Limitations

Question 1

Runway slope

Answer 1

+/- 2%

Question 2

Munimum Runwat width (company limit)

Answer 2

30m

Question 3

Minimum Taxiway width (company)

Answer 3

15m

Question 4

Maximum tailwind component

Answer 4

15kt /10kt

Question 5

Maximum Operating Altitude

Answer 5

41000ft

Question 6

Maximum takeoff and landingaltitude

Answer 6

8400ft

Question 7

Maximum flight latitude

Answer 7

82N - 82S
Between 80W and 130W : 70N
Between 120E and 160E : 60S

Question 8

HF radios

Answer 8

Do not operate during refuelling operations

Question 9

Minimum width for 180° Turn

Answer 9

24.1m

Question 10

Fight Manoeuvring loads

Answer 10

Flaps Up: 2.5G to -1.0G
Flaps down 2.0G to 0.0G

Question 11

Maximum Wind for ground ops and LVO

Answer 11

Max for ground ops : 60kts
Max tailwind: 15kt / 10kt
Max headwind for autoland : 25kts
Max crosswind for autoland : 20kts

Question 12

Recommended max crosswind

Answer 12

Dry RWY : 34kts
Wet RWY: 25kts TO / 34kts Landing
BA GOOD: 25kts TO / 34kts Landing
BA MEDIUM : 20kts
BA POOR: 5kts

The landing numbers may be used for TO if:
- flaps 5 or greater
- CG no more than 25%MAC
- Runway Width 45m or more

Question 13

Assumed Temperature

Answer 13

• only allowed on DRY or WET runways
• NOT allowed with Antiskid INOP

Question 14

Crosswind limit correction for reduced runway width

Answer 14

0.5kts per m, to a maximum of 30m width

Question 15

Fuel tank temperatures

Answer 15

Maximum 49°C
Minimum -43°C or 3°C above freezing point, whichever is higher

Question 16

Lateral fuel imbalance

Answer 16

Scheduled to be zero
453kg max for taxi, takeoff and landing

Question 17

Fuel capacity

Answer 17

Each wing tank - 3915kg
Centre tank - 13066kg

Wings must be full if centre tank contains more than 453kg

Question 18

Engine ignition (start switches)

Answer 18

Must be on (CONT) for:
- takeoff
- landing
- operation in heavy rain
- anti ice operation

Question 19

Reversers

Answer 19

Intentional selection in flight is prohibited

Question 20

APU operation

Answer 20

Bleed + Electrical load - 10000ft
Bleed - 17000ft
Electrical load - 41000ft

Question 21

APU starter

Answer 21

3 consecutive start attempts followed by a 15 minute cooling period

Question 22

Cabin differential pressure

Answer 22

Maximum 9.1 psi

Question 23

Packs in High

Answer 23

Do not operate for Takeoff, Approach or Landing when one or both engine bleed switches are ON

Question 24

QFE Operations

Answer 24

Prohibited

Question 25

WX radar

Answer 25

Do not operate in a hangar Do not operate within 50ft of fuelling operations or fuel spills

Question 26

Landing gear

Answer 26

Do not apply brakes until after touchdown

Question 27

Autopilot and Flight director system

Answer 27

1. Use of aileron trim with A/P engaged is prohibited 2. Do not engage the A/P for takeoff below 400ft 3. Minimum use height for single channel is 158ft 4. Maximum and minimum glideslope angles 2.5° and 3.25° 5. Autoland capability is only with flaps 30/40 and both engines operative

Question 28

Level Change

Answer 28

Do not use below 1000ft AFE

Question 29

Maximum flap extension altitude

Answer 29

20000ft

Question 30

Flap limit speed

Answer 30

1 - 250kts 5 - 250kts 10 - 210kts 15 - 200kts 25 - 190kts 30 - 175kts 40 - 162kts

Question 31

Alternate flap duty cycle

Answer 31

Allow 15 seconds after releasing switch before moving switch again After a complete extend/retract cycle, allow 15min cooling

Question 32

Speedbtakes

Answer 32

1. Do not extend beyond FLIGHT DETENT in flight 2. Do not use speed brakes below RA 1000ft 3. Do not use speedbrakes with flaps in transit 4. Use of speedbrakes with flap 15 should be avoided

Question 33

Max allowable inflight difference between CAPT and FO altimeters

Answer 33

200ft

Question 34

Max allpwable difference on ground between CAPT and FO altimeter

Answer 34

50ft between Capt and Fo 75 between field elevation and Capt or Fo

Question 35

Guarding of flight controls

Answer 35

PF shall always be able to take controls if autopilot disengages Below 5000ft both pilots must guard the rudder pedals, and the PF must guard the contol column.