt - 35 kt / 70% N1
121
ENGINE CROSSWIND / TAILWIND:
Below 6000 feet:
From ____ to ____ Crosswind limited to _________
25 kt - 35 kt / 70% N1
122
ENGINE CROSSWIND / TAILWIND:
Below 6000 feet:
From ____ to ____ Tailwind or Crosswind limited to _________ for engine start and taxi
35 kt - 50 kt / 40% N1
123
ENGINE CROSSWIND / TAILWIND:
At or Above 6000 feet:
From ____ to ____ Tailwind limited to _________
10 kt - 35 kt / 70% N1
124
ENGINE CROSSWIND / TAILWIND:
At or Above 6000 feet:
From ____ to ____ Crosswind limited to _________
10 kt - 35 kt / 70% N1
125
ENGINE CROSSWIND / TAILWIND:
At or Above 6000 feet:
Engine operation is _____________ with tailwind or crosswind component over _________ .
Not permitted / 35 knots
126
NOSE DOWN PITCH:
Do Not Exceed
15 degrees
127
NOSE DOWN PITCH TRIM:
Normal Operations
1.5 degrees
128
NOSE DOWN PITCH TRIM:
Air Refueling Operations
3.8 degrees
129
NOSE DOWN PITCH TRIM:
Nose down Settings > 2.7 degrees, Limit Speed to:
CG Forward of 30% _____________
CG Aft of 30% ____________
270 KCAS / .65 M
| 300 KCAS / .775 M
130
HIGH ALTITUDE PENETRATION:
Shall Not Be Initiated at Altitudes ____________
Shall Not be Initiated at Gross Weights ____________
Above FL200
| Above 600,000 lbs
131
BOLDFACE:
ENGINE FIRE ON THE GROUND
1. FIRE HANDLE - “PULLED” (P)
| 2. AGENT - “DISCHARGED” (P)
132
BOLDFACE:
EMERGENCY ENGINE SHUTDOWN
1. THROTTLE - “IDLE” (PF)
2. FIRE HANDLE - “PULLED” (PM)
3. AGENT - “AS REQUIRED” (PM)
133
BOLDFACE:
SMOKE/FUMES IN THE AIRPLANE
1. OXYGEN - “ON, 100%” (CP, P, E)
134
BOLDFACE:
LOSS OF PRESSURIZATION
1. OXYGEN - “ON, 100%” (CP, P, E)
