Limitations

Question 1

Maximum Takeoff and Landing Tailwind Component

Answer 1

15 kts

Question 2

Turbulent air penetration speed (in severe turbulence) is defined as:

Answer 2

• 290 KIAS below 25,000 feet
• 310 KIAS/.84 Mach (whichever is lower) at and above 25,000 feet. (Refer to Severe Turbulence in Chapter SP., Section 16, for additional information.)

Question 3

Do not operate HF radios

Answer 3

when refueling

Question 4

Avoid weather radar operation

Answer 4

in a hangar, or within 50 feet (15.25 meters) of fueling operations or a fuel spill.

Avoid weather radar operation when personnel are within the area normally enclosed by the aircraft nose radome.

Question 5

The autopilot must not be engaged

Answer 5

below a minimum engage altitude of 200 feet AGL after takeoff.

Question 6

Autoland capability may only be used

Answer 6

for operations into runways at or below 8400 feet airport field elevation.

Question 7

G-ZBJA - G-ZBJH
# Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged

Answer 7

below 100 feet AGL.

Question 8

G-ZBKA - ZB371
# Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged

Answer 8

below 135 feet AGL.

Question 9

With LAND 2 or LAND 3 annunciated and glidepath angles greater than 3.25 degrees,

Answer 9

the autopilot must be disengaged below 100 feet AGL.

Question 10

Maximum wind component speeds when takeoff weather minima are predicated on HUD takeoff operations:

Answer 10

Headwind…………….25 knots
# Tailwind………………..15 knots
# Crosswind…………….20 knots (USA - 15 knots)

The HUD takeoff system has been demonstrated to perform satisfactorily in non-LVO conditions in the following wind conditions:
• Headwind: 50 knots
• Tailwind: 15 knots
• Crosswind: 36 knots

Question 11

Maximum wind component speeds when landing weather minima are predicated on autoland operations:

Answer 11

# Headwind..............25 knots
# Tailwind..................15 knots
# Crosswind..............25 knots (USA - 15 knots)

The automatic landing system has been demonstrated to perform satisfactorily in non-LVO conditions with all engines and one engine inoperative, with and without autothrottle, in the following wind conditions:
• Headwind: 48 knots
• Tailwind: 15 knots
• Crosswind: 33 knots (28 knots with one engine inoperative)
Rollout performance has been demonstrated on both wet and dry runways. Each autobrake setting has been demonstrated.

Question 12

The maximum glidepath angle for automatic landings is

Answer 12

3.25 degrees

Question 13

The minimum glideslope angle for automatic landings is

Answer 13

2.5 degrees

Question 14

Autoland capability may be used with flaps

Answer 14

20, 25, or 30, with both engines operative or with one engine inoperative.

Question 15

Do not use FLCH on final approach

Answer 15

below 1,000 feet AFE.

Question 16

Engine Oil System
# Oil temperature must be greater than ??? for engine start.

Answer 16

-40° C

Question 17

Intentional selection of reverse thrust in flight is ???

Backing the airplane with use of reverse thrust is ???

Answer 17

Prohibited.

Question 18

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

Answer 18

structural failure at any speed, including below VA.

Question 19

Do not extend flaps above

Answer 19

20,000 feet.

Question 20

Minimum taxiway width in normal operation ???

This taxiway width guidance is specific to British Airways operation and has been developed following correspondence with Boeing.

Answer 20

20m.

Taxi with extreme caution when taxiway width is less than 23m. Use of taxiways less than 20m wide is only permitted with fleet approval and guidance to avoid departing the paved surface

Question 21

If glidepath angle greater than 3.77 degrees the autopilot must be disengaged by?

Answer 21

50 feet below MDA / DH

L 10.4

Question 22

A) Maximum tank fuel temperature at takeoff is ????

B) Inflight fuel temp is limited to ????

C) Tank fuel temp prior to takeoff must be no less than ????

D) In-flight fuel temp must be maintained at least ????

Answer 22

A) 49 degrees C for jet A/ A-1, JP-5, JP8 or TS-1

B) 65 degrees C (except TS-1)

C) -29 degrees C

D) -42 degrees C, as well as 3 degrees above fuel freezing point of the fuel being used.