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unnamed > 1C-135(RC)-1 Sec 5 > Flashcards

1C-135(RC)-1 Sec 5 Flashcards

This flashcard deck was created using Flashcardlet's card creator

1
Q

EGT limit (max continuous)

A

610 - 870 degrees C

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2
Q

EGT limit (flight idle)

A

> 390 degrees C

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3
Q

EGT limit (starting)

A

725 degrees C

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4
Q

Time limit (TRT)

A

5 min

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5
Q

Time limit (max continuous)

A

Continuous

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6
Q

Time limit (flight idle)

A

Continuous

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7
Q

Time limit (ground idle)

A

Continuous

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8
Q

Action taken (overspeed)

A

Retard until next landing

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9
Q

Action taken (shutdown)

A

Shutdown precautionary

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10
Q

Time limit (EGT 870 - 905)

A

5 min (TRT)

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11
Q

Action taken (EGT 906 - 930)

A

Retard until next landing

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12
Q

Action taken (EGT >930)

A

Shutdown precautionary

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13
Q

N1 limit (TRT)

A

102%

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14
Q

N1 limit (max continuous)

A

102%

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15
Q

N1 limit (flight idle)

A

30 - 70%

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16
Q

N1 limit (ground idle)

A

16 - 22%

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17
Q

N1 limit (overspeed)

A

102.1 - 105%

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18
Q

N1 limit (shutdown)

A

> 105%

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19
Q

N2 limit (TRT)

A

105%

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20
Q

N2 limit (max continuous)

A

105%

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21
Q

N2 limit (flight idle)

A

71 - 84%

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22
Q

N2 limit (ground idle)

A

54 - 62%

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23
Q

N2 limit (overspeed)

A

105.1 - 106%

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24
Q

N2 limit (shutdown)

A

> 106%

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25
Q

Oil temperature limit (TRT)

A

5 to 160 degrees C

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26
Q

Oil temperature limit (max continuous)

A

-10 to 160 degrees C

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27
Q

Oil temperature limit (flight idle)

A

-10 to 160 degrees C

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28
Q

Oil temperature limit (ground idle)

A

-50 to 160 degrees C

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29
Q

Oil temperature limit (starting)

A

-50 to 160 degrees C

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30
Q

Oil temp limit (normal range)

A

-10 to 160 degrees C

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31
Q

Oil temperature limit (EWO)

A

None

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32
Q

Time limit (Oil temp 160 - 175)

A

10 minutes

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33
Q

Action taken (oil temp >175)

A

Shutdown precautionary

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34
Q

Oil pressure limit (TRT)

A

11 - 92 psi

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35
Q

Oil pressure limit (max continuous)

A

11 - 92 psi

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36
Q

Oil pressure limit (flight idle)

A

11 psi minimum

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37
Q

Oil pressure limit (ground idle)

A

11 psi minimum

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38
Q

Oil pressure limit (starting)

A

Positive indication before idle RPM

Cold WX: positive indication before adding fuel

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39
Q

Oil pressure limit (normal range)

A

11 - 92 psi

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40
Q

Oil pressure limit (EWO)

A

Positive indication 10 seconds before T/O thrust

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41
Q

Oil pressure limit (fluctuation)

A

+/- 5 psi (10 psi total) w/in limits

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42
Q

Reserve brake limit (preload)

A

1000 psi

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43
Q

Reserve brake limit (normal range)

A

1300 - 3050 psi

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44
Q

Reserve brake limit (one application)

A

1300 psi

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45
Q

L/R hydraulic system limit (preload)

A

2000 psi

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46
Q

L/R hydraulic system limit (normal range)

A

2400 to 3050 psi

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47
Q

Powered rudder (low range)

A

2100 - 2400 psi

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48
Q

Powered rudder (high range)

A

2800 - 3050 psi

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49
Q

JFS start wait time (1st attempt; no start)

A

5 minutes

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50
Q

JFS start wait time (1st attempt; <60 seconds)

A

2 minutes

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51
Q

JFS start wait time (1st attempt; 60 - 90 seconds)

A

5 minutes

52
Q

JFS start wait time (1st attempt; >90 seconds)

A

1 hour

53
Q

JFS start wait time (2nd attempt; <90 seconds)

A

5 minutes

54
Q

JFS start wait time (2nd attempt; >90 seconds)

A

1 hour

55
Q

JFS start wait time (3rd attempt)

A

1 hour

56
Q

Pneumatic starting limit (continuous operation/cooling)

A

90 seconds / 60 seconds cooling

57
Q

Pneumatic starting limit (attempts)

A

3

58
Q

Pneumatic starting limit (cooling time after 3 attempts)

A

5 minutes

59
Q

Pneumatic motoring limit (continued operation)

A

5 minutes

60
Q

Pneumatic motoring limit (1st cooling)

A

10 minutes

61
Q

Pneumatic motoring limit (2nd attempt)

A

30 minutes

62
Q

AC frequency limit (danger/caution)

A

380 - 395 Hz

63
Q

AC frequency limit (normal)

A

400 +/- 5 Hz

64
Q

AC frequency limit (caution)

A

405 - 420 Hz

65
Q

AC volt limit (danger/caution)

A

180 - 190 VAC

66
Q

AC volt limit (normal)

A

200 +/- 10 VAC

67
Q

AC volt limit (caution)

A

210 - 220 VAC

68
Q

DC load limit (danger/caution)

A

0

69
Q

DC load limit (normal)

A

0 - 1

70
Q

DC load limit (caution)

A

1 - 1.25

71
Q

JFS/main limit w/o AC power (danger/caution)

A

= 24 VDC

72
Q

JFS/main limit w/o AC power (normal)

A

> 24 VDC

73
Q

JFS/main limit with AC power (danger/caution)

A

= 24 VDC

74
Q

JFS/main limit with AC power (normal)

A

> 24 - 29 VDC

75
Q

JFS/main limit with AC power (caution)

A

> 29 VDC

76
Q

TR limit (danger/caution)

A

<26 VDC

77
Q

TR limit (normal)

A

26 - 30 VDC

78
Q

TR limit (caution)

A

> 30 VDC

79
Q

Battery charging limit (normal)

A

0 - 7 amps

80
Q

Battery charging limit (low)

A

7 - 30 amps

81
Q

AC ammeter (maximum)

A

250 amps

82
Q

Minimum crew

A

Pilot, copilot, & navigator

p 5-1

83
Q

Emergency crew

A

Aircraft commander & copilot

or

Instructor pilot & either copilot or instructor navigator

p 5-1

84
Q

When all engines are at the same N1 setting at flight idle or above, the EGT difference between any two engines should not exceed __ degrees.

A

40

p 5-7

85
Q

An internal failure of the turbine engine monitor system (TEMS) can cause EGT indications to increase ___ to ___ degrees C above those that actually exist in the engine.

A

120 to 135

p 5-7

86
Q

Normal oil consumption

A

0.8 pints per hour

p 5-9

87
Q

Engine oil consumption in excess of ___ pints per hour or any sudden increase in oil consumption of ___ pints per hour shall be cause for rejection of the engine.

A
  1. 2
  2. 6

p 5-9

88
Q

Do not reengage the JFS above _____. Reengagement above this speed may result in JFS damage.

A

5% N2

p 5-9

89
Q

The JFS will operate for _____ seconds before automatic shutdown.

A

180 to 190 seconds

p 5-9

90
Q

Regardless of the type of fuel, takeoff shall not be attempted with any _____ inoperative, unless mission requirements dictate otherwise.

A

Boost pumps

p 5-10

91
Q

Flight under conditions where temperature is within _____ of the fuel freeze point should be avoided.

JP-8 fuel freeze point: _____

A

6 degrees C

-47 degrees C

p 5-10,5-10A

92
Q

Vmo

A

350 KIAS

.85 mach

p 5-12

93
Q

On the ground with the cg at more than _____, the airplane can be tipped over on the tail section by movement of very few persons or cargo to the aft end of the airplane.

A

35% MAC

p 5-12

94
Q

On the ground with the cg at more than _____, the airplane can be tipped over on the tail section by movement of very few persons or cargo to the aft end of the airplane.

A

35% MAC

p 5-12

95
Q

The difference in total fuel in the left wing tanks and the total fuel in the right wing tanks should not exceed _____ during air refueling.

A

1000 lbs

p 5-12

96
Q

Because of possible damage due to sonic airflow at certain angles of attack, do not extend flaps above _____.

A

20,000 feet pressure altitude

p 5-12

97
Q

g limits

A

0.2 - 2.0

p 5-12

98
Q

Maximum speed (clean configuration)

A

350 KIAS/0.85 IM

p 5-13

99
Q

Maximum speed (during landing gear - extension or retraction)

A

270 KIAS below 38,000 ft
IM = 0.85 above 38,000 ft

p 5-13

100
Q

Maximum speed (landing gear down)

A

320 KIAS below 30,500 ft
IM = 0.85 above 30,500 ft

p 5-13

101
Q

Maximum speed (emergency gear - extension, retraction, or gear down)

A

Same as clean configuration

p 5-13

102
Q

Maximum speed (wing flaps)

A

50 degrees - 200 KIAS
40 degrees - 210 KIAS
30 degrees - 220 KIAS
20 degrees - 230 KIAS

p 5-13

103
Q

Maximum speed (speed brakes)

A

Same as clean configuration

p 5-13

104
Q

Maximum speed (slipway doors)

A

Same as clean configuration

p 5-13

105
Q

On the ground, to preclude bleed air temperature from exceeding the capacity of the precooler:

(1) do not operate both air conditioning packs with fewer than _____ engines supplying bleed air

A

Four

p 5-27

106
Q

On the ground, to preclude bleed air temperature from exceeding the capacity of the precooler:

(2) do not operate either air conditioning pack with fewer than _____

A

Two

p 5-27

107
Q

On the ground, to preclude bleed air temperature from exceeding the capacity of the precooler:

(3) avoid engine operation in the _____ range in excess of _____ with either air conditioning switch in COND AIR.

A

30% - 50% N1 rpm

p 5-27

108
Q

The oxygen regulator is suitable for routine use up to _____ feet and for emergency use up to _____ feet.

A

42,000
50,000

p 5-27

109
Q

In case of a loss of cabin pressure, descent to an altitude of _____ feet or below within _____.

A

42,000
5 minutes

p 5-27

110
Q

Do not operate taxi lights on the ground for longer than _____.

A

15 min

p 5-27

111
Q

Do not operate nacelle lights on the ground for longer than _____.

A

15 minutes

p 5-27

112
Q

For TAWS to fully function the system requires:

A 
An operational radio altimeter
ADC 2
INS 2
Gear and flap position
An FMS position with GPS sensor

p 5-28

113
Q

The tires are limited to a maximum groundspeed of _____.

A

195 kts

p 5-28

114
Q

The thermal fuses may release tire pressure after accumulating _____ of kinetic energy per brake.

Heat transfer from brakes to thermal fuses may take up to _____.

A

22 million ft lbs (steel)/25 million ft lbs (carbon)

15 min (steel)/45 min (carbon)

p 5-29

115
Q

Landing gear extension decreases three-engine rate of climb approximately _____.

A

420 feet per minute

p 5-31

116
Q

Do not approach overheated brakes for _____.

A 
30 minutes (steel brakes)
45 min (carbon brakes)

p 5-31

117
Q

Peak temperatures are reached in the brake housing _____ after braking.

A

Approximately 15 min (steel brakes)

Within approximately 30 min (carbon brakes)

p 5-31

118
Q

Reserve tank transfer should not be initiated at flight gross weights above _____.

A

293,000 lbs

p 5-36G

119
Q

Weight limit - with the reserve and main tanks filled to capacity

A

322,500 lbs

p 5-38

120
Q

Weight limit - with the reserves empty and the mains full

A

293,000 lbs

p 5-38

121
Q

Weight limit - with the main wing and reserve tanks empty

A

240,000 lbs

p 5-38

122
Q

Do not exceed a fuel load of more than _____ in the aft body tank during air refueling.

A

39,450 lbs

p 5-38

123
Q

The aircraft can handle landing contact sinking speed of _____.

A

9 fps (540 fpm)

p 5-38A

124
Q

Mandatory Form 781 entries can be found on what page?

A

p 5-39

125
Q

EGT limit (TRT)

A

905 degrees C

unnamed (11 decks)

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