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AJX: AW > AW: B767 Limitations > Flashcards

AW: B767 Limitations Flashcards

1
Q

Engines

A

2 x GE CF6-80C2B6F

F means FADEC

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2
Q

Wingspan

A
  1. 57m without Winglets

50. 88m with Winglets

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3
Q

Length

A

54.94m

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4
Q

Height

A

15.85m

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5
Q

Min required pavement width for 180* turn

A

46.3m

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6
Q

Max deflection of nose wheel

Tiller and Pedal Steering

A

65* and 7*

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7
Q

MTW: -300ER (Class 1)

A

401,000 LBS

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8
Q

MTW: -300ER (Class 2)

A

347,000 LBS

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9
Q

MTW: -300ER (Class 3)

A

290,700 LBS

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10
Q

MTOW: -300ER (Class 1)

A

400,000 LBS

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11
Q

MTOW: -300ER (Class 2)

A

345,000 LBS

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12
Q

MTOW: -300ER (Class 3)

A

288,700 LBS

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13
Q

MLW: -300ER (Class 1)

A

326,000 LBS

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14
Q

MLW: -300ER (Class 2)

A

320,000 LBS

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15
Q

MLW: -300ER (Class 3)

A

288,700 LBS

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16
Q

MZFW: -300ER (w/o winglets)

A

288,000 LBS

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17
Q

MZFW: -300ER (with winglets)

A

291,300 LBS

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18
Q

Flap Speeds (VFE); -300ER/F

1, 5, 15, 20, 25, 30

A 
Flap 1 - 250 KIAS
Flap 5 - 230 KIAS
Flap 15 - 210 KIAS
FLAP 20 - 210 KIAS
FLAP 25 - 180 KIAS
FLAP 30 - 170 KIAS
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19
Q

Gear Retraction

A

270 KIAS

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20
Q

Gear Extension

A

270 KIAS / 0.82M

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21
Q

Alternate Gear Extension

A

250 KIAS / 0.75M

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22
Q

Max Gear Extended (VLE)

A

270 KIAS / 0.82M

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23
Q

Max tailwind component for take-off and landing

A

RWY 2001m or ABOVE - 15kts

RWY 2000m or BELOW - 10kts

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24
Q

Runway Slope Limit

A

+/- 2%

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25
Q

Max operating altitude

A

43,100ft

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26
Q

Max Take-off and Landing Altitude

A

8,400ft

27
Q

Max cabin differential pressure

A

9.1psi

28
Q

Auto regulated differential

A

8.6psi

29
Q

Max allowable differential pressure for take-off and landing

A

0.125psi

30
Q

Min altitude to engage CMD or CWS on take-off

A

200ft

31
Q

When must the autopilot be turned off?

A

On approach leaving the DA or MDA

32
Q

Max wind component for auto land?

Headwind
Tailwind
Crosswind

A

Headwind - 25kts
Tailwind - 15kts (10kts)
Crosswind - 25kts

33
Q

Max N1 RPM

A

117.5%

34
Q

Max N2 RPM

A

112.5%

35
Q

Max EGT, take-off (5 mins)

A

960*c

36
Q

Max EGT, Continuous

A

925*c

37
Q

Max EGT, Starting

A

750c (870c for 40 seconds)

38
Q

Flaps, Max operating altitude

A

20,000ft

39
Q

When can you not operate the weather radar?

A

In a hangar; within 50ft of personnel; or a fuel spill

40
Q

IRS, Max alignment

A

78.2* North and South

41
Q

IRS, Valid heading information

A

73* North and 60* South

42
Q

IRS, Max Navigation, Guidance and MAP

A

87* North and South

43
Q

Max allowable fuel weight

Left Main Tank
Right Main Tank
Centre Tank
Total

A

Left Main Tank - 42,671 LBS
Right Main Tank - 42,671 LBS
Centre Tank - 84,490 LBS
Total - 169,832 LBS

44
Q

Max fuel allowable imbalance

A

1,500 LBS imbalance @ 79,800 LBS or MORE Fuel Load

2,000 LBS imbalance @ 61,000 LBS Fuel Load

2,500 LBS imbalance @ 48,000 LBS or LESS Fuel Load

45
Q

Do not reset which circuit breakers?

A

a FUEL PUMP or FUEL PUMP CONTROL circuit breaker

46
Q

Prohibited Fuels

A

JET B and JP4

47
Q

Approved Fuels

A

JET A, JET A1, JP5 and JP8

48
Q

Max fuel tank temperature

A

+49*c

49
Q

Minimum fuel tank temperature

A

+3*c

Fuel Freezing Point

50
Q

Fuel freezing points: JET A, JET A1, JP5 and JP8

A

JET A: -40c
JET A1: -47c
JP5: -46c
JP8: -47c

51
Q

Maximum break away thrust on ground

A

40% N1

52
Q

Maximum Crosswind

DRY (including DAMP)
WET (Grooved)
WET (Un-grooved)
FLOODED

A

DRY (including DAMP): 33
WET (Grooved): 25
WET (Un-grooved): 20
FLOODED: 10

53
Q

Maximum Crosswind

Braking Action (Ice or Snow)

A 
Good: 20
Medium to Good: 20 (15)
Medium: 20 (15)
Poor to Medium: 15 (10)
Poor: 10
54
Q

Maximum Crosswind

SLUSH/Depth

A

2mm or less: 15

3mm - 12mm: 10

55
Q

Application of crosswind gusts: If wind exceeds ‘x’ from the average, then..

Formula

A

10kts

Steady + (Max Wind - Steady)/2; OR

(Max Wind + Steady)/2

56
Q

Hydroplanning, 3 types are…

A

Dynamic
Viscous
Rubber Reversion

57
Q

Dynamic Hydroplanning

A

Tyre is lifted off the runway by water

Completely Supported by water

Occurs at a speed determined by: VP (KTS) = 9 * Square Root of the tyre pressure (psi)

58
Q

Viscous Hydroplanning

A

Tyre cannot penetrate thin film of fluid

Normally in zones of rubber deposits (TDZ)

Proceeds dynamic hydroplanning

This is the reason for a firm touchdown when film of water is present in the TDZ

59
Q

Rubber Reversion

A

Friction between tyres and surface generate heat

Heat combined with standing water produces steam

Steam lifts the tyre off the surface and on water

Proceeds dynamic hydroplanning

60
Q

Maximum airspeed and descent rates

Below 5000’
Between 2000-1000’
Below 1000’

A

Below 5000’: MAX V/S -2500fpm and 300KIAS

Between 2000-1000’: MAX V/S -1500fpm

Below 1000’: MAX V/S -1000fpm

61
Q

Turbulence penetration speed

A

290KIAS/0.78M

62
Q

PAX: Minimum O2 for dispatch (inc URUMQI)

A

850psi

Urumqi: 1250psi

63
Q

Freighter: Minimum O2 for dispatch

Non-ETOPS
2 Crew
1 Jumpseat
2 Jumpseat

A

Non-ETOPS: 850psi

2 Crew: 850psi

1 Jumpseat: 1250psi

2 Jumpseat: 1500psi

AJX: AW (22 decks)

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