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Max operating altitude
43,100 ft. pressure altitude
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Max T/O & Ldg altitude
8,400 ft. pressure altitude
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Max T/O & Ldg tailwind
15 knots
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Max Demonstrated crosswind TO and LDG
29 knots
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Turbulent air penetration speed
290 KIAS/.78 Mach
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Flap Extension Maximum altitude
20,000
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FUEL USAGE I (No Center Tank Fuel)
Use tank-to engine fuel for takeoff and landing with all operable main tank fuel pumps on and crossfeed valve(s) closed. Open crossfeed valve(s) for minimum fuel operations or to correct/prevent fuel imbalance.
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FUEL USAGE II (Fuel In Center Tank)
Use the center tank fuel for all operations with all operable boost pumps ON and crossfeed valve(s) closed until the center tank is depleted, then use FUEL USAGE I. Open crossfeed valve(s) for minimum fuel operations or to correct/prevent fuel imbalance.
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Intentional dry running of a _______ is prohibited.
center tank fuel pump (CTR L FUEL PUMP or CTR R FUEL PUMP message displayed on EICAS)
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If a center tank fuel pump fails with ample fuel in the center tank, accomplish the __________
- FUEL PUMP Non-Normal Procedure
- Note: B767 aircraft with center tank fuel pumps deactivated (inop): No fuel may be in the center tank for dispatch except that which drains from the fuel line manifold into the center tank following each fueling operation. (See Chap. 4, Sec. 2; Fuel System Operations)
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When fueling, load _____ equally within balance limits. If _______ are full and more fuel is required, load the __________.
- main tanks
- main tanks
- center tank (if activated)
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Center tank fuel (applicable only to aircraft with activated center tank fuel system): Maximum of _______ pounds of fuel may be loaded in the center tank with less than full wing tanks, provided __________________.
- 22,050
- the weight of the fuel in the center tank plus actual Zero Fuel Weight does not exceed Maximum Zero Fuel Weight, and balance limits are observed. Fuel must be used in accordance with FUEL USAGE II.
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On takeoff, do not engage CMD mode below _________.
400 feet AGL
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Starter Operation: B767 GE CF6
Engine Normal Duty Cycle:____________
Extended Duty Cycle:________________
- Normal: Five (5) minutes ON, followed by one and one half (1½) minutes OFF
- Extended:
- 1) Five (5) minutes ON, followed by one and one half (1½) minutes OFF.
- 2) Two (2) consecutive five (5) minute cycles require a ten (10) minute cooling period before additional five (5) minute cycles.
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Starter Re-engagement
- 0% N2 Recommended starter Re-engagement.
- 0-20% N2 Permissible starter Re-engagement.
- 21-30% N2 Permissible for purging or to clear a fire. Re-engagement above 30% N2 may result in starter or gearbox damage.
- Note: A logbook entry is required whenever the starter is reengaged above 20% N2.
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Continuous ignition shall be on for ____________
flight in severe turbulence
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Reverse thrust is for ______ only. Intentional election of reverse thrust ______ is prohibited.
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On the ground, _______ the airplane with use of ________ is prohibited.
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When is engine anti-ice required on ground and take off?
- 10° C OAT or below
- Visible moisture:
- precipitation, visibility < 1 mile, RVR <5000 Temp/Dewpoint spread < 3° C.
- Runway and/or taxiway is contaminated with standing water, slush, or snow.
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When is engine anti-ice required for climb and cruise?
- From 10° C TAT to -40° C SAT
- Visible moisture present or anticipated.
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When is engine anti-ice required for descent?
- Less than 10° C TAT including SAT less than -40°C
- Visible moisture present or anticipated.
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When is wing anti ice required on descent?
- At or below 22,000 ft
- less than 10° C TAT including SAT less than -40°C
- Visible Moisture.
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Flap placard speeds VFE (B-767-200):
- 1 = 240
- 5 = 220
- 15 = 210
- 20 = 195
- 25 = 190
- 30 = 162
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Flap placard speeds VFE (B-767-300):
- 1 = 250
- 5 = 230
- 15 = 210
- 20 = 210
- 25 = 180
- 30 = 170
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Maximum winds for autoland:
- Headwind 25 kts
- Crosswind 25 kts
- Tailwind 15 kts.
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Use of ______ with autopilot engaged is prohibited.
aileron trim
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Autoland not authorized when aircraft weight exceeds _______________.
max landing weight
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APU starter duty cycle is ___________
3 start attempts (maximum) followed by 60 minutes to let the temperature of the starter decrease.
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Landing Gear placard speeds (normal):
- Retract VLO = 270
- Extend VLO = 270 MLO = .82
- Extended VLE = 270 MLE = .82
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Landing gear extended with alternate system
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Max engine oil temp (GE CF6)
Continuous: _______
Temp: _____ for _____ min
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Min engine oil pressure (GE CF6):
10 psi
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Min engine oil quantity for dispatch (GE CF6)
17 quarts
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Maximum wind for main cargo door operation ______.
Maximum wind with main cargo door open (static) _______.
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The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation is ______
200 feet
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The maximum allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM operation are:
- Field Elevation///Max Diff between Capt & F/O///Max Diff between Capt or F/O & Field Elevation
- Sea Level /// 40 feet /// 75 feet
- 5,000 feet /// 45 feet /// 75 feet
- 10,000 feet /// 50 feet /// 75 feet
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Maximum allowable fuel imbalance between the left and right main tanks for all operations:
- Fuel Imbalance (pounds) ///// Main Tank Fuel Load (pounds)
- 2,500 /// 48,000 or less
- Linear reduction to 1,500 //// 48,000 to 79,800
- 1,500 /// Greater than 79,800
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Maximum tank fuel temperature
49°C
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Minimum fuel tank temperatures:
3°C above the freezing point of the fuel being use
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