Limitations

Question 1

Maximum Operating Altitude

3.1.1.2

Answer 1

41,000 feet

Question 2

Maximum Flight Operation Latitude

3.1.1.3

Answer 2

82° North and 82° South

Question 3

Maximum Runway Slope

3.1.1.6.

Answer 3

+/- 2%

Question 4

Take off & landing tail wind - Maximum

3.1.1.7

Answer 4

10 knots

Question 5

Takeoff crosswind - Maximum

3.1.1.7

Answer 5

-700/-800 33 knots, -8 35 knots

Question 6

Landing crosswind - Maximum

3.1.1.7

Answer 6

-700/-800 33 knots, -8 32 knots

Question 7

Land Crosswind limit - BAR - Dry Runway

3.1.1.7

Answer 7

-700/-800 33 knots, -8 32 knots

Question 8

Land Crosswind limit - BAR - Good

3.1.1.7

Answer 8

-700/-800 33 knots. -8 32 knots

Question 9

Land Crosswind limit - BAR - Good to Medium

3.1.1.7

Answer 9

All 25 Knots

Question 10

Land Crosswind limit - BAR - Medium

3.1.1.7

Answer 10

All 20 knots

Question 11

Land Crosswind limit - BAR - Medium to Poor

3.1.1.7

Answer 11

All 15 knots

Question 12

Land Crosswind limit - BAR - Poor

3.1.1.7

Answer 12

All 10 knots

Question 13

Maximum Speeds

3.1.1.10

Answer 13

Observe Gear and flap placards

Question 14

Escape Slide Retention Bar On revenue passenger flights during taxi , takeoff, and landing

3.1.1.11

Answer 14

Installed

Question 15

Autopilot Engaged - Minimum Altitude - Takeoff

3.2.2

Answer 15

400 feet AGL

Question 16

Autopilot Engaged - Minimum Altitude - Single channel operation during approach

3.2.2

Answer 16

50 feet AGL

Question 17

Engine Limitations and Display Markings - Maximum and Minimum Limits

3.4.1

Answer 17

Red

Question 18

Engine Limitations and Display Markings - Caution Limits

3.4.1

Answer 18

Amber

Question 19

Engine Ignition - On

3.4.2

Answer 19

Takeoff, Landing, Operation in Heavy Rain & Ant-ice operation

Question 20

Starter Duty Cycle - NG

3.4.3

Answer 20

2 Minutes On - 10 seconds between start attempts

Question 21

Starter Duty Cycle - MAX

3.4.3

Answer 21

3 Minutes On - 10 seconds between start attempts

Question 22

Reverse Thrust Intentional selection in flights

3.4.4

Answer 22

Prohibited

Question 23

APU - Bleed and Electrical Load - Maximum altitude

3.4.5

Answer 23

10,000 feet

Question 24

APU - Bleed Only - Maximum altitude

3.4.5

Answer 24

17,000 feet

Question 25

APU - Electrical load only - Maximum altitude ## Footnote 3.4.5

Answer 25

41,000 feet

Question 26

What must be avoided with a Dual Bleed light illuminated?

Answer 26

Thrust must be limited to idle

Question 27

Wide Cut Fuels JP-4 or Jet B ## Footnote 3.5.1

Answer 27

Prohibitied

Question 28

Maximum fuel tank temperature ## Footnote 3.5.2

Answer 28

49°C

Question 29

Minimum fuel tank temperautre

Answer 29

-43° C or 3°C above the freezing point of fuel being used. Whichever is higher.

Question 30

Fuel Imbalance - Allowable lateral imbalance between main and tanks 1 and 2 ## Footnote 3.5.3

Answer 30

Must be scheduled to be zero

Question 31

Random fuel imbalance for taxi, takeoff, flight or landing ## Footnote 3.5.3

Answer 31

Must not exceed 1,000 lbs

Question 32

Maximum flap extension altitude ## Footnote 3.6.1

Answer 32

20,000 feet

Question 33

Holding in icing conditions with flaps extended ## Footnote 3.6.1

Answer 33

Prohibited

Question 34

Under what conditions must engine anti-ice be selected on?

Answer 34

When icing conditions exist or are anticipated, except during climb and cruise below -40°C SAT. Icing conditions are defined as, the ambient temperature is +10°C or below and any of the following conditions exist; Visible moisture such as clouds or fog with visibility less than 1nm, rain, snow, sleet, or ice crystals; Standing water, ice, snow, is present on ramps, taxiways, or runways.

Question 35

Speedbrakes - Minimum radio altitudes for deployment in flight ## Footnote 3.6.2

Answer 35

1,000 feet

Question 36

Under what conditions are reduced thrust takeoffs not permitted?

Answer 36

Slippery or contaminated runways, anti skid inop, when special departure procedures specify max Thrust for T/O, wind shear is present, or EEC in alternate mode

Question 37

Maximum Differential ## Footnote 3.9.1

Answer 37

9.1 PSI

Question 38

AUTOLAND Maximum allowable wind speeds when landing weather minima are predicated on autoland operations? FOM 3.2.3

Answer 38

Headwind 25 knots; Tailwind 10 knots; Maximum crosswind 20 knots; and Autoland capability may only be used with flaps 30 or 40 and both engines operative. Not authorized for overweight landings. The maximum and minimum glideslope angles are 3.25 and 2.5 degrees, respectively.

Question 39

Engine Warm Up Requirement FOM 4.5.1

Answer 39

(B737NG) Verify an increase in engine oil temperature before takeoff (B737MAX) Verify engine oil temperature is at or above 31°C before takeoff Run the engine, for at least 2 minutes (B737NG) or 3 minutes (B737MAX), using a thrust setting normally used for taxi operations before applying takeoff thrust