Limitations and General info

Question 1

Max T/O tailwind component

Answer 1

15 kts

Question 2

Max LDG tailwind component

Answer 2

15 kts

Question 3

Max operating altitude

Answer 3

41,000 ft

Question 4

Max takeoff and landing altitude

Answer 4

8,400 ft

Question 5

Max takeoff and landing temp

Answer 5

• 54 C

Question 6

Max operating limit

Answer 6

Observe VMO/MMO and Gear/Flap Placards

Question 7

Severe Turbulence Penetration Target Speed

Answer 7

280 KIAS/.76M*

Question 8

With either one or both engine BLEED air switches ON…

Answer 8

.. do not operate air conditioning
packs in HIGH for takeoff, approach or landing.

Question 9

The engine anti-ice system must be_____ during all ground and flight operations when icing
conditions exist or are anticipated, except during climb and cruise below _____.

Answer 9

ON,- 40°C SAT

Question 10

Engine anti-ice must be____ prior to and during descent in all icing conditions, including
temperatures below _____.

Answer 10

ON,-40°C SAT

Question 11

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

Answer 11

OFF

Question 12

Do not engage the autopilot below ______ on takeoff.

Answer 12

1000 ft AGL

Question 13

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

Answer 13

50 ft AGL.

Question 14

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

Answer 14

500 ft AGL

Question 15

Use of aileron trim with autopilot engaged is ______.

Answer 15

prohibited

Question 16

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

Answer 16

3 minutes prior to takeoff

Question 17

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

Answer 17

3 minutes prior to shutdown.

Question 18

Maximum Time Limit for Takeoff Thrust

Answer 18

5 minutes or 10 minutes allowed in the event of the loss of thrust on one engine during takeoff

Question 19

ENGINE START switches must be in the CONT position for:

Answer 19

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

Question 20

ENGINE START switches must be in the FLT position for:

Answer 20

• Operation in severe turbulence

Question 21

Minimum Oil Temperature before setting takeoff thrust

Answer 21

NG: N/A
MAX: 31 C

Question 22

Intentional selection of reverse thrust in flight is _______.

Answer 22

prohibited

Question 23

Max APU bleed and electrical supply

Answer 23

10,000 ft

Question 24

Max APU bleed only

Answer 24

17,000 ft

Question 25

Max APU electrical supply only

Answer 25

41,000 ft

Question 26

Max APU operating altitude

Answer 26

41,000 ft

Question 27

Ensure APU BLEED air switch is closed for ____ minutes after start and for _____ minute prior to shutdown.

Answer 27

2, 1

Question 28

When the APU switch is moved to OFF...

Answer 28

the time delay is met automatically.

Question 29

APU bleed valve may be open during engine start, but...

Answer 29

avoid engine power above idle.

Question 30

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

Answer 30

Closed, the left bleed air duct.

Question 31

Max flap extension altitude

Answer 31

20,000 ft

Question 32

Holding in icing conditions with flaps extended is________.

Answer 32

prohibited

Question 33

Do not deploy speed brakes in flight below

Answer 33

1000 ft AGL

Question 34

In flight, do not extend the SPEED BRAKE lever beyond the

Answer 34

FLIGHT DETENT

Question 35

Do not deploy speed brakes with more than Flaps...

Answer 35

10

Question 36

Manually overriding the Load Alleviation System is...

Answer 36

not authorized.

Question 37

Min fuel temp

Answer 37

- 37 C,unless actual fuel freeze point is known

Question 38

Allowable lateral imbalance between Main Tanks 1 and 2 must be scheduled to....

Answer 38

0

Question 39

Fuel imbalance must not exceed...

Answer 39

1000 lbs for taxi, takeoff, flight, or landing.

Question 40

Main Wing Tanks must be scheduled to be full if....

Answer 40

the Center Tank contains more than 1000 lbs

Question 41

Maximum fuel temperature:

Answer 41

49°C

Question 42

What engine does the NG use?

Answer 42

CFM56-7

Question 43

What engine does the max use?

Answer 43

CFM LEAP-1B

Question 44

For ground operation, Center Tank FUEL PUMP switches must not be positioned to ______ unless the Center Tank fuel quantity exceeds ______ , except when________.

Answer 44

ON, 1000 lbs, defueling or transferring fuel.

Question 45

Center Tank Fuel Pumps must not be on unless personnel are available in the Flight Deck to monitor....

Answer 45

LOW PRESSURE lights

Question 46

For ground and flight operations, the corresponding Center Tank Fuel Pump switch must be ______ when the LOW PRESSURE light illuminates.

Answer 46

positioned OFF

Question 47

If the Center Tank is empty, position both Center Tank FUEL PUMP switches to _______.

Answer 47

OFF

Question 48

If the Center Tank contains less than 1000 lbs, leave the pumps ______ until in flight and established in a level attitude.

Answer 48

OFF

Question 49

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

Answer 49

1675 lbs