Limitations

Question 1

Runway slope

Answer 1

+/- 2%

Question 2

Maximum Takeoff and Landing Tailwind
Component

Answer 2

Tailwind 15 knots #
Takeoff 15 knots #

Question 3

Maximum Operating Altitude

Answer 3

41,000ft pressure altitude

Question 4

Maximum Takeoff and Landing Altitude

Answer 4

8,400ft pressure altitude

Question 5

Severe Turbulent Air Penetration speed

Answer 5

280 KIAS / .76M, whichever is lower

Question 6

HF Radio during refueling

Answer 6

Do not operate #

Question 7

Altimeter tolerance
1) Max Difference Between
Captain & F/O

2) Max Difference Between
Captain or F/O & Field
Elevation

Answer 7

1) 50ft

2) 75ft

Question 8

Maximum Taxi Weight

Maximum Takeoff Weight

Answer 8

Taxi - 70,760 Kilograms

Takeoff - 70,533 Kilograms

Question 9

Maximum Landing Weight

Answer 9

65,317 Kilograms

Question 10

Max Zero Fuel

Answer 10

61,688 Kilograms

Question 11

Maximum Cabin Diff

Answer 11

9.1 psi

Question 12

With either one or both engine bleed air switches ON….takeoff, approach or landing.

Answer 12

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

Question 13

After any ground deicing/anti-icing of the horizontal stabilizer using Type II or
Type IV fluids,

Answer 13

After any ground deicing/anti-icing of the horizontal stabilizer using Type II or
Type IV fluids, airspeed must be limited to 270 KIAS until the crew has been
informed that applicable maintenance procedures have been accomplished that
would allow exceedance of 270 KIAS

Question 14

Aileron trim with the autopilot engaged

Answer 14

Use of aileron trim with the autopilot engaged is prohibited.#

Question 15

Do not engage the autopilot for takeoff below

Answer 15

Do not engage the autopilot for takeoff below 400 feet AGL #

Question 16

Autoland maximum wind

Answer 16

• Headwind 25 knots
• Crosswind 20 knots
• Tailwind 15 knots.

Question 17

Autoland max and min glideslope

Answer 17

3.25 max and 2.5 min #

Question 18

Autoland flaps and engine req

Answer 18

Autoland capability may only be used with flaps 30 or 40 and both engines
operative. #

Question 19

Autoland landing alt

Answer 19

Autoland capability may only be used to runways at or below 8,400 ft pressure
altitude.

Question 20

LVL CHG on final approach

Answer 20

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

Question 21

Engine Limit Display Markings

Answer 21

Maximum and minimum limits are red.
Caution limits are amber.

Question 22

Engine ignition must be on for:

Answer 22

• takeoff
• landing
• operation in heavy rain
• anti-ice operation.

Question 23

Anti-skid inoperative take off

Answer 23

Operation with assumed temperature reduced takeoff thrust is not permitted with
anti-skid inoperative.

Question 24

Reverse Thrust

Answer 24

Intentional selection of reverse thrust in flight is prohibited.

Question 25

APU bleed + electrical load - max alt

Answer 25

APU bleed + electrical load: max alt 10,000 ft. #

Question 26

# APU bleed: max alt Airplanes operating under FAA Rules: Ground only - APU bleed + electrical load: max alt ? # APU bleed: max alt ? # APU electrical load: max alt ?

Answer 26

# APU bleed: max alt 17,000 ft. Airplanes operating under FAA Rules: Ground only - APU bleed + electrical load: max alt 15,000 ft. # APU bleed: max alt 17,000 ft. # APU electrical load: max alt 41,000 ft.

Question 27

APU bleed valve must be closed when:

Answer 27

* ground air connected and isolation valve open * engine no. 1 bleed valve open * isolation and engine no. 2 bleed valves open.

Question 28

The maximum altitude with flaps extended is

Answer 28

The maximum altitude with flaps extended is 20,000 ft. #

Question 29

Holding in icing conditions with flaps extended is

Answer 29

Holding in icing conditions with flaps extended is prohibited.#

Question 30

Avoid ___ and ___ alternating control inputs, especially in combination with large changes in __, __, or __ (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.

Answer 30

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.#

Question 31

Do not deploy the speedbrakes in flight at radio altitudes less than

Answer 31

Do not deploy the speedbrakes in flight at radio altitudes less than 1,000 feet. #

Question 32

Maximum tank fuel temperature

Answer 32

Maximum tank fuel temperature is 49°C.

Question 33

Minimum tank fuel temperature prior to takeoff and inflight is –

Answer 33

Minimum tank fuel temperature prior to takeoff and inflight is –43°C, or 3°C above the fuel freezing point temperature, whichever is higher.

Question 34

Lateral imbalance between main tanks 1 and 2 must be scheduled to be ___. Random fuel imbalance must not exceed ______ for taxi, takeoff, flight or landing.

Answer 34

Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero. Random fuel imbalance must not exceed 1000 lbs / 453 kgs for taxi, takeoff, flight or landing.

Question 35

Main tanks 1 and 2 must be full if center tank contains more than ____

Answer 35

Main tanks 1 and 2 must be full if center tank contains more than 1000 lbs / 453 kgs.