Limitations

Question 1

Runway slope

Answer 1

+/- 2%

Question 2

Maximum Takeoff and Landing Tailwing Component

Answer 2

15 kts

Question 3

Maximum Operating Altitude

Answer 3

43,100 feet

Question 4

Maximum Takeoff and Landing Altitude

Answer 4

8,400 ft

Question 5

Maximum DEMONSTRATED Take Off and Landing Crosswind

Answer 5

38kts

Question 6

Severe Turbulent Air Penetration Speed

Answer 6

270 kts below 25,000 ft

280 kts or 0.82 Mach whichever is lower at 25,000 ft or above.

Question 7

HF Radios

Answer 7

Do not operate HF radios during re-fuelling operations

Question 8

Weather Radar

Answer 8

Avoid weather radar operation in a hangar (does not apply to weather radar test mode)

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

Question 9

RVSM Operations

Answer 9

Prior to takeoff the maximum difference between Captain’s or First Officer’s altitude display and field elevation is 75 ft.

Standby altimeter does not meet altimeter accuracy requirements if RVSM airspace.

Question 10

Autopilot / Flight Director System

Answer 10

The autopilot must not be engaged below a minimum engage altitude of 200 feet AGL after take off.

Without LAND 2 or LAND 3 annumciated, the autopilot must be disengaged below 200 feet AGL.

Question 11

PVD Take Off

Answer 11

Maximum crosswind allowed for LVOs where a PVD system is used is 15kts

Question 12

Automatic Landing

Answer 12

When landing weather minima are predicated on autoland operations the following limits apply:

Headwind - 25 kts
Tailwind - 15 kts
Crosswind - 25 kts (15 kts in USA)

Maximum Glideslope angle - 3.25 deg

Minimum Glideslope angle - 2.5 deg

Autothrottle is mandated to conduct a CAT 3B approach.

The AFDS must display LAND 2 or LAND 3 and following must NOT be displayed:

SLATS DRIVE,
SGL SOURCE DISPLAYS
SGL SOURCE RAD ALT
SGL SOURCE ILS.

Question 13

FLCH

Answer 13

DO NOT use FLCH on final approach below 1000 ft AFE

Question 14

Engines Limit Display Markings

Answer 14

Maximum and minimum limits are RED

Caution limits are AMBER

Question 15

Engine Oil System

Answer 15

RR - Oil temperature must be greater than -40 degrees C for engine start and 50 degrees C before advancing thrust levers to take off power.

Question 16

Engine Fuel System

Answer 16

Maximum tank fuel temperature is 49 degrees C

Tank fuel temperature prior to take-off must be not less than :

GE: -40 deg C or 3 deg C above fuel freeze point whichever is higher

RR: -37 deg C or 3 deg C above fuel freeze point whichever is higher

In flight tank fuel temperature must be maintained at least 3 deg C above fuel freeze point of fuel being used.

Main tanks must be scheduled to be full if centre tank fuel is loaded

Centre tank may contain up to 1360 kgs of fuel with less than full main tanks.

Question 17

Reverse Thrust

Answer 17

RR- After an RTO is performed where reversers where deployed, take off is prohibited until maintenance action is complete.

Question 18

APU

Answer 18

APUs starter motors duty cycle (electric starter and air turbine starter) is 3 start attempts in a 60 minute period.

Wait 1 minute between each start.

Question 19

Flaps

Answer 19

Maximum altitude with flaps extended is 20,000 ft