737 limitations

Question 1

Max tailwind component - takeoff

Answer 1

15 kts

Question 2

Max tailwind component - landing

Answer 2

15 kts

Question 3

Max operating altitude

Answer 3

41,000ft

Question 4

Max takeoff and landing altitude

Answer 4

8,400ft

Question 5

Minimum takeoff and landing temperature

Answer 5

-54°C

Question 6

Maximum Operating Limit Speed

Answer 6

Observe Vmo/Mmo and Gear/Flap placards

Question 7

Severe turbulence penetration speed

Answer 7

280 kts or .76M (whichever is lower)

Question 8

Do NOT operate air conditioning packs in HIGH with

Answer 8

either or both engine bleed air switches ON for takeoff, approach, or landing.

Question 9

Engine Anti-Ice must be ON when

Answer 9

icing conditions exist or are anticipated (on the ground or in flight) EXCEPT during climb or cruise below -40°C SAT and prior to and during descent in ALL icing conditions, including below -40°C SAT.

Question 10

Autopilot must be disengaged below

Answer 10

1000ft AGL on takeoff
Below 50ft AGL on single channel approach
Below 500ft AGL on manually flown HGS AIII (A3) approach

Question 11

NO AILERON TRIM with

Answer 11

autopilot engaged.

Question 12

Engine must run for

Answer 12

3 minutes prior to takeoff and 3 minutes before shutdown (at or near idle - taxi thrust OK)

Question 13

Max time limit for takeoff thrust

Answer 13

5 minutes*

*10 minutes if single engine after takeoff

Question 14

ENGINE START switches must be in CONT position for

Answer 14

Takeoff
Landing
Anti-ice operation
Hail, sleet, or moderate to heavy rain

Question 15

ENGINE START switches must be in FLT position for

Answer 15

operation in severe turbulence.

Question 16

Minimum oil temperature before setting takeoff thrust

Answer 16

MAX only - +31°C, no limit for NG

Question 17

Reverse thrust in flight is

Answer 17

prohibited

Question 18

Bleed & Electric (APU load) Max Altitude

Answer 18

10,000ft

Question 19

Bleed Only (APU load) Max Altitude

Answer 19

17,000ft

Question 20

Electric Only (APU load) Max Altitude

Answer 20

41,000ft

Question 21

Max Operating Altitude (APU load) Max Altitude

Answer 21

41,000ft

Question 22

The APU BLEED AIR switch must be CLOSED for 2 minutes after

Answer 22

start and 1 minute before shutdown (turning the switch off meets this time limit automatically)

Question 23

Avoid power above idle with the

Answer 23

with the APU bleed valve open.

Question 24

APU bleed valve must be CLOSED when

Answer 24

another source is pressurizing L bleed air duct.

Question 25

Max altitude for flap extension

Answer 25

20,000ft

Question 26

Holding in icing conditions with flaps extended is

Answer 26

prohibited

Question 27

No speed brakes below

Answer 27

1,000ft AGL

Question 28

In flight, do NOT extend SPEED BRAKE lever beyond

Answer 28

the FLIGHT DETENT (shouldn’t allow you to anyways)

Question 29

Do not deploy speed brakes with more than

Answer 29

Flaps 10 extended

Question 30

Do not manually override the

Answer 30

Load Alleviation System.

Question 31

Minimum fuel temperature

Answer 31

-37°C (unless actual fuel freeze point is known).

Question 32

Fuel imbalance must be scheduled to be

Answer 32

zero.

Question 33

No more than 1,000lbs imbalance for

Answer 33

taxi, takeoff, flight, or landing.

Question 34

Main tanks must be FULL with more than

Answer 34

1,000lbs in center tank.

Question 35

On the ground center tank fuel pumps must be OFF with less than

Answer 35

1,000lbs in tank (except for defueling or transferring fuel).

Question 36

Center tank fuel pumps must be OFF unless

Answer 36

someone is in the flight deck to monitor LOW PRESSURE lights

Question 37

Center tank fuel pumps must be turned OFF when

Answer 37

low pressure light illuminates (under 1000lbs) or the tank is empty.

Question 38

Ground operation of electric hydraulic pump requires minimum

Answer 38

1675 in respective fuel tank.