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Max operating altitude
43,100 ft
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Max T/O and Landing Altitude
8400 ft
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Max T/O and Landing tailwind
15 kts
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Turbulent air penetration speed
290 kts /.78 M
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Nav display system does not support ops at latitudes greater than:
87 N or S
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RVSM altimeter cross check limits
in flight
200 ft max between capt and FO altimeters
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RVSM altimeter cross check limits
on ground
- Btw Capt/FO
- Sea Lvl 40 ft
- 5,000 ft 45 ft
- 10,000 ft 50 ft
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Main Cargo Door
Max wind gust with door open
60 kts
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Main Cargo Door
Max wind for operating
40 kts
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Supernumery and Crew Evacuation
Must be available for use, at least _______________
one operable inertial reel and one operable escape harness for each occupant
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Weather Radar
Don't operate radar in a ________ or within _______
hanger
50 ft of any personnel or fuel spill
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Flight Deck Security Door
Verify that an operational check of the Flight Deck Access System has been accomplished ___________
once each flight day
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Auto Flight
After T/O, autopilot must not be engaged below _______
200 ft AGL
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Auto Flight
Use of __________ with the autopilot engaged is prohibited.
aileron trim
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Auto Flight
Max allowable wind speeds for landing when landing weather minima are predicated on autoland operations
- Headwind 25 kts
- Crosswind 25 kts
- Tailwind 15 kts
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Engine
Continuous ignition ________ and in the _____ mode while operating in severe turbulence
ON (eng start selector in the CONT position)
Note: Cont ignition is automatically provided in icing conditions when engine anti-ice is on
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Engine
Flight crew shall not ________ display during takeoff
blank engine vibration
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Engine Fuel System
Min inflight fuel tank temp
3 C (5 F) above the freeze point of the fuel being used.
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Engine Fuel System
Max fuel temp
- 49 C (120 F)
- Note: Jet B/JP-4 prohibited for 767
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Engine Fuel System
Center tank may contain up to _________ of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the max zero fuel weight (266,000 lbs) and CG limits are observed.
22,050 lbs
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Reverse Thrust is for _______ only
ground
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Flight Controls
Max altitude for flap extension
20,000 ft
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Flight Controls
Do not extend speedbrakes below ________
800 ft AGL
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Navigation
Do not operate under IFR or at night into airports north of _____, or south of ________whose nav aids are referenced to _________
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Navigation
If an approach is predicated on the use of DME data associated with an ILS or Localizer, __________
correct tuning of the DME's must be verified by aural station ident or DME data cross comparison between left and right DME's prior to executing the approach
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GPWS
Do not use the terrain display for ______
navigation
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GPWS
The use of look-ahead terrain alerting and terain display functions is prohibited within _______
15 nm of T/O, app or landing at an airport not contained in the GPWS terrain database.
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Normal starter duty cycle
- 5 on
- 30 sec off for each minute on
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Starter extended duty cycle
2 consecutive starts require 10 min cooling before additional 5 min cycle
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APU starter duty cycle limit
3 consecutive starts or attempts within a 60 min period
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