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B767-300F > Limitations > Flashcards

Limitations Flashcards

1
Q

What are the Dimensions:
Wingspan?
Tail Height?
Length?

A

Wingspan: 50.88 m
Tail Height: 15.85 m
Length: 54.94 m

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2
Q

Min Pavement Width

A

44.6 m

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3
Q

Eye Height at Touchdown

A

8.25 m

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4
Q

Max Altitude

A

43,100 ‘

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5
Q

Turbulence Penetration Speed

A

290 KIAS / 0.78 M

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6
Q

Max Runway Slope

A

+/- 2%

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7
Q

Max Take Off and Land Altitude

A

8,400 ‘

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8
Q

Autoland:
Max Headwind
Max Crosswind
Max Tailwind

A

Max Headwind: 25 kts
Max Crosswind: 25 kts
Max Tailwind: 15 kts

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9
Q

Max Take Off and Land Tailwind

A

15 kts

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10
Q

Min autopilot engage height

A

200 ‘ AGL

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11
Q

What is trim is prohibited with autopilot engaged?

A

Aileron trim

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12
Q

Max Altitude for flap extension?

A

20,000 ‘

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13
Q

Min Alt for Speedbrake extension?

A

800 ‘

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14
Q

Speedbrake must not be used with what configuration?

A

Landing flaps 25 or 30

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15
Q

APU Starter Cycle

A

3 x start attempts in 60 mins

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16
Q

APU Bleed Air

A

17,000 ‘

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17
Q

APU Electrical

A

43,100 ‘

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18
Q

When is ENG CONT IGNITION used?

A
  1. Must be selected ON in severe turbulence
  2. Automatic ON when ENG Anti-Ice ON in icing conditions
  3. Flap lever out of the UP position
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19
Q

Engine Starter Duty Cycle?

A

Continuous for 5 mins
Cool for 30 sec per min of operation

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20
Q

Max Fuel Tank Temperature

A

49 °C

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21
Q

Min in flight Fuel Tank Temp (*JET A1)

A

-44 °C
(3 °C above the Fuel Freezing temp for specified fuel)

22
Q

HF Radios

A

Do not use HF radios while refuelling

23
Q

APU use while fuelling

A

Not allowed for start or shutdown

24
Q

WX Radar use on ground

A

Do not use while in hangar, or 50 ft near a fuel spill or fuelling.
Do not use near ground personnel

25
Q

Max Taxi Weight

A

187,333 kgs

26
Q

Max Take Off Weight

A

186,880 kgs

27
Q

Max Landing Weight

A

147,871 kgs

28
Q

Max Zero Fuel Weight

A

140,160 kgs (Tasman 141,656 kgs)

29
Q

What should flight crew NOT blank during take off?

A

ENG Vibratation display

30
Q

Use of Centre Tank Fuel

A

Centre tank may contain up to 10,000 kgs of fuel with less than full main tanks, provided centre tank fuel weight plus actual zero fuel weight does not exceed MZFW and CofG limits observed

31
Q

Fuel Imbalance

A

1,134 kgs (21,772 kgs or less)
linear reduction to 680 kgs (36,197 kgs)

32
Q

Centre Fuel Tank Pumps

A

Intentional Dry run of Centre tank fuel pumps prohibited

33
Q

Time limit for use of TO/GA thrust

A

5 mins

34
Q

Use of Wing Anti-Ice

A

The wing anti-ice system may be used as a de-icer or anti-icer in flight only.
Wing anti-ice must not be used with TAT above 10 °C

35
Q

Icing conditions exist when

A

OAT is 10° C or below during ground operations, takeoff, initial climb or go-around or
TAT is 10° C or below in-flight and
visible moisture (clouds, fog with visibility less than one mile, rain, snow, sleet, ice crystals, and so on) is present or
standing water, ice, or snow is present on the ramps, taxiways or runways.

36
Q

Use of Engine Anti-Ice

A

Engine anti-ice must be ON during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below -40° C SAT.

37
Q

Max Cabin Diff Press

A

8.6 psi

38
Q

Pax Oxy auto deploy

A

14,000 ‘

39
Q

The emergency lighting system is powered by ? and for how many minutes?

A

Remote batteries for 15 mins

40
Q

Flight Deck Temp selectors set temps between

A

18-30 °C

41
Q

In the automatic mode, the outflow valve will close if cabin altitude exceeds?

A

11,000 ‘

42
Q

The CABIN ALT light illuminates if cabin altitude exceeds?

A

10,000’

43
Q

Flap limit speeds:
Flaps 1
Flaps 5
Flaps 15
Flaps 20
Flaps 25
Flaps 30

A

Flaps 1: 250 KIAS
Flaps 5: 230 KIAS
Flaps 15: 210 KIAS
Flaps 20: 210 KIAS
Flaps 25: 180 KIAS
Flaps 30: 170 KIAS

44
Q

RAT provides adequate hydraulic power above what speed

A

130 KIAS

45
Q

Nose wheel steering angle with tiller

A

65°

46
Q

Nose wheel steering angle with rudder

A

7°

47
Q

Max speed with geer extended

A

270 KIAS / 0.82 M

48
Q

Max speed to retract gear

A

270 KIAS

49
Q

Fuel Quantities

A

Tasman:
L or R Main Tank: 19,355 kgs
Centre Tank: 38,517 kgs
Total: 77,227 kgs

General:
L or R Main Tank: 18,267 kgs
Centre Tank: 36,349 kgs
Total: 72,882 kgs

50
Q

Taxi Speeds…
Straight
Lo-Vis/slippery spd
Turn
Turn 90°

A

Straight: 30 kts
Lo-Vis / Slippery: 10 kts
Turn: 15 kts
Turn 90°: 10 kts

B767-300F (2 decks)

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