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767-200 > Limits > Flashcards

Limits Flashcards

1
Q

What is max operating altitude?

A

43,100 feet

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2
Q

Main deck cargo door max wind for operating?

A

40 knots

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3
Q

Main deck cargo door max wind while in the open position?

A

60 knots

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4
Q

Max runway slope?

A

+/- 2%

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5
Q

Max takeoff and landing altitude?

A

8400 feet pressure altitude

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6
Q

Max takeoff and landing tailwind component?

A

15 knots

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7
Q

Contaminated runway max depth of allowable precipitation?

A

6cm of dry snow, 12mm of standing water, wet snow, slush.

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8
Q

Maximum airspeed?

A

360 knots IAS, 0.86 Mach.

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9
Q

Minimum airspeed clean?

A

Below FL200 VREF 30+80, FL200 and above VREF 30+100

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10
Q

Max Alt for flap extension?

A

20,000 feet

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11
Q

Flap 25 landing should be considered if VREF 30 + increments is in excess of………..?

A

150 knots

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12
Q

Takeoff on……………….. is not to be attempted whatever the reported braking action?

A

Wet ice

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13
Q

The minimum braking action for takeoff and landing is?

A

Poor, medium/poor, medium/poor.

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14
Q

To provide bird strike protection do not exceed…………..below…………..feet.

A

313 knots, 8000 feet.

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15
Q

What are the flight manoeuvring load acceleration limits?

A

Flaps up: +2.5g to -1.0g

Flaps down: +2.0g to 0.0g

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16
Q

Turbulent air penetration speed is …………………….., whichever is lower, and ………………… below 10,000 feet.

A

290 KIAS/0.78 Mach, 250 knots

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17
Q

Is it permissible to operate HF radios during refuelling?

A

No

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18
Q

Is it permissible to start the APU during refuelling operations?

A

No

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19
Q

The maximum allowable in-flight difference between captain and first officer altitude displays for RVSM operations is…………..feet.

A

200

20
Q

Minimum inflight weight is………………..LBS.

A

168,000

21
Q

The maximum payload on the main cargo deck is………..LBS.

A

94,000

22
Q

If one fitting of the barrier net is damaged or has been disengaged, or one webbing strap has been cut the total main deck payload should be reduced to………………LBS.

A

56,400

23
Q

Payload LMCs are restricted to +/- …………LBS, and for fuel +/- ……….LBS.

A

1100, 4400.

24
Q

Max allowable cabin differential is…………… psi.

A

9.10

25
Q

Max operating differential during climb is……………..psi.

A

8.6 +/- 0.10

26
Q

Max differential for takeoff and landing is…………..psi.

A

0.125

27
Q

After takeoff the autopilot must not be engaged below ……….feet AGL.

A

400

28
Q

In an approach using V/S mode, the autopilot must be disengaged at or above…………… feet above runway threshold elevation.

A

300

29
Q

On a single channel ILS approach, disengage the autopilot at not less than……………… feet above runway threshold elevation.

A

180

30
Q

The autopilot must be………………..in severe turbulence.

A

Disengaged

31
Q

The maximum allowable wind speeds for automatic landing are:- Headwind……………knots, Tailwind…………….knots, Crosswind…………knots.

A

25, 15, 25.

32
Q

The maximum and minimum glide slope angles for automatic landing are…………………and………………….respectively.

A

3.1 and 2.5

33
Q

For an automatic landing, at least………… autopilots must be engaged and the autoland status annunciations must show……………….at and below………………feet.

A

Two, land 2 or land 3, 600.

34
Q

APU starter duty cycle?

A

Maximum of 3 consecutive starts or attempts within a 60 minute period.

35
Q

Engine starter duty cycle, normal and extended.

A

Normal, 5 minutes on followed by half a minute off per minute on.
Extended, 2 consecutive 5 minute cycles require a 10 minute cooling period before additional 5 minute cycles.

36
Q

Engine RPM, the maximum N1 for the low pressure compressor rotor is…………….%.
N2 intermediate pressure compressor rotor is…………. %

A
  1. 5

110. 5

37
Q

Max engine EGT for takeoff is………….C for……………minutes.

A

940, 5

38
Q

Engine EGT maximum continuous is…………….C.

A

895

39
Q

Engine EGT max for starting is……….C maximum transient for………….seconds.
And………….C unlimited.

A

870, 40 seconds

750

40
Q

Minimum oil pressure is………..PSI.

A

10

41
Q

Maximum oil temperature for continuous operation is……….C, and for a maximum period of………………minutes is…………..C.

A

160

15, 175

42
Q

Minimum oil quantity for despatch is…………quarts

A

17

43
Q

Maximum fuel temperature is…………….C.

A

49

44
Q

Minimum fuel temperature is ……………….or at least…………above fuel freezing point, whichever is higher.

A

-45C, 3C

45
Q

The maximum fuel weight for the left or right wing tanks is……..LBS. max for centre tank is…………..LBS.

A

43,097, 32,367.

767-200 (3 decks)

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