Limitations

Question 1

Operating Pressure Altitude

Answer 1

41,000 feet

Question 2

Takeoff/Landing Pressure Altitude

Answer 2

10,000 feet

Question 3

Minimum runway width

Answer 3

100 feet (30 meters)

Question 4

MAXIMUM TAKEOFF/LANDING TAILWIND COMPONENT

Answer 4

★15 knots

Question 5

Maximum gear extension speed

Answer 5

270 knots/.82 Mach

Question 6

SEVERE TURBULENCE PENETRATION SPEED

Answer 6

★280 knots/.76 Mach

Question 7

Takeoff Crosswind Component Guidelines
6 dry
5 wet
Landing

Answer 7

33
25
37

Question 8

Maximum cabin pressure differential

Answer 8

9.10 psi

Question 9

Limit on pack takeoff

Answer 9

When engine bleeds are on (either one or both), do not operate air conditioning
packs in high for takeoff, approach, and landing.

Question 10

Duct pressure

Answer 10

A duct pressure difference of more than 8 PSI may indicate a mechanical
malfunction. If a duct pressure split is observed after bleeds are configured for
flight, and the lowest indication is approximately 18 PSI or less, contact
Maintenance

Question 11

Engine anti ice ground

Answer 11

OAT 10c or below
Visible moisture in any form is present (i.e., clouds, fog with visibility of 1 mile
or less, rain, snow, sleet, or ice crystals), or
While operating on ramps, taxiways, or runways where snow, standing water,
or slush may be ingested by the engines or freeze on the engines, nacelles,
or engine sensor probes.

Question 12

Engine anti ice flight

Answer 12

10 c TAT

Question 13

Engine ignition regarding anti ice

Answer 13

Must be turned on before anti ice

Question 14

Window heat on prior to takeoff time

Answer 14

10 min

Question 15

Minimum Altitude for Use of Autopilot on Approach

Answer 15

ILS/GLS coupled approaches (no autoland) ★50 feet AGL
Non-precision approaches ★50 feet below MDA/DA

Question 16

Level change

Answer 16

Do not use LVL CHG on final approach below 1000 feet AFE.

Question 17

Normal starter duty cycle:

Answer 17

Multiple consecutive start attempts are permitted. Each start attempt is limited to
2 minutes (700/800/900/9ER)/3 minutes (MAX) of starter usage.

Question 18

Reduced thrust in ALTN mode

Answer 18

Operation with assumed temperature reduced for takeoff thrust is not permitted
with the Electronic Engine Control (EEC) in ALTN mode.

Question 19

APU MAXIMUM ALTITUDE
Bleed electrical

Answer 19

APU bleed and electrical 10,000 feet
APU bleed 17,000 feet
APU electrical load 41,000 feet

Question 20

Holding in icing conditions

Answer 20

Holding with flaps extended prohibited

Question 21

Speed brake lever in flight operation

Answer 21

Do not extended with flaps 10 or greater selected

Question 22

RNP AR operations in a MAX

Answer 22

Minima below 0.3 not allowed

Question 23

Max fuel imbalance

Answer 23

Not exceeding 1000 pounds

Question 24

Minimum accumulator brake pressure

Answer 24

1200 psi

Question 25

Engine cool down time

Answer 25

3 minutes or at the gate