B767 FM Flashcards

Memory items from the 757 PHB

1
Q

Maximum altitude for flap extension

A

20,000 ft

p37

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2
Q

Minimum engagement altitude for autopilot after takeoff

A

1000 ft AGL

p34

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3
Q

Autopilot minimum altitude coupled ILS without auto land

A

50 ft AGL

p34

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4
Q

Autopilot minimum altitude Non-precision with VNAV

A

50 ft below DA
100 ft below DDA
p34

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5
Q

Autopilot minimum altitude Non-precision with V/S

A

50 ft below DA
100 ft below DDA
p34

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6
Q

757/767 Autoland authorized flap settings

A

flaps 25 or 30

p34

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7
Q

During Performance briefing, the takeoff CG difference of up to ___ % between Wt and Balance and FMS is allowed.

A

1

p112

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8
Q

When is the engine anti-ice required to be on in-flight?

A

Engine anti-ice must be ON during all flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below -40 deg C SAT.
P362

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9
Q

What is the recommended cool down time at idle/taxi thrust after landing?

A

3 minutes

p136

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10
Q

What speed do you use for max rate of climb 757/767?

A

Vref30 + 130 until intercepting .76/.78 respt.

p100,101 FTM

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11
Q

Take-offs are not permitted when slush, standing water, or wet snow is more than ___ inch on the runway.

A

1/2

p28

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12
Q

Take-offs are not permitted when dry snow depth is more than ___ inches.

A

4

p28

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13
Q

Maximum landing weight

A

326.0K

p23

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14
Q

767 Maximum Take-off wt

A

408.0K

p23

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15
Q

767 Flap Limiting Speed - Flap 1

A

250kts

p26

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16
Q

767 Flap Limiting Speed - Flap 5

A

230kts

p26

17
Q

767 Flap Limiting Speed - Flap 15

A

210kts

p26

18
Q

767 Flap Limiting Speed - Flap 20

A

210kts

p26

19
Q

767 Flap Limiting Speed - Flap 25

A

180kts

p26

20
Q

767 Flap Limiting Speed - Flap 30

A

170kts

p26

21
Q

Max 757/767 landing gear operating and extended speeds

A

270kts/.82

p26

22
Q

What are the Engine Anti-ice taxi out procedures for the GE engine?

A

When engine anti-ice is required and the OAT is 3 deg C or below, do and engine run-up. Run-up to a minimum of 60% N1 for approximately 30 seconds at intervals no greater than 30 minutes.
p360

23
Q

What is the engine anti-ice take-off procedure for the GE engine?

A

When engine anti-ice is required and the OAT is 3 deg C or below, take-off must be preceded by a static engine run-up. Run-up to a minimum of 60% N1 for approximately 30 seconds. Confirm stable engine operation before the start of the take-off roll.
p361

24
Q

767 Non-Standard Fuel Load Allowable ZFW

A

The center tank may contain up to 22,050 # of fuel with less than full main tanks provided:
1) Center tank fuel weight plus actual zero fuel weight does not exceed max zero fuel weight.
2) Center of gravity limits are observed.
p40

25
Q

767 Fuel Imbalance between tanks when main tank fuel is less than 48,000 #

A

2500#

p40

26
Q

767 Fuel Imbalance between tanks when main tank fuel is greater than 48,000 #

A

1500#

p40

27
Q

767 max ZFW

A

309.0k p23

28
Q

767 max operating altitude

A

43,100 ft p25

29
Q

Do not use the autopilot below 100 ft radio altitude at airport pressure altitudes above _____ ft.

A

8500 p35

30
Q

What N1 takeoff thrust setting to use before selecting THR (auto throttle)?

A

70%

p. 124

31
Q

What is the minimum runway width for a 180 degree turn?

A

146ft (44.6m)

p. 28

32
Q

Engine warm-up time (GE)

A

GE - 3 minutes

p 122