B767 FM Flashcards

Memory items from the 757 PHB (32 cards)

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

17
Q

767 Flap Limiting Speed - Flap 15

18
Q

767 Flap Limiting Speed - Flap 20

19
Q

767 Flap Limiting Speed - Flap 25

20
Q

767 Flap Limiting Speed - Flap 30

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
767 Fuel Imbalance between tanks when main tank fuel is less than 48,000 #
2500# | p40
26
767 Fuel Imbalance between tanks when main tank fuel is greater than 48,000 #
1500# | p40
27
767 max ZFW
309.0k p23
28
767 max operating altitude
43,100 ft p25
29
Do not use the autopilot below 100 ft radio altitude at airport pressure altitudes above _____ ft.
8500 p35
30
What N1 takeoff thrust setting to use before selecting THR (auto throttle)?
70% | p. 124
31
What is the minimum runway width for a 180 degree turn?
146ft (44.6m) | p. 28
32
Engine warm-up time (GE)
GE - 3 minutes | p 122