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MQF study cards T38 > 1T-38C-1 > Flashcards

1T-38C-1 Flashcards

1
Q

A3V149. The _______ sensing system varies the nozzle area to maintain EGT within limits at
both MIL and MAX range throttle positions. (T.O. 1T-38C-1)
A. T2
B. T5
C. T8
D. T4
Reference:

A

B. T5

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2
Q

A3V151. The throttles, when placed at OFF, electrically shut off fuel to the engine at the main
fuel control and mechanically shut off fuel to the engine at the fuel shutoff valves. (T.O.
1T-38C-1)
True
False

A

False

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3
Q

A3V209. If you suspect engine damage during a compressor stall, you should: (T.O. 1T-38C-1)
A. advance the throttle above idle only if required.
B. never advance the throttle above idle.
C. advance the throttle cautiously above 80% to determine the maximum usable engine
speed.

A

A. advance the throttle above idle only if required.

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4
Q

A3V210. A compressor stall may be recovered prior to complete flameout by: (T.O. 1T-38C-1)
A. selecting MAX power.
B. rapidly retarding the throttle to idle.
C. pressing the affected engine’s start button.
D. a and c
E. b and c

A

E. b and c

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5
Q 
A3V212. If the engine cannot be shut down with the throttle, the \_\_\_\_\_ switch (affected engine)
should be closed. (T.O. 1T-38C-1)
A. boost pump 
B. fuel shutoff
C. crossfeed
D. generator
A

B. fuel shutoff

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6
Q

A3V213. With boost pumps inoperative, engine flameout may occur if above 25,000 feet. (T.O.
1T-38C-1)
True
False

A

True

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7
Q

A3V214. Vibrations accompanied by fumes and/or odors from the air conditioning system may
indicate air conditioner turbine failure. You should _____. (T.O. 1T-38C-1)
A. select oxygen - 100%
B. descend below FL250
C. select RAM DUMP
D. all of the above
E. B and C

A

D. all of the above

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8
Q 
A3V215. After losing a canopy, the minimum drag airspeed is approximately \_\_\_\_\_ KIAS. (T.O.
1T-38C-1)
A. 200
B. 225
C. 250
D. 275
A

B. 225

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9
Q

A3V216. Simultaneous failure of the engine RPM and oil pump (oil pressure zero) may be an
indication of: (T.O. 1T-38C-1)
A. Airframe mounted gearbox failure.
B. Left generator failure without crossover.
C. Right generator failure without crossover.
D. Oil pump shaft shear.

A

D. Oil pump shaft shear.

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10
Q

A3V217. If the operating engine requires shutdown, the previously shutdown engine for an oil
system malfunction may be restarted. (T.O. 1T-38C-1)
True
False

A

True

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11
Q

A3V218. Under controlled flight, do not delay ejection below _______ feet in futile attempts to
start the engines or for other reasons that may commit you to an unsafe ejection. (T.O.
1T-38C-1)
A. 1,000
B. 2,000
C. 5,000
D. 15,000

A

B. 2,000

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12
Q

A3V220. Simultaneous illumination of the generator and hydraulic caution lights for the same
engine may indicate a gearbox failure. This can be confirmed by checking the appropriate _____
indicator. (T.O. 1T-38C-1)
A. oil pressure
B. hydraulic pressure
C. nozzle

A

B. hydraulic

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13
Q

A3V221. Hydraulic pressure provided solely by a windmilling engine will allow control of the
aircraft for landing. (T.O. 1T-38C-1)
True
False

A

False

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14
Q

A3V222. If utility hydraulic pressure is depleted: (T.O. 1T-38C-1)
A. land with all gear up.
B. stop straight ahead and have the gear pins installed prior to clearing the runway.
C. the flight control hydraulic system backs up all the utility driven systems.
D. the flaps will not extend.

A

B. stop straight ahead and have the gear pins installed prior to clearing the runway.

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15
Q

A3V223. With dual hydraulic system failure: (T.O. 1T-38C-1)
A. eject.
B. hydraulic pressure provided solely by a windmilling engine is sufficient to control the aircraft
for landing
C. land as soon as conditions permit.
D. b and c.

A

A. eject.

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16
Q

A3V224. Touchdowns as high as _______ KCAS are possible. (T.O. 1T-38C-1)
A. 180
C. 220
D. 240

A

B. 200

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17
Q

A3V225. If takeoff is made with flap-slab interconnect system failure (non-locking): (T.O.
1T-38C-1)
A. a lighter than normal stick force will be required for rotation.
B. a reduced amount of stick travel will be required for rotation.
C. until the flaps are retracted, significant forward stick pressure will be required to keep the
pitch from increasing.
D. all of the above.

A

D. all of the above.

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18
Q

A3V227. During single-engine landing, at high density altitude or high gross weights, selecting
full flaps in the flare, an immediate touchdown and premature landing may occur. (T.O.
1T-38C-1)
True
False

A

True

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19
Q

A3V230. Vibrations accompanied by fumes and/or odors from the air-conditioning system may
indicate failure of the _______. (T.O. 1T-38C-1)
A. air conditioner turbine
B. right/left airframe mounted gearbox
C. right/left generator
D. right/left oil pump shaft

A

A. air conditioner turbine

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20
Q 
A3V231. Normal load capacity of the WSSP is approximately \_\_\_\_\_ pounds. (T.O. 1T-38C-1)
A. 130
B. 140
C. 150
D. 160
A

B. 140

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21
Q

A3V232. An overstress failure of the main landing gear sidebrace trunion may occur if the gear
is: (T.O. 1T-38C-1)
A. extended with greater than 30 degrees of bank.
B. extended/retracted with greater than 45 degrees of bank.
C. extended at greater than 1.5 Gs. D. b or c above.

A

D. b or c above.

22
Q 
A3V234. The nosewheel tire is rated to \_\_\_ knots groundspeed. (T.O. 1T-38C-1) 
A. 174
B. 195
C. 204
D. SETOS+10.
A

A. 174

23
Q 
A3V237. Nozzle position at MIL is \_\_\_\_\_\_\_%. (T.O. 1T-38C-1) 
A. 0 - 20
B. 20 - 55
C. 50 - 85
D. 50 - 100
A

A. 0-20

24
Q

A3V240. If full aileron deflection in the direction of the spin is not maintained, spin recovery may
be prolonged or prevented. (T.O. 1T-38C-1)
True
False

A

True

25
Q

A3V241. If normal crossfeed operation is continued until the active system runs dry:(T.O.
1T-38C-1)
A. dual engine flameout will occur.
B. gravity feed will supply sufficient fuel from the other fuel system.
C. only the corresponding engine will flameout.
D. engine restart will be impossible due to air in the lines.

A

A. dual engine flameout will occur.

26
Q

A3V243. If flight through moderate precipitation is unavoidable, you should: (T.O. 1T-38C-1)
A. slow to minimum practical airspeed to lessen rain damage.
B. fly at maximum practical airspeed to minimize time in the precipitation.
C. set a high power

A

A. slow to minimum practical airspeed to lessen rain damage

27
Q 
A3V244. Flight in moderate precipitation may damage the: (T.O. 1T-38C-1) 
A. nose cone.
B. vertical stabilizer. 
C. canopies. 
D. A or B.
A

D. A or B.

28
Q

A3V245. The recommended best penetration airspeed if turbulence and thunderstorms are
experienced is _______ KCAS. (T.O. 1T-38C-1)
A. 250
B. 280
C. 300
D. 350

A

B. 280

29
Q

A3V247. On solo missions, the rear cockpit standby ADI should be _____. (T.O. 1T-38C-1)
A. caged
B. uncaged

A

B. uncaged

30
Q 
A3V248. Which of the following component(s) is(are) lost when the cabin pressure switch is placed in RAM DUMP? (T.O. 1T-38C-1)
A. Anti-G suit.
B. Canopy defog.
C. Cabin pressurization.
D. Air conditioning systems. 
E. All of the above.
A

E. All of the above.

31
Q 
A3V249. The aircraft stall is characterized by airframe buffet and a \_\_\_\_\_\_ rather than by a clean nose-down pitch motion. (T.O. 1T-38C-1) 
A. high sink rate.
B. wing rock.
C. nose-up pitch motion.
D. all of the above
A

A. high sink rate.

32
Q

A3V252. Throttle friction can be adjusted: (T.O. 1T-38C-1)
A. only by ground maintenance.
B. from the rear cockpit anytime.
C. is not adjustable.

A

A. only by ground maintenance.

33
Q

A3V254. Placing either or both fuel shutoff switches to the CLOSED position shuts off fuel flow to
either or both engines in approximately _____ second(s) without using the throttles. (T.O.
1T-38C-1)
A. 1
B. 3
C. 5
D. 10

A

A. 1

34
Q 
A3V259. Activation of the speedbrake requires \_\_\_\_\_ power. (T.O. 1T-38C-1) 
A. hydraulic and DC.
B. hydraulic and AC.
C. AC and DC.
D. hydraulic, AC, and DC.
A

A. hydraulic and DC.

35
Q

A3V264. What will be the correct indications after practicing alternate gear extension, with the
landing gear lever in the LG UP position? (T.O. 1T-38C-1)
A. Three green, light out in handle, horn sounding.
B. Three green, light on in handle, horn sounding.
C. Three green, light on in handle, horn not sounding.

A

C. Three green, light on in handle, horn not sounding.

36
Q

A3V268. During start, if ignition does not occur before fuel flow reaches 360 LB/HR, retard the
throttle to OFF and: (T.O. 1T-38C-1)
A. abort the aircraft.
B. maintain airflow to permit fuel and vapors to purge.
C. wait a minimum of 2 minutes before attempting another start. D. b and c above.

A

D. b and c above.

37
Q 
A3V272. Fuel required for a go-around (closed pattern) is approximately \_\_\_\_\_ pounds. (T.O.
1T-38C-1)
A. 100 
B. 150
C. 200
D. 250
A

B. 150

38
Q

A3V273. Extreme nose high aerobraking when crossing raised arresting cables may result in damage to the _____. (T.O. 1T-38C-1)
A. afterburner ejectors
B. main tires
C. main gear doors

A

A. afterburner ejectors

39
Q 
A3V274. Allow \_\_\_\_\_ seconds for landing-taxi light retraction and (or) closure of ram dump door prior to engine shutdown. (T.O. 1T-38C-1)
A. 2
B. 5 
C. 10
D. 20
A

C. 10

40
Q

A3V275. The canopy seals will remain inflated if the engines are shutdown with _____, making
the canopies more difficult to open. (T.O. 1T-38C-1)
A. both canopies locked
B. either canopy locked
C. the front canopy locked

A

A. both canopies locked

41
Q 
A3V278. Aerodynamic braking is more effective than cautious wheel braking above \_\_\_\_\_. (T.O.
1T-38C-1) 
A. 100 KCAS
B. MACS
C. NACS
D. 120 KCAS
A

A. 100 KCAS

42
Q

A3V281. During a single-engine takeoff/go-around, at high gross weight, with the landing gear
extended, flap retraction should not be initiated prior to _______ KCAS. (T.O. 1T-38C-1)
A. 190
B. 200
C. 220
D. 240

A

C. 220

43
Q

A3V283. _____ should be attempted immediately upon detection of dual engine flameout at low altitudes, if time permits. (T.O. 1T-38C-1)
A. Ejection
B. Normal Restart
C. Alternate Airstart

A

C. Alternate Airstart

44
Q 
A3V291. The minimum altitude recommended for bailout in a controlled situation is \_\_\_\_\_ feet AGL. (T.O. 1T-38C-1)
A. 1500 
B. 2000
C. 2500 
D. 3000
A

B. 2000

45
Q

A3V295. If you suspect brake fluid venting overboard, pump the brakes in flight to ensure you will
have pressure after landing. (T.O. 1T-38C-1)
True
False

A

False

46
Q

A3V297. If you suspect the right brake system has failed, with no other directional control problems, plan to land in (on) the _____ of the runway. (T.O. 1T-38C-1)
A. right side.
B. left side.
C. center.

A

C. center.

47
Q 
A3V301. At full afterburner, the nozzles should read between \_\_\_\_\_\_\_. (T.O. 1T-38C-1)
A. 0 - 20
B. 5 - 20
C. 20 - 55 
D. 50 - 85
A

D. 50 - 85

48
Q

A3V302. During cold weather starts, oil pressure above 55 PSI may be observed. As the oil
warms up, oil pressure should continue to decrease and return to normal operating limits. (T.O.
1T-38C-1)
True
False

A

True

49
Q 
A3V303. Crossfeeding is recommended when fuel differences exceed \_\_\_\_\_ pounds. (T.O.
1T-38C-1)
A. 100
B. 150 
C. 200
D. 175
A

C. 200

50
Q 
A3V305. Which of the following components is NOT lost when the cabin pressure switch is
placed at RAM DUMP? (T.O. 1T-38C-1)
A. Anti-G suit
B. Canopy defog 
C. Anti-ice
D. Air conditioner
A

C. Anti-ice

MQF study cards T38 (8 decks)

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