Limitations

Question 1

Maximum Tailwind for Takeoff and Landing

Answer 1

15 knots

*10 kts for takeoff on contaminated runway

*5 kts for landing IF BA < GOOD and LDA < 7,000’

Question 2

Maximum Steady State and Gust Wind

Answer 2

Steady State - 50 knots

Gust - 20 knots

Question 3

Maximum Takeoff Crosswind (dry runway)

Answer 3

700 - 40kts

8/900 - 33kts

MAX - 34kts

Question 4

Maximum Takeoff Crosswind WET/BA GOOD

Answer 4

25 knots

Question 5

Maximum Landing Crosswind (dry runway)

Answer 5

700 and MAX - 40 knots

800 and 900 - 37 knots

Question 6

Maximum Operating Altitude

Answer 6

41,000’

Question 7

Maximum Takeoff and Landing Altitude

Answer 7

8,400’

Question 8

Minimum Temperature for Takeoff and Landing (max?)

Answer 8

Minimum -54C

Maximum +54C at sea-level

Question 9

Maximum Operating Speed Limit

Answer 9

Vmo/Mmo and Gear/Flap placards

Question 10

Severe Turbulence Penetration Target Speed

Answer 10

280 KIAS / .76M

Whichever is lower

Question 11

When must the A/C packs not be in HIGH?

Answer 11

Takeoff, approach, and landing

If engine bleed(s) ON

Question 12

When must EAI be on?

Answer 12

During all ground and flight operations when icing conditions exist or are anticipated

Except during climb/cruise below -40C SAT

Question 13

Minimum altitude to engage autopilot

Answer 13

1,000’ AGL

Question 14

Minimum altitude to leave autopilot engaged

Answer 14

50’ AGL for single-channel approaches

500’ AGL for hand-flown HGS AIII

Question 15

Aileron trim with autopilot engaged?

Answer 15

Prohibited

Question 16

Engine warm-up and cool-down time

Answer 16

3 minutes

31C oil temperature for 737MAX

Question 17

Maximum time for takeoff thrust

Answer 17

5 minutes

Unless OEI then 10 minutes

Question 18

Engine Start switches must be in CONT for

Answer 18

Takeoff

Landing

Anti-Ice operation

Rain (moderate to heavy), hail, and sleet

Question 19

Engine Start Switches must be in FLT for

Answer 19

Severe turbulence

Question 20

Minimum oil temperature before setting takeoff thrust

Answer 20

31C

MAX only

Question 21

Reverse thrust selection in-flight

Answer 21

Prohibited

Question 22

APU altitude limits

Answer 22

41,000’ - Operating and electrics
17,000’ - Bleed load
10,000’ - Bleed and electrical load

Question 23

APU Bleed warm-up/cool-down time

Answer 23

2 minutes for warm up

1 minute for cool down (automatically met)

Question 24

Maximum Flap Extension Altitude

Answer 24

20,000’

Question 25

Holding in icing conditions with flaps extended

Answer 25

Prohibited

Question 26

Minimum height for speed brake deployment in-flight

Answer 26

1,000' AGL

Question 27

Maximum speed brake deployment position in-flight

Answer 27

FLIGHT DETENT

Question 28

Maximum flap position for speed brake deployment

Answer 28

Flaps 10 *Avoid with flaps extended if possible

Question 29

Load alleviation system

Answer 29

Manual override prohibited

Question 30

Maximum altimeter differences

Answer 30

50' between CA and FO on the ground 75' between CA or FO and field elevation 200' in flight for RVSM

Question 31

Minimum fuel temperature (max?)

Answer 31

-37C Unless fuel freeze point is known Then freeze point +3C minimum -43C (Maximum +49C)

Question 32

Maximum fuel imbalance between main tanks

Answer 32

Scheduled to be zero Fuel imbalance must not exceed 1,000lbs for taxi, takeoff, flight, or landing

Question 33

How much fuel can be in the center tank if main tanks are less than full?

Answer 33

1,000lbs Main tanks must be scheduled to be full if the Center Tank has more than 1,000lbs

Question 34

Center Tank Fuel Pump Limits

Answer 34

Must not be on unless personnel in flight deck to monitor LOW PRESSURE lights, and Center fuel quantity must be > 1,000lbs to operate them on the ground, except for defueling or transferring fuel (also no pax onboard), and Center fuel pump must be switched OFF when LOW PRESSURE light illuminates, intentional dry running of center fuel pump prohibited

Question 35

Minimum fuel quantity for ground operation of electric hydraulic pumps?

Answer 35

1,675lbs in respective main fuel tank *does not apply after landing

Question 36

*Bleed duct pressure limits

Answer 36

60 psi - Max 18 psi - Min in-flight 15 psi - Min on the ground Report differential > 20 psi to MX Also, do not operate packs in HIGH for takeoff, approach, or landing

Question 37

*Cold soaked fuel frost

Answer 37

Up to 1/8" permitted on lower wing Upper wing -within the "box" -OAT >= 4C -Fuel temp >= -16C -No precipitation or visible moisture

Question 38

*Assumed temperature thrust reduction

Answer 38

Prohibited for -Windshear -Contaminated runway -MEL (antiskid, EEC ALTN, dual FMC inop) -27k bump

Question 39

*Cargo door wind limits

Answer 39

Fully open up to 40 knots CANOPY up to 65 knots Lower door to CANOPY if door begins oscillating

Question 40

*Navigation performance scales

Answer 40

RNP < 0.3 - A/P or NPS required RNP < 0.11 - NPS required

Question 41

*Starter duty cycle

Answer 41

NG - 2 min on MAX - 3 min on 10 seconds off for second and subsequent attempts

Question 42

*Wing anti-ice

Answer 42

Do not use on the ground when OAT > 10C Do not using on the ground AFTER deicing

Question 43

*Minimum in-flight temperature

Answer 43

-72C at FL350 (-73C at 410)