B 737-400 _ Quizlet 1
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Transcript of B 737-400 _ Quizlet 1
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7/29/2019 B 737-400 _ Quizlet 1
1/3
25/01/2013 Testing 737-400 | Quizlet
quizlet.com/2577700/test/
e
c
d
a
b
1. Max N1RPM
INCORRECT:No answer given
ANSWER: 106%
2. autoland may be used, config settings
INCORRECT:No answer given
ANSWER: with flaps 30 or 40 and both engines
operative.
3. Reverse Thrust
INCORRECT:No answer given
ANSWER: Intentional selection of RT is probihited
4. (Engine)Max Continuous EGT
INCORRECT:No answer given
ANSWER: 895C
5. Gear: Max Spd Extd:
INCORRECT:No answer given
ANSWER: 320 kt / M.82
5 Written Questions
1. Do not reset a tripped fuel pump CB
INCORRECT: You gave no answer
ANSWER: Fuel pump CB
2. 17,000 feet
INCORRECT: You gave no answer
ANSWER: with APU bleed , max alt
3. Random fuel imbalance must not exceed 453 Kgs at anytime
INCORRECT: You gave no answer
ANSWER: Fuel Balance -imbalance
4. vor app- must have raw data displayed no later than FAF
INCORRECT: You gave no answer
ANSWER: FMC earlier than U7.2
5. 51,255 kgs
INCORRECT: You gave no answer
ANSWER: Max Zero Fuel Weight
5 Matching Questions
737-400 - 20 Questions
NAME: ________________________
a 895C
b 320 kt / M.82
c with flaps 30 or 40 and both engines operative.
d Intentional selection of RT is probihited
e 106%
F0%
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25/01/2013 Testing 737-400 | Quizlet
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5 Multiple C hoice Questions
1. Do not apply brakes until after touchdown
(No Answer)
a. Engine TAI
b. Max N2RPM
c. CORRECT:Landing Gear
d. Max Landing Weight
2. 45 feet
(No Answer)
a. RVSM Operations Max Difference between Capt or F/O and Field elevation - Sea level
b. RVSM Operations Max Allowable Difference Between Captain and First Officer altitude Displays- In Flight
c. RVSM Operations Max Difference between Capt or F/O and Field elevation - 5000 feet
d. CORRECT:RVSM Operations Max Allowable Difference Between Captain and First Officer altitude Displays - On the Ground - Field
Eleveation - 5000 feet
3. Min fuel temp -45C or freezing point +3C, whichever is higher (jet A1 - FP -47C)
(No Answer)
a. Fuel pump CB
b. Max fuel temp
c. Engine TAI
d. CORRECT:Min Fuel temp
4. must be on when icing conditions/anticipated, except during climb and cruise below -40C SAT
(No Answer)
a. Tyre
b. Reverse Thrust
c. Wx Radar
d. CORRECT:Engine TAI
5. 20,000 feet
(No Answer)
a. Max Takeoff Weight
b. CORRECT:max flap extension alt
c. Max fuel temp
d. Max Landing Weight
5 True/False Questions
1. Max TailWind Component 63,049 kgs
This is false. You gave no answer.
It should be Max TailWind Component 15 Knots.
2. CG. Limits Use Approved Weight n Bal Sys
This is true. You gave no answer.
3. speed brake do not extend beyond FLIGHT DETENT in flight
This is true. You gave no answer.
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7/29/2019 B 737-400 _ Quizlet 1
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25/01/2013 Testing 737-400 | Quizlet
quizlet.com/2577700/test/
4. Apu bleed valve must be closed when ground air .1 bleed valve open
This is false. You gave no answer.
It should be Apu bleed valve must be cl osed when ground air connected and isolation valve open.
5. Gear: Max Spd Ext: 270 kt / M.82
This is true. You gave no answer.