1C-135(RC)-1 Sec 5 Flashcards
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EGT limit (max continuous)
610 - 870 degrees C
EGT limit (flight idle)
> 390 degrees C
EGT limit (starting)
725 degrees C
Time limit (TRT)
5 min
Time limit (max continuous)
Continuous
Time limit (flight idle)
Continuous
Time limit (ground idle)
Continuous
Action taken (overspeed)
Retard until next landing
Action taken (shutdown)
Shutdown precautionary
Time limit (EGT 870 - 905)
5 min (TRT)
Action taken (EGT 906 - 930)
Retard until next landing
Action taken (EGT >930)
Shutdown precautionary
N1 limit (TRT)
102%
N1 limit (max continuous)
102%
N1 limit (flight idle)
30 - 70%
N1 limit (ground idle)
16 - 22%
N1 limit (overspeed)
102.1 - 105%
N1 limit (shutdown)
> 105%
N2 limit (TRT)
105%
N2 limit (max continuous)
105%
N2 limit (flight idle)
71 - 84%
N2 limit (ground idle)
54 - 62%
N2 limit (overspeed)
105.1 - 106%
N2 limit (shutdown)
> 106%
Oil temperature limit (TRT)
5 to 160 degrees C
Oil temperature limit (max continuous)
-10 to 160 degrees C
Oil temperature limit (flight idle)
-10 to 160 degrees C
Oil temperature limit (ground idle)
-50 to 160 degrees C
Oil temperature limit (starting)
-50 to 160 degrees C
Oil temp limit (normal range)
-10 to 160 degrees C
Oil temperature limit (EWO)
None
Time limit (Oil temp 160 - 175)
10 minutes
Action taken (oil temp >175)
Shutdown precautionary
Oil pressure limit (TRT)
11 - 92 psi
Oil pressure limit (max continuous)
11 - 92 psi
Oil pressure limit (flight idle)
11 psi minimum
Oil pressure limit (ground idle)
11 psi minimum
Oil pressure limit (starting)
Positive indication before idle RPM
Cold WX: positive indication before adding fuel
Oil pressure limit (normal range)
11 - 92 psi
Oil pressure limit (EWO)
Positive indication 10 seconds before T/O thrust
Oil pressure limit (fluctuation)
+/- 5 psi (10 psi total) w/in limits
Reserve brake limit (preload)
1000 psi
Reserve brake limit (normal range)
1300 - 3050 psi
Reserve brake limit (one application)
1300 psi
L/R hydraulic system limit (preload)
2000 psi
L/R hydraulic system limit (normal range)
2400 to 3050 psi
Powered rudder (low range)
2100 - 2400 psi
Powered rudder (high range)
2800 - 3050 psi
JFS start wait time (1st attempt; no start)
5 minutes
JFS start wait time (1st attempt; <60 seconds)
2 minutes
JFS start wait time (1st attempt; 60 - 90 seconds)
5 minutes
JFS start wait time (1st attempt; >90 seconds)
1 hour
JFS start wait time (2nd attempt; <90 seconds)
5 minutes
JFS start wait time (2nd attempt; >90 seconds)
1 hour
JFS start wait time (3rd attempt)
1 hour
Pneumatic starting limit (continuous operation/cooling)
90 seconds / 60 seconds cooling
Pneumatic starting limit (attempts)
3
Pneumatic starting limit (cooling time after 3 attempts)
5 minutes
Pneumatic motoring limit (continued operation)
5 minutes
Pneumatic motoring limit (1st cooling)
10 minutes
Pneumatic motoring limit (2nd attempt)
30 minutes
AC frequency limit (danger/caution)
380 - 395 Hz
AC frequency limit (normal)
400 +/- 5 Hz
AC frequency limit (caution)
405 - 420 Hz
AC volt limit (danger/caution)
180 - 190 VAC
AC volt limit (normal)
200 +/- 10 VAC
AC volt limit (caution)
210 - 220 VAC
DC load limit (danger/caution)
0
DC load limit (normal)
0 - 1
DC load limit (caution)
1 - 1.25
JFS/main limit w/o AC power (danger/caution)
= 24 VDC
JFS/main limit w/o AC power (normal)
> 24 VDC
JFS/main limit with AC power (danger/caution)
= 24 VDC
JFS/main limit with AC power (normal)
> 24 - 29 VDC
JFS/main limit with AC power (caution)
> 29 VDC
TR limit (danger/caution)
<26 VDC
TR limit (normal)
26 - 30 VDC
TR limit (caution)
> 30 VDC
Battery charging limit (normal)
0 - 7 amps
Battery charging limit (low)
7 - 30 amps
AC ammeter (maximum)
250 amps
Minimum crew
Pilot, copilot, & navigator
p 5-1
Emergency crew
Aircraft commander & copilot
or
Instructor pilot & either copilot or instructor navigator
p 5-1
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
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
Normal oil consumption
0.8 pints per hour
p 5-9
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.
- 2
- 6
p 5-9
Do not reengage the JFS above _____. Reengagement above this speed may result in JFS damage.
5% N2
p 5-9
The JFS will operate for _____ seconds before automatic shutdown.
180 to 190 seconds
p 5-9
Regardless of the type of fuel, takeoff shall not be attempted with any _____ inoperative, unless mission requirements dictate otherwise.
Boost pumps
p 5-10
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
Vmo
350 KIAS
.85 mach
p 5-12
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
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
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
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
g limits
0.2 - 2.0
p 5-12
Maximum speed (clean configuration)
350 KIAS/0.85 IM
p 5-13
Maximum speed (during landing gear - extension or retraction)
270 KIAS below 38,000 ft
IM = 0.85 above 38,000 ft
p 5-13
Maximum speed (landing gear down)
320 KIAS below 30,500 ft
IM = 0.85 above 30,500 ft
p 5-13
Maximum speed (emergency gear - extension, retraction, or gear down)
Same as clean configuration
p 5-13
Maximum speed (wing flaps)
50 degrees - 200 KIAS
40 degrees - 210 KIAS
30 degrees - 220 KIAS
20 degrees - 230 KIAS
p 5-13
Maximum speed (speed brakes)
Same as clean configuration
p 5-13
Maximum speed (slipway doors)
Same as clean configuration
p 5-13
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
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
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
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
In case of a loss of cabin pressure, descent to an altitude of _____ feet or below within _____.
42,000
5 minutes
p 5-27
Do not operate taxi lights on the ground for longer than _____.
15 min
p 5-27
Do not operate nacelle lights on the ground for longer than _____.
15 minutes
p 5-27
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
The tires are limited to a maximum groundspeed of _____.
195 kts
p 5-28
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
Landing gear extension decreases three-engine rate of climb approximately _____.
420 feet per minute
p 5-31
Do not approach overheated brakes for _____.
30 minutes (steel brakes) 45 min (carbon brakes)
p 5-31
Peak temperatures are reached in the brake housing _____ after braking.
Approximately 15 min (steel brakes)
Within approximately 30 min (carbon brakes)
p 5-31
Reserve tank transfer should not be initiated at flight gross weights above _____.
293,000 lbs
p 5-36G
Weight limit - with the reserve and main tanks filled to capacity
322,500 lbs
p 5-38
Weight limit - with the reserves empty and the mains full
293,000 lbs
p 5-38
Weight limit - with the main wing and reserve tanks empty
240,000 lbs
p 5-38
Do not exceed a fuel load of more than _____ in the aft body tank during air refueling.
39,450 lbs
p 5-38
The aircraft can handle landing contact sinking speed of _____.
9 fps (540 fpm)
p 5-38A
Mandatory Form 781 entries can be found on what page?
p 5-39
EGT limit (TRT)
905 degrees C
