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C-5M Pilot Boldface & Limitations > C-5M Study at Training > Flashcards

C-5M Study at Training Flashcards

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Charter Pilot (Part 135) - Oral flashcards
1
Q

AIRPLANE WEIGHT LIMITS:

Maximum Ramp

A

840,000 lbs

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2
Q

AIRPLANE WEIGHT LIMITS:

Maximum Takeoff

A

840,000 lbs

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3
Q

AIRPLANE WEIGHT LIMITS:

Maximum Inflight

A

840,000 lbs

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4
Q

AIRPLANE WEIGHT LIMITS:

Maximum Landing

A

840,000 lbs

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5
Q

AIRPLANE WEIGHT LIMITS:

Maximum Fuel

A

332,500 lbs

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6
Q

AIRPLANE WEIGHT LIMITS:

Maximum Zero Fuel (ZFW)

A

686,190 lbs

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7
Q

AIRPLANE WEIGHT LIMITS:

Normal Landing

A

635,850 lbs

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8
Q

AIRPLANE WEIGHT LIMITS:

Normal Landing Fuel

A

142,600 lbs

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9
Q

AIRPLANE WEIGHT LIMITS:

Heavyweight

A

635,850 lbs

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10
Q

PITCH AND BANK:

Normal Pitch on Rotation

A

8-10 degrees

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11
Q

PITCH AND BANK:

Max Pitch on Rotation

A

13 degrees

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12
Q

PITCH AND BANK:

Pitch Attitude (Windshear Recovery)

A

15-18 degrees

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13
Q

PITCH AND BANK:

Max Pitch (Rapid Descent)

A

15 degrees

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14
Q

PITCH AND BANK:

Max Pitch (Below 200 Feet)

A

10 degrees

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15
Q

PITCH AND BANK:

Max Bank (Below 200 Feet)

A

15 degrees

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16
Q

PITCH AND BANK:

Max Bank (Below 50 Feet)

A

5 degrees

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17
Q

AOA:

Clean, Holding

A

4.5 degrees

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18
Q

AOA:

Vapp 100% Flaps

A

6.9 degrees

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19
Q

AOA:

Vapp 40% Flaps

A

7.8 degrees

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20
Q

AOA:

Vapp No Flap

A

7.2 degrees

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21
Q

AOA:

Vapp 100% Flaps and Slats Up

A

5 degrees

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22
Q

AOA:

Vstall Flaps Up

A

13-14 degrees

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23
Q

AOA:

Vstall Flaps Down

A

17-19 degrees

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24
Q

Oxygen Pressure:

Static (No Flow)

A

275-450 PSIG

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25
Q

Oxygen Pressure:

Stabilized (Flow)

A

275-400 PSIG

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26
Q

ICING:

On the Ground: If ice buildups are noted or suspected, momentarily advance the engines to greater than ___ percent N1 every ___ minutes.

A

70 percent N1 every 5 minutes

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27
Q

ICING:

Inflight: Avoid prolonged operation at thrust settings below ___ percent N1.

A

70 percent N1

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28
Q

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.

A

10-30 seconds / 70 percent / 10 minutes / 15,000 feet / 6 minutes / 15,000 feet

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29
Q

ENGINE EGT LIMITS:

MTO Below 15,000 feet

A

5 minutes / 960 degrees

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30
Q

ENGINE EGT LIMITS:

Maximum Continuous

A

925 degrees

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31
Q

ENGINE EGT LIMITS:

Starting: Ground

A

750 degrees

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32
Q

ENGINE EGT LIMITS:

Starting: Flight

A

960 degrees

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33
Q

ENGINE EGT LIMITS:

Maximum Reverse

A

960 degrees

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34
Q

CG LIMITS

A

19-41 %

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35
Q

MAX NLG STEERING ANGLE:

< or = to 732,500 pounds, Asymetric thrust and braking

A

60 degrees

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36
Q

MAX NLG STEERING ANGLE:

> 732,500 pounds, Symetric thrust and braking

A

60 degrees

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37
Q

MAX NLG STEERING ANGLE:

> 732,500 pounds, Asymetric thrust OR braking - Castered ____ , Fixed ___

A

Castered 60 degrees, Fixed 45 degrees

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38
Q

MAX NLG STEERING ANGLE:

> 732,500 pounds, Asymetric thrust AND braking - Castered ____ , Fixed ___

A

Castered 45 degrees, Fixed 30 degrees

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39
Q

STARTER DUTY LIMITATIONS -

DUTY CYCLE:
___ Minutes On, ___ Minutes Off
___ Minutes On, ___ Minutes Off
___ Minutes On, ___ Minutes Off (Continuous)

A

5 Minutes On, 2 Minutes Off
5 Minutes On, 2 Minutes Off
5 Minutes On, 10 Minutes Off (Continuous)

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40
Q

HYDRAULIC PRESSURE:

Normal

A

3,000 +/- 150 PSI

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41
Q

HYDRAULIC PRESSURE:

Overpressure

A

3,400 PSI

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42
Q

HYDRAULIC PRESSURE:

Min for NLG Emergency Extension

A

2,500 PSI

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43
Q

HYRDAULIC PRESSURE:

Min for 1 Full Brake Application

A

1,000 PSI

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44
Q

MAXIMUM SPEEDS:

Clean Recommended

A

350 KCAS / .825 M

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45
Q

MAXIMUM SPEEDS:

Rapid Descent

A

350 KCAS / .825 M

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46
Q

MAXIMUM SPEEDS:

Emergency Descent

A

350 KCAS / .85 M

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47
Q

MAXIMUM SPEEDS:

Landing Light Extended

A

300 KCAS / .825 M

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48
Q

MAXIMUM SPEEDS:

Yaw Aug Faulted / INOP

A

300 KCAS / .825 M

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49
Q

MAXIMUM SPEEDS:

Max Taxi > 732,500 lbs

A

30 kts

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50
Q

MAXIMUM SPEEDS:

Max Taxi > 772,000 lbs

A

20 kts

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51
Q

THRUST REVERSERS (INFLIGHT):

Max to Deploy Inboard TR

A

300 KCAS / .825 M

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52
Q

THRUST REVERSERS (INFLIGHT):

Max w/Inboard TR Extended

A

350 KCAS / .825 M

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53
Q

THRUST REVERSERS (INFLIGHT):

Max to Stow Inboard TR

A

250 KCAS / .77 M

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54
Q

THRUST REVERSERS (INFLIGHT):

Min with Inboard TR Extended

A

215 KCAS

55
Q

THRUST REVERSERS (On the Ground):

TR Levers to Reverse Idle at

A

60 KCAS

56
Q

THRUST REVERSERS (On the Ground):

If Rev Thrust Idle is exceed below _____, an engine & TR System inspection is required.

A

50 KCAS

57
Q

Landing Gear Extension

A

250 KCAS / .60 M

58
Q

Landing Gear Operation

A

250 KCAS / .60 M

59
Q

Landing Gear Recommended

A

200 KCAS

60
Q

TAKEOFF & LANDING:

Vapp Increase for Ice on Wing/Tail

A

5 KCAS

61
Q

TAKEOFF & LANDING:

Min Touchdown Speed Vapp minus

A

6 kt

62
Q

TAKEOFF & LANDING:

Landing ( < or = Normal Landing Weights)

A

540 ft/min

63
Q

TAKEOFF & LANDING:

Landing ( > Normal Landing Weights)

A

360 ft/min

64
Q

AIRSTART:

EEC Prevents Start Engagement Above ______

A

30% N2

65
Q

AIRSTART:

Most Favorable Conditions:
N2 at or greater than _____,
Altitudes below ________

A

15% N2 / 20,000 feet

66
Q

EMERGENCY:

RAT - Max Extension

A

350 KCAS / .825 M

67
Q

EMERGENCY:

RAT - Max Retraction

A

180 KCAS / .45 M

68
Q

EMERGENCY:

RAT - Minimum for Hydraulics > or = 15,000 feet

A

190 KCAS

69
Q

EMERGENCY:

RAT - Minimum for Hydraulics < 15,000 feet

A

175 KCAS

70
Q

EMERGENCY:

Minimum for Flight Instruments

A

155 KCAS

71
Q

EMERGENCY:

Main Tank Low (If fuel mismanagement has occurred)

A

280 KCAS / .825 M

72
Q

EMERGENCY:

Main Sump Low

A

280 KCAS / .825 M

73
Q

EMERGENCY:

3 Engine Enroute Climb:
> 600,000 lbs. ____________
< or = 600,000 lbs _____________

A

270 KCAS / .65 M

250 KCAS / .65 M

74
Q

EMERGENCY:

2 Engine Enroute Climb:
> 600,000 lbs. ____________
< or = 600,000 lbs _____________

A

250 KCAS / .50 M

230 KCAS / .50 M

75
Q

EMERGENCY:

Drift down (2 or 3 Engine)

A

250 KCAS / .45 M

76
Q

TURBULENCE:

CLEAN (Severe Turbulence)

A

280 KCAS / .825 M

77
Q

TURBULENCE:

Recommended Penetration

A

240 KCAS / .74 M

78
Q

FLAPS & SLATS:

40% Flaps (Slats Ext / Retract)

A

215 KCAS / .45 M

79
Q

FLAPS & SLATS:

62.5% Flaps

A

195 KCAS / .45 M

80
Q

FLAPS & SLATS:

Landing Flaps

A

180 KCAS / .45 M

81
Q

FLAPS & SLATS:

62.5% Flaps (No Slats)

A

185 KCAS / .45 M

82
Q

FLAPS & SLATS:

Landing Flaps (No Slats)

A

175 KCAS / .45 M

83
Q

FLAPS & SLATS:

Slats Extended (No Flaps)

A

215 KCAS / .45 M

84
Q

AIR REFUELING:

AR Door Open

A

350 KCAS / .825 M

85
Q

AIR REFUELING:

Normal Rendezvous

A

300 KCAS / .72 M

86
Q

AIR REFUELING:

Rendezvous Outside 3 NM

A

325 KCAS

87
Q

AIR REFUELING:

KC-135 at 1/2 NM

A

270 KCAS / .65 M

88
Q

AIR REFUELING:

KC-135 Contact

A

252 KCAS / .62 M

89
Q

AIR REFUELING:

KC-135 Max Refueling

A

265 KCAS / .64 M

90
Q

AIR REFUELING:

KC-10 at 1/2 NM

A

290 KCAS / .70 M

91
Q

AIR REFUELING:

KC-10 Contact

A

275 KCAS / .66 M

92
Q

AIR REFUELING:

KC-10 Max Refueling

A

300 KCAS / .77 M

93
Q

OXYGEN SYSTEM:

Cabin Press Low CWA

A

10,000 feet

94
Q

OXYGEN SYSTEM:

Oxygen Warning Activation

A

12,500 - 14,000 feet

95
Q

OXYGEN SYSTEM:

Auto Reset of Oxygen Warning System

A

11,500 feet

96
Q

ENGINE ANTI-ICE:

Use anti-ice on the ground when visible moisture is present and the temperature is below ____

A

8 degrees Celsius

97
Q

LANDING GEAR EMERGENCY:

MLG may not rotate at air speeds > ______ with hydraulic pressure available.

A

185 KCAS

98
Q

LANDING GEAR EMERGENCY:

MLG will not rotate at air speeds > ______ with accumulator pressure only.

A

170 KCAS

99
Q

LANDING GEAR EMERGENCY:

Max Brake Applications with Fully Charged Accumulator

A

3 times

100
Q

ENGINE SUCTION FEED LIMITS:

During Climb with JP8 -
Outboard Engines ___________
Inboard Engines. ___________

A

32,000 feet

40,000 feet

101
Q

DOORS:

Max Wind to Open Visor

A

35 kts

102
Q

DOORS:

Max Winds with Visor Open

A

70 kts

103
Q

DOORS:

Max WInds to Open Aft Doors

A

35 kts

104
Q

DOORS:

Max Winds with Aft Doors Open

A

70 kts

105
Q

ALDCS INOP:

Light Turbulence

A

300 KCAS / .825 M

106
Q

ALDCS INOP:

Moderate / Severe Turbulence

A

300 KCAS / .825 M

107
Q

LANDING LIGHTS:

On the ground when less than fully extended do no operate for more than _____ minutes.

A

25 minutes

108
Q

TAKEOFF & LANDING:

Rudder Effective for Direction Control

A

80 KCAS

109
Q

TAKEOFF & LANDING:

Max Vrot / Vapp Increase for Gusts

A

10 KCAS

110
Q

TAKEOFF & LANDING:

Max Vrot Increase for Gusts, XW, & Ice

A

15 KCAS

111
Q

TAKEOFF & LANDING:

After flap retraction, do not exceed ____ bank until accelerating to minimum of _______________ .

A

10 degrees / Vmfr + 15 KCAS

112
Q

TAXI:

Min Taxiway Width

A

75 feet

113
Q

TAXI:

Min Runway Width

A

147 feet

114
Q

TAXI:

Min Width for 180 degrees MRT (CASTERED):
(FIXED):

A 
150 feet (Castered)
228 feet (Fixed)
115
Q

TAXI:

Max from Edge for 180 degree MRT

A

4 feet

116
Q

TAXI:

Wingsapn

A

222.9 feet

117
Q

TAXI:

Turn Anti-Skid Off When Taxiing Below ______

A

20 kts

118
Q

TAXI:

If stopped in turn w/aft MLG Castered, limit NLG to no more than _______ from stopped position.

A

30 degrees

119
Q

TAXI:

If stopped and all MLG at zero degrees, the NLG may be turned _______ prior to forward motion.

A

45 degrees

120
Q

ENGINE CROSSWIND / TAILWIND:
Below 6000 feet:

From ____ to ____ Tailwind limited to _________

A

10 kt - 35 kt / 70% N1

121
Q

ENGINE CROSSWIND / TAILWIND:
Below 6000 feet:

From ____ to ____ Crosswind limited to _________

A

25 kt - 35 kt / 70% N1

122
Q

ENGINE CROSSWIND / TAILWIND:
Below 6000 feet:

From ____ to ____ Tailwind or Crosswind limited to _________ for engine start and taxi

A

35 kt - 50 kt / 40% N1

123
Q

ENGINE CROSSWIND / TAILWIND:
At or Above 6000 feet:

From ____ to ____ Tailwind limited to _________

A

10 kt - 35 kt / 70% N1

124
Q

ENGINE CROSSWIND / TAILWIND:
At or Above 6000 feet:

From ____ to ____ Crosswind limited to _________

A

10 kt - 35 kt / 70% N1

125
Q

ENGINE CROSSWIND / TAILWIND:
At or Above 6000 feet:

Engine operation is _____________ with tailwind or crosswind component over _________ .

A

Not permitted / 35 knots

126
Q

NOSE DOWN PITCH:

Do Not Exceed

A

15 degrees

127
Q

NOSE DOWN PITCH TRIM:

Normal Operations

A

1.5 degrees

128
Q

NOSE DOWN PITCH TRIM:

Air Refueling Operations

A

3.8 degrees

129
Q

NOSE DOWN PITCH TRIM:
Nose down Settings > 2.7 degrees, Limit Speed to:

CG Forward of 30% _____________
CG Aft of 30% ____________

A

270 KCAS / .65 M

300 KCAS / .775 M

130
Q

HIGH ALTITUDE PENETRATION:

Shall Not Be Initiated at Altitudes ____________
Shall Not be Initiated at Gross Weights ____________

A

Above FL200

Above 600,000 lbs

131
Q

BOLDFACE:

ENGINE FIRE ON THE GROUND

A
  1. FIRE HANDLE - “PULLED” (P)

2. AGENT - “DISCHARGED” (P)

132
Q

BOLDFACE:

EMERGENCY ENGINE SHUTDOWN

A
  1. THROTTLE - “IDLE” (PF)
  2. FIRE HANDLE - “PULLED” (PM)
  3. AGENT - “AS REQUIRED” (PM)
133
Q

BOLDFACE:

SMOKE/FUMES IN THE AIRPLANE

A
  1. OXYGEN - “ON, 100%” (CP, P, E)
134
Q

BOLDFACE:

LOSS OF PRESSURIZATION

A
  1. OXYGEN - “ON, 100%” (CP, P, E)

C-5M Pilot Boldface & Limitations (1 decks)

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