B767 FM Flashcards
Memory items from the 757 PHB
Maximum altitude for flap extension
20,000 ft
p37
Minimum engagement altitude for autopilot after takeoff
1000 ft AGL
p34
Autopilot minimum altitude coupled ILS without auto land
50 ft AGL
p34
Autopilot minimum altitude Non-precision with VNAV
50 ft below DA
100 ft below DDA
p34
Autopilot minimum altitude Non-precision with V/S
50 ft below DA
100 ft below DDA
p34
757/767 Autoland authorized flap settings
flaps 25 or 30
p34
During Performance briefing, the takeoff CG difference of up to ___ % between Wt and Balance and FMS is allowed.
1
p112
When is the engine anti-ice required to be on in-flight?
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
What is the recommended cool down time at idle/taxi thrust after landing?
3 minutes
p136
What speed do you use for max rate of climb 757/767?
Vref30 + 130 until intercepting .76/.78 respt.
p100,101 FTM
Take-offs are not permitted when slush, standing water, or wet snow is more than ___ inch on the runway.
1/2
p28
Take-offs are not permitted when dry snow depth is more than ___ inches.
4
p28
Maximum landing weight
326.0K
p23
767 Maximum Take-off wt
408.0K
p23
767 Flap Limiting Speed - Flap 1
250kts
p26
767 Flap Limiting Speed - Flap 5
230kts
p26
767 Flap Limiting Speed - Flap 15
210kts
p26
767 Flap Limiting Speed - Flap 20
210kts
p26
767 Flap Limiting Speed - Flap 25
180kts
p26
767 Flap Limiting Speed - Flap 30
170kts
p26
Max 757/767 landing gear operating and extended speeds
270kts/.82
p26
What are the Engine Anti-ice taxi out procedures for the GE engine?
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
What is the engine anti-ice take-off procedure for the GE engine?
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
767 Non-Standard Fuel Load Allowable ZFW
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
767 Fuel Imbalance between tanks when main tank fuel is less than 48,000 #
2500#
p40
767 Fuel Imbalance between tanks when main tank fuel is greater than 48,000 #
1500#
p40
767 max ZFW
309.0k p23
767 max operating altitude
43,100 ft p25
Do not use the autopilot below 100 ft radio altitude at airport pressure altitudes above _____ ft.
8500 p35
What N1 takeoff thrust setting to use before selecting THR (auto throttle)?
70%
p. 124
What is the minimum runway width for a 180 degree turn?
146ft (44.6m)
p. 28
Engine warm-up time (GE)
GE - 3 minutes
p 122