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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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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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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.