Limitations

Question 1

Maximum Takeoff Tailwind Component (AFM)

Answer 1

15 kts

Question 2

Maximum Landing Tailwind Component (AFM)

Answer 2

15 kts

Question 3

Maximum Operating Altitude (ft)

Answer 3

41,000

Question 4

Maximum Takeoff and Landing Altitude (ft)

Answer 4

8,400

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 Target Speed

Answer 7

280 kts/.76M (whichever is lower)

Question 8

With either one or both engine BLEED air switches ON, do not operate air condition in HIGH for ______.

Answer 8

Takeoff, approach, or landing

Question 9

The engine anti-ice system must be ON during all ground and flight operations when icing conditions exist or are anticipated, except ___.
Engine anti-ice must be ON prior to and during descent _______.

Answer 9

Except during climb and cruise below -40C SAT.

In all icing conditions, including temperatures below -40C SAT

Question 10

(MAX) Engine anti-ice must be turned ______ when not in actual or anticipated icing conditions

Answer 10

OFF

Question 11

Do not engage autopilot below _______ on takeoff

Answer 11

1,000 ft AGL (AFM/ASA)

Question 12

For single channel operation during approach, the autopilot shall not remain engaged below _______.

Answer 12

50 ft AGL (AFM)

Question 13

For manually flown HGS AIII approach, the autopilot shall not remain engaged below ______

Answer 13

500 ft AGL

Question 14

Use of aileron trim with autopilot engaged is ________

Answer 14

Prohibited (AFM)

Question 15

Warm-up:
Engines must be operated for a minimum of _______ prior to takeoff.

Answer 15

3 minutes (ASA)

Question 16

Cool-down:
Engines must be operated at or near idle (taxi thrust acceptable) for a minimum of ________ prior to shutdown.

Answer 16

3 minutes (ASA)

Question 17

Maximum Time Limit for Takeoff Thrust

Answer 17

5 Minutes
(10 minutes allowed in the event of the loss of thrust on one engine during takeoff)

Question 18

ENGINE START switches must be in the CONT position for:

Answer 18

Takeoff
Landing
Anti-ice operation
Operation in hail, sleet or moderate to heavy rain

Question 19

ENGINE START switches must be in the FLT position for:

Answer 19

Operation in severe turbulence

Question 20

Minimum Oil Temperature before setting takeoff thrust

Answer 20

31C (MAX)

Question 21

Intentional selection of reverse thrust in flight is

Answer 21

Prohibited

Question 22

APU LOAD
Bleed and Electric Load

Answer 22

10,000 ft

Question 23

APU LOAD
Bleed Only

Answer 23

17,000 ft

Question 24

APU LOAD
Electric Only

Answer 24

41,000 ft

Question 25

APU LOAD Maximum Operating Altitude

Answer 25

41,000 ft

Question 26

Ensure APU BLEED air switch is closed for _______ after start and for ______ prior to shutdown

Answer 26

2 minutes 1 minute NOTE: When the APU switch is moved to OFF, the time delay is met automatically.

Question 27

Maximum Flap Extension Altitude

Answer 27

20,000 ft (AFM)

Question 28

Holding in icing conditions with flaps extended is

Answer 28

Prohibited (AFM)

Question 29

Do no deploy speed brakes in flight below

Answer 29

1,000 ft AGL

Question 30

In flight, do not extend the SPEED BRAKE lever beyond

Answer 30

the FLIGHT DETENT (AFM)

Question 31

Do no deploy speed brakes with more than

Answer 31

Flaps 10 Extended (Although not prohibited, the use of speed brakes with Flaps 1-10 extended should be avoided as much as possible. The use of speed brakes with flaps extended increases loads on the trailing edge flaps, resulting in increased wear and tear)

Question 32

Manually overriding the Load Alleviation System is

Answer 32

Not authorized

Question 33

Minimum fuel temperature

Answer 33

-37c unless actual fuel freeze point is known.

Question 34

Allowable lateral imbalance between main tanks 1 and 2 must be scheduled to be ______. Fuel imbalance must not exceed ________ for _____, _____, ______ or _______

Answer 34

Zero 1,000 lbs Taxi, takeoff, flight or landing

Question 35

Main Wing Tanks must be scheduled to be ______ if the Center Tank contains more than ______

Answer 35

Full 1,000 lbs

Question 36

For ground operations, Center Tank FUEL PUMP switches must not be positioned to ON unless ____, except when defueling or transferring fuel. Center Tank Fuel Pumps must not be on unless ____.

Answer 36

Center Tank fuel quantity exceeds 1,000 lbs Personnel are available in the flight deck to monitor LOW PRESSURE lights.

Question 37

Center Tank Fuel Pumps must not be ______ unless personnel are available in the ________ to monitor __________

Answer 37

ON Flight Deck FLOW PRESSURE lights

Question 38

For ground and flight operations, the corresponding Center Tank Fuel Pump switch must be positioned OFF when _____. If the Center Tank is empty, position both Center Tank FUEL PUMP switches to ___.

Answer 38

The LOW PRESSURE light illuminates OFF

Question 39

Ground operation of electric hydraulic pump requires minimum _________ in the respective fuel tank.

Answer 39

1,675 lbs

Question 40

Except for engine start, the APU bleed valve must be closed when another source is pressurizing ____.

Answer 40

Left blead air duct

Question 41

The APU bleed valve may be open during engine start, but avoid engine power _____.

Answer 41

Above idle