1C-135(RC)-1 Sec 5 Flashcards
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1
Q
EGT limit (max continuous)
A
610 - 870 degrees C
2
Q
EGT limit (flight idle)
A
> 390 degrees C
3
Q
EGT limit (starting)
A
725 degrees C
4
Q
Time limit (TRT)
A
5 min
5
Q
Time limit (max continuous)
A
Continuous
6
Q
Time limit (flight idle)
A
Continuous
7
Q
Time limit (ground idle)
A
Continuous
8
Q
Action taken (overspeed)
A
Retard until next landing
9
Q
Action taken (shutdown)
A
Shutdown precautionary
10
Q
Time limit (EGT 870 - 905)
A
5 min (TRT)
11
Q
Action taken (EGT 906 - 930)
A
Retard until next landing
12
Q
Action taken (EGT >930)
A
Shutdown precautionary
13
Q
N1 limit (TRT)
A
102%
14
Q
N1 limit (max continuous)
A
102%
15
Q
N1 limit (flight idle)
A
30 - 70%
16
Q
N1 limit (ground idle)
A
16 - 22%
17
Q
N1 limit (overspeed)
A
102.1 - 105%
18
Q
N1 limit (shutdown)
A
> 105%
19
Q
N2 limit (TRT)
A
105%
20
Q
N2 limit (max continuous)
A
105%
21
Q
N2 limit (flight idle)
A
71 - 84%
22
Q
N2 limit (ground idle)
A
54 - 62%
23
Q
N2 limit (overspeed)
A
105.1 - 106%
24
Q
N2 limit (shutdown)
A
> 106%
25
Oil temperature limit (TRT)
5 to 160 degrees C
26
Oil temperature limit (max continuous)
-10 to 160 degrees C
27
Oil temperature limit (flight idle)
-10 to 160 degrees C
28
Oil temperature limit (ground idle)
-50 to 160 degrees C
29
Oil temperature limit (starting)
-50 to 160 degrees C
30
Oil temp limit (normal range)
-10 to 160 degrees C
31
Oil temperature limit (EWO)
None
32
Time limit (Oil temp 160 - 175)
10 minutes
33
Action taken (oil temp >175)
Shutdown precautionary
34
Oil pressure limit (TRT)
11 - 92 psi
35
Oil pressure limit (max continuous)
11 - 92 psi
36
Oil pressure limit (flight idle)
11 psi minimum
37
Oil pressure limit (ground idle)
11 psi minimum
38
Oil pressure limit (starting)
Positive indication before idle RPM
Cold WX: positive indication before adding fuel
39
Oil pressure limit (normal range)
11 - 92 psi
40
Oil pressure limit (EWO)
Positive indication 10 seconds before T/O thrust
41
Oil pressure limit (fluctuation)
+/- 5 psi (10 psi total) w/in limits
42
Reserve brake limit (preload)
1000 psi
43
Reserve brake limit (normal range)
1300 - 3050 psi
44
Reserve brake limit (one application)
1300 psi
45
L/R hydraulic system limit (preload)
2000 psi
46
L/R hydraulic system limit (normal range)
2400 to 3050 psi
47
Powered rudder (low range)
2100 - 2400 psi
48
Powered rudder (high range)
2800 - 3050 psi
49
JFS start wait time (1st attempt; no start)
5 minutes
50
JFS start wait time (1st attempt; <60 seconds)
2 minutes
51
JFS start wait time (1st attempt; 60 - 90 seconds)
5 minutes
52
JFS start wait time (1st attempt; >90 seconds)
1 hour
53
JFS start wait time (2nd attempt; <90 seconds)
5 minutes
54
JFS start wait time (2nd attempt; >90 seconds)
1 hour
55
JFS start wait time (3rd attempt)
1 hour
56
Pneumatic starting limit (continuous operation/cooling)
90 seconds / 60 seconds cooling
57
Pneumatic starting limit (attempts)
3
58
Pneumatic starting limit (cooling time after 3 attempts)
5 minutes
59
Pneumatic motoring limit (continued operation)
5 minutes
60
Pneumatic motoring limit (1st cooling)
10 minutes
61
Pneumatic motoring limit (2nd attempt)
30 minutes
62
AC frequency limit (danger/caution)
380 - 395 Hz
63
AC frequency limit (normal)
400 +/- 5 Hz
64
AC frequency limit (caution)
405 - 420 Hz
65
AC volt limit (danger/caution)
180 - 190 VAC
66
AC volt limit (normal)
200 +/- 10 VAC
67
AC volt limit (caution)
210 - 220 VAC
68
DC load limit (danger/caution)
0
69
DC load limit (normal)
0 - 1
70
DC load limit (caution)
1 - 1.25
71
JFS/main limit w/o AC power (danger/caution)
= 24 VDC
72
JFS/main limit w/o AC power (normal)
>24 VDC
73
JFS/main limit with AC power (danger/caution)
= 24 VDC
74
JFS/main limit with AC power (normal)
>24 - 29 VDC
75
JFS/main limit with AC power (caution)
>29 VDC
76
TR limit (danger/caution)
<26 VDC
77
TR limit (normal)
26 - 30 VDC
78
TR limit (caution)
>30 VDC
79
Battery charging limit (normal)
0 - 7 amps
80
Battery charging limit (low)
7 - 30 amps
81
AC ammeter (maximum)
250 amps
82
Minimum crew
Pilot, copilot, & navigator
p 5-1
83
Emergency crew
Aircraft commander & copilot
or
Instructor pilot & either copilot or instructor navigator
p 5-1
84
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.
40
p 5-7
85
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.
120 to 135
p 5-7
86
Normal oil consumption
0.8 pints per hour
p 5-9
87
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.
3. 2
1. 6
p 5-9
88
Do not reengage the JFS above _____. Reengagement above this speed may result in JFS damage.
5% N2
p 5-9
89
The JFS will operate for _____ seconds before automatic shutdown.
180 to 190 seconds
p 5-9
90
Regardless of the type of fuel, takeoff shall not be attempted with any _____ inoperative, unless mission requirements dictate otherwise.
Boost pumps
p 5-10
91
Flight under conditions where temperature is within _____ of the fuel freeze point should be avoided.
JP-8 fuel freeze point: _____
6 degrees C
-47 degrees C
p 5-10,5-10A
92
Vmo
350 KIAS
.85 mach
p 5-12
93
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.
35% MAC
p 5-12
94
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.
35% MAC
p 5-12
95
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.
1000 lbs
p 5-12
96
Because of possible damage due to sonic airflow at certain angles of attack, do not extend flaps above _____.
20,000 feet pressure altitude
p 5-12
97
g limits
0.2 - 2.0
p 5-12
98
Maximum speed (clean configuration)
350 KIAS/0.85 IM
p 5-13
99
Maximum speed (during landing gear - extension or retraction)
270 KIAS below 38,000 ft
IM = 0.85 above 38,000 ft
p 5-13
100
Maximum speed (landing gear down)
320 KIAS below 30,500 ft
IM = 0.85 above 30,500 ft
p 5-13
101
Maximum speed (emergency gear - extension, retraction, or gear down)
Same as clean configuration
p 5-13
102
Maximum speed (wing flaps)
50 degrees - 200 KIAS
40 degrees - 210 KIAS
30 degrees - 220 KIAS
20 degrees - 230 KIAS
p 5-13
103
Maximum speed (speed brakes)
Same as clean configuration
p 5-13
104
Maximum speed (slipway doors)
Same as clean configuration
p 5-13
105
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
Four
p 5-27
106
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 _____
Two
p 5-27
107
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.
30% - 50% N1 rpm
p 5-27
108
The oxygen regulator is suitable for routine use up to _____ feet and for emergency use up to _____ feet.
42,000
50,000
p 5-27
109
In case of a loss of cabin pressure, descent to an altitude of _____ feet or below within _____.
42,000
5 minutes
p 5-27
110
Do not operate taxi lights on the ground for longer than _____.
15 min
p 5-27
111
Do not operate nacelle lights on the ground for longer than _____.
15 minutes
p 5-27
112
For TAWS to fully function the system requires:
```
An operational radio altimeter
ADC 2
INS 2
Gear and flap position
An FMS position with GPS sensor
```
p 5-28
113
The tires are limited to a maximum groundspeed of _____.
195 kts
p 5-28
114
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 _____.
22 million ft lbs (steel)/25 million ft lbs (carbon)
15 min (steel)/45 min (carbon)
p 5-29
115
Landing gear extension decreases three-engine rate of climb approximately _____.
420 feet per minute
p 5-31
116
Do not approach overheated brakes for _____.
```
30 minutes (steel brakes)
45 min (carbon brakes)
```
p 5-31
117
Peak temperatures are reached in the brake housing _____ after braking.
Approximately 15 min (steel brakes)
Within approximately 30 min (carbon brakes)
p 5-31
118
Reserve tank transfer should not be initiated at flight gross weights above _____.
293,000 lbs
p 5-36G
119
Weight limit - with the reserve and main tanks filled to capacity
322,500 lbs
p 5-38
120
Weight limit - with the reserves empty and the mains full
293,000 lbs
p 5-38
121
Weight limit - with the main wing and reserve tanks empty
240,000 lbs
p 5-38
122
Do not exceed a fuel load of more than _____ in the aft body tank during air refueling.
39,450 lbs
p 5-38
123
The aircraft can handle landing contact sinking speed of _____.
9 fps (540 fpm)
p 5-38A
124
Mandatory Form 781 entries can be found on what page?
p 5-39
125
EGT limit (TRT)
905 degrees C
