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Maximum taxi weight
171,500
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Maximum takeoff weight
171,000
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Maximum landing weight
134,000
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Maximum zero fuel weight
126,000
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Minimum takeoff weight (27K)
130,000
Lower minimum takeoff weights that account for the actual pressure altitude and outside air temperature may be obtained by using the Minimum Takeoff Weight table in the Takeoff section of the Performance Dispatch (PD) chapter.
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Minimum takeoff weight (26K)
125,000
Lower minimum takeoff weights that account for the actual pressure altitude and outside air temperature may be obtained by using the Minimum Takeoff Weight table in the Takeoff section of the Performance Dispatch (PD) chapter.
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Maximum takeoff and landing tailwind
15 KNOTS
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Maximum operating altitude
41,000 ft
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Maximum takeoff and landing altitude
13, 500 ft
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Maximum fuel temperature
49°C
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Minimum inflight tank fuel temperature
-43 OR 3C abv frz pt
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Random fuel imbalance must not exceed ____ for _____, _____, _____, _________
1000lbs for taxi, takeoff, flight or landing
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Minimum runway length
5000 ft
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Minimum runway width
98ft
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Minimum taxiway width
49 ft
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Minimum width for 180 degree turn
75 ft
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Maximum wind any direction
50 knots
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Engine TAI must be on when icing conditions _____ or _____, except during _____ and ______ below ______SAT
exist or are anticipated, except during climb and cruise below -40 SAT
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Icing conditions exist when _____ is _____ and:_____is present_____ is present on the ramps, taxiways or runways
Icing conditions exist when TAT is 10°C and: Visible moisture is present standing water, ice or snow is present on the ramps, taxiways or runways
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CAUTION: Do not operate ____ or _____ when the total total air temperature (TAT) is above _____
CAUTION: Do not operate ENGINE or WING ANTI-ICE when the total total air temperature (TAT) is above 10°C
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CAUTION: Use of wing anti-ice above approximately _____may cause _____ and possible loss of _____
CAUTION: Use of wing anti-ice above approximately FL350 may cause bleed trip off and possible loss of cabin pressure
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Engine Ignition must be on for:
1. Takeoff
2. Landing
3. Operation in heavy rain
4. Operation of anti-ice
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Use of ____ with the autopilot engaged is prohibited
Use of aileron trim with the autopilot engaged is prohibited
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Do not engage the autopilot for takeoff below _____
Do not engage the autopilot for takeoff below 400 ft AGL
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For single channel operation during approach, the autopilot shall not remain engaged below _____
For single channel operation during approach, the autopilot shall not remain engaged below 50 ft AGL
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Maximum allowable wind speeds when landing weather minima are predicated on autoland operations:
Headwind
Crosswind
Tailwind
Maximum allowable wind speeds when landing weather minima are predicated on autoland operations:
Headwind 25
Crosswind 20
Tailwind 15
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Abort: Above 80 knots and prior to V1, the takeoff should be rejected for:
1. Fire or Fire Warning
2. Engine Failure
3. Predictive windshear warning
4. If the airplane is unsafe or unable to fly
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At first indication of stall buffet or stick shaker
1. Hold: Control Column Firmly
2. Disconnect: Autopilot and auto throttle
3. Smoothly: Apply nose down elevator
4. Roll: In the shortest direction to wings level
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Ground Proximity Warning
1. Disconnect autopilot
2. Disconnect autothrottle
3. Aggressively apply maximum thrust
4. Simultaneously roll wings level and rotate to an initial pitch attitude of 20 degrees
5. Retract speedbrakes
6. If terrain remains still remains a threat rotate to PLI or stick shaker
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Windshear Escape Maneuver (Manual Flight)
1. Disconnect autopilot
2. Press TO/GA
3. Aggressively apply maximum thrust
4. Disconnect autothrottle
5. Simultaneously roll wings level and rotate to an initial pitch attitude of 15 degrees
6. Retract speed brakes
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Severe Turbulence Air Penetration Speed
280/.76, whichever is lower.
Applicable to climb and descent only. During cruise, refer to SP 1.7.
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The maximum allowable in-flight difference between Captain and FO for RVSM:
200 feet.
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The maximum allowable on the ground altitude display differences for RVSM are:
Max difference between Capt. and FO
Field elevation 5000 and below: 50 feet
Field elevation 5001-10000: 60 feet
Max difference between Capt. and/or FO and Field Elevation: 75 feet.
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Maximum cabin differential
9.1 psi.
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Do not use LVL CHG on final approach below ____.
1000 feet AFE.
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APU bleed max altitude
17,000 ft.
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APU electrical load max altitude
41,000 ft.
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APU bleed and electrical load max altitude
10,000 ft.
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Max altitude with flaps extended
20,000 ft.
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Main tanks 1 and 2 must be full if center tank exceeds ____
1000 lbs.
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Takeoff crosswind limits-DRY
33 knots
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Takeoff crosswind limits-Wet
25 knots
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The autopilot must be engaged when the RNP specified for the approach is less than ___.
0.3
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Landing crosswind limits-DRY
33 knots
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Landing crosswind limits-WET
33 knots
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Landing crosswind limits-CAT II/III Manual Land
10 knots
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Minimum length for touch and go landings
6000 feet
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Touch and go crosswind limits
Dry
Wet
Dry: 25 knots
Wet: 20 knots
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Do not use Assumed Temperature for reduced thrust on _____.
Contaminated runways.
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Max runway depth for dry snow
4 inches
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Max runway depth for slush, standing water, or wet snow
.5 inches
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Initial speed for emergency descent
(Not a limitation)
Target speed for emergency descent
(Not a limitation)
Initial speed: .80/270 maximum
Target speed .76/300
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