Memory Items and Limitations

Question 1

Max Takeoff Tailwind Component (AFM)

Answer 1

15 kts

Question 2

Max Landing Tailwind Component (AFM)

Answer 2

15 kts

Question 3

Maximum Operating Altitude (ft)

Answer 3

41,000

Question 4

Max Takeoff and Landing Altitude (ft)

Answer 4

8400

Question 5

Minimum Takeoff and Landing Temperature

Answer 5

minus 54°C

Question 6

Severe Turbulence Penetration Target Speed

Answer 6

280 KIAS/.76M*

*Whichever is lower

Question 7

Air Conditioning
(High Flow Limit)

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.

Question 8

Autopilot Minimum Engagement Height on Takeoff

Answer 8

1000 ft AGL (AFM/ASA)

Question 9

Minimum Autopilot Height During Approach with Single Channel

Answer 9

50 ft AGL. (AFM)

Question 10

Minimum Autopilot Height for Manually flown HGS AIII Approach

Answer 10

500 ft AGL

Question 11

Use of aileron trim with autopilot engaged is…

Answer 11

Use of aileron trim with autopilot engaged is prohibited. (AFM)

Question 12

Minimum Engine Warm-up time prior to Takeoff

Answer 12

3 minutes (ASA)

Question 13

Minimum Engine Cool-down prior to shutdown

Answer 13

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

Question 14

Maximum Time Limit for Takeoff Thrust

Answer 14

5 minutes*

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

Question 15

ENGINE START switches must be in the CONT position for:

Answer 15

-Takeoff
-Landing
-Anti-ice operation
-Operation in hail, sleet or moderate to heavy rain
ENGINE START switches must be in the FLT position for:
-Operation in severe turbulence

Question 16

Minimum Oil Temperature before setting takeoff thrust

Answer 16

31°C (Max Only)

Question 17

Reverse Thrust (AFM)

Answer 17

Intentional selection of reverse thrust in flight is prohibited.

Question 18

Max Altitude for APU Bleed and Electric Load

Answer 18

10,000 ft

Question 19

Max Altitude for APU Bleed Only

Answer 19

17,000 ft

Question 20

Max Altitude for APU Electric Only

Answer 20

41,000 ft

Question 21

APU Maximum Operating Altitude

Answer 21

41,000 ft

Question 22

APU BLEED air switch Limitations

Answer 22

-Switch must be closed for 2 minutes after start and for 1 minute prior to shutdown (OFF is met automatically)
-Switch may be open for engine start, but avoid power above idle
-Except for starting the APU bleed valve must be closed when another source is pressuring the left bleed duct.

Question 23

Maximum flap extension altitude

Answer 23

20,000 ft. (AFM)

Question 24

Holding in icing conditions…

Answer 24

Holding in icing conditions with flaps extended is prohibited. (AFM)

Question 25

Minimum Height for speed brake usage

Answer 25

1000 ft AGL

Question 26

Max SPEED BRAKE extension in flight

Answer 26

In flight, do not extend the SPEED BRAKE lever beyond the FLIGHT DETENT. (AFM)

Question 27

Max flap setting with speed brakes

Answer 27

Do not deploy speed brakes with more than 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 28

Load Alleviation System (700W/900ER)

Answer 28

Manually overriding the Load Alleviation System is not authorized.

Question 29

Minimum fuel temperature

Answer 29

-37°C unless actual fuel freeze point is known.

Question 30

Max Fuel Imbalance

Answer 30

Allowable lateral imbalance between Main Tanks 1 and 2 must be scheduled to be zero. Transient fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing. Main Wing Tanks must be scheduled to be full if the center tank contains more than 1000 lbs.

Question 31

Center Tank Fuel Pumps (AFM/ASA)

Answer 31

-For ground operation, Center Tank FUEL PUMP switches must not be ON unless Center Tank quantity exceeds 1000 lbs, except when defueling or transferring fuel. -Center Tank Fuel Pumps must not be on unless Flight Deck is attended to monitor LOW PRESSURE lights. -For ground and flight operations, the corresponding Center Tank Fuel Pump switch must be positioned OFF when the LOW PRESSURE light illuminates. If the Center Tank is empty, position both Center Tank FUEL PUMP switches to OFF.

Question 32

Minimum fuel level for ground operation of electric hydraulic pumps

Answer 32

Ground operation of electric hydraulic pump requires minimum 1675 lbs in respective fuel tank.

Question 33

Smoke, Fire or Fumes in Passenger Cabin or Flight Deck

Answer 33

1 Oxygen Masks & Regulators (if required)…………………..On, 100% 2 Smoke Goggles (If required)…… ….………………………………ON

Question 34

Runaway Stabilizer

Answer 34

1 Control Column…………Hold firmly 2 Autopilot (if engaged)……Disengage 3 Autothrottle (if engaged)…Disengage 4 Control Column and Thrust Levers…. ……Control aircraft pitch attitude and airspeed 5 Main Electric Stabilizer Trim…Reduce control column forces 6 If the runaway stops after autopilot is disengaged: Do not re-engage autopilot or autothrottle. [] [] [] [] 7 If the runaway continues after the autopilot is disengaged: STAB TRIM cutout switches (both)……CUTOUT If the runaway continues: Stabilizer Trim Wheel……. Grasp & Hold

Question 35

CABIN ALTITUDE WARNING or Rapid Depressurization

Answer 35

1 Oxygen Masks & Regulators………. ……ON, 100% 2 Crew Communications….Establish

Question 36

Airspeed Unreliable

Answer 36

1 Autopilot (if engaged)……. Disengage 2 Autothrottle (if engaged)…Disengage 3 F/D Switches (both)…………..OFF 4 Set the following gear up pitch attitude and thrust: Flaps Extended…..10° and 80%N1 Flaps Up………………4° and 75%N1