Limitations

Question 1

Maximum Takeoff Tailwind Component (AFM) AND

Maximum Landing Tailwind Component (AFM)

Answer 1

15 kts

Question 2

Maximum Operating Altitude (ft)

Answer 2

41,000

Question 3

Maximum Takeoff and Landing Altitude (ft)

Answer 3

8400

Question 4

Minimum Takeoff and Landing Temperature

Answer 4

-54°C

Question 5

Maximum Operating Limit (AFM)

Answer 5

Observe VMO/MMO and Gear/Flap Placards

Question 6

Severe Turbulence Penetration Target Speed

Answer 6

280 KIAS/.76M*

Question 7

AIR CONDITIONING

Answer 7

With either one or both engine BLEED air switches on, do not operate air conditioning packs
in HIGH for takeoff, approach or landing.

NOTE: Non-normal procedures take precedence over the restriction from operating air
conditioning pack in HIGH during takeoff, approach or landing. The CARGO FIRE
and SMOKE/ FUMES REMOVAL checklists require placing the operating pack
switch(es) to HIGH in order to increase ventilation for smoke removal.

Question 8

Engine Anti Ice

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 ___.

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

Answer 8

ON / -40°C SAT.

ON / -40°C SAT.

Question 9

AUTOMATIC FLIGHT

AUTOPILOT

Answer 9

Do not engage the autopilot below 1000 ft AGL on takeoff. (AFM/ASA)

For single channel operation during approach, the autopilot shall not remain engaged below
50 ft AGL. (AFM).

For manually flown HGS AIII approach, the autopilot shall not remain engaged below 500
ft AGL.

Use of aileron trim with autopilot engaged is prohibited. (AFM).
The Autopilot / Flight Director system has been certified for Category II and III Automatic Approach and Landing operations. (AFM)

Question 10

CIRCUIT BREAKERS (ASA)

Answer 10

Do not reset a tripped fuel quantity indication system circuit breaker under any circumstance.

Question 11

ENGINES

Warm-up : Cool-Down

Answer 11

Warm-up :Engines must be operated for a minimum of 3 minutes prior to takeoff. (ASA)

Cool-Down: Engines must be operated at or near idle (taxi thrust acceptable) for a
minimum of 3 minutes prior to shutdown. (ASA)

Question 12

ENGINE EGT (AFM)

Answer 12

Maximum Time Limit for Takeoff Thrust 5 minutes*

10 minutes allowed in the event of the loss of thrust on one engine during.

Question 13

ENGINE IGNITION

ENGINE START switches must be in the CONT position for:

Answer 13

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

Question 14

ENGINE IGNITION (AFM/ASA)ENGINE START switches must be in the FLT position for:

Answer 14

• Operation in severe turbulence

NOTE:
When checklists call for “Start Switches… ON,” use either CONT or FLT as appropriate for the
existing flight operation.

Question 15

Reverse Thrust

Answer 15

Intentional selection of reverse thrust in flight is prohibited

Question 16

APU LOAD - Bleed and Electric

Answer 16

10,000 ft

Question 17

APU LOAD - Bleed Only

Answer 17

17,000 ft

Question 18

APU- Electric Only

Answer 18

41,000 ft

Question 19

APU - MAX operating altitude

Answer 19

41,000 ft

Question 20

APU GENERAL - Ensure ble3ed air switch is closed for _____ minute(s) after start and for ___ minute(s) prior to shutdown

Answer 20

2 / 1

When APU switch is moved to OFF, this time delay is met automatically.
APU bleed valve may be open during engine start, but avoid engine power above idle.
Except for engine start, the APU bleed valve must be closed when another source is pressurizing left bleed air duct

Question 21

Flaps -Max flap extension Altitude

Answer 21

20,000 ft

Question 22

Flaps - Holding in icing conditions with flaps extended is…

Answer 22

PROHIBITED

Question 23

SPEED BRAKES - Do not deploy speed brakes in flight below?

Answer 23

1000 ft.

Question 24

In flight do not extend speed brake lever beyond the ____ Detent

Answer 24

Flight

Question 25

Do NOT deploy speed brakes with more than ____ extended

Answer 25

Flap 10

Question 26

Load Alleviation System (700/900)

Manually overriding the load alleviation system is?

Answer 26

NOT authorized

Question 27

Min fuel tank temp:

Answer 27

• minus 37 degrees

* Unless actual freeze point is known

Question 28

Allowable lateral imbalance between main tank 1 and 2 must be scheduled to ____.
Transient fuel imbalance must not exceed _______ lbs. for taxi, takeoff, flight or landing.

Answer 28

zero / 1000 lbs

Question 29

Center Fuel Tank Pumps
For ground ops- CTFP switches must positioned ___
UNLESS…
__________.

CTFP must not be on unless _______.

Answer 29

ON

CT fuel quantity exceeds 1000 lbs, except when defueling or transferring fuel.
(So if you don’t have 1000 lbs… they should be off…)

personnel are available in the flight deck to monitor LOW PRESSURE lights.

**For ground and flight ops, the corresponding center tank fuel pump switch must be position OFF when the LOW PRESSURE annunciator light illuminates. Of the center tank is empty, position both CTFP switches to OFF.

Question 30

Hydraulics: Ground Ops of electric hydraulic pumps requires minimum of ___ lbs. in respective fuel tank.

Answer 30

1675 lbs.