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Maximum takeoff and landing tailwind component
10 not
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Maximum operating altitude
43,100 ft pressure altitude
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Maximum takeoff and landing altitude for 787-8
14,000 ft pressure altitude
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Maximum takeoff and landing altitude for 787-9
11,000 pressure altitude
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The maximum demonstrated crosswind for takeoff / landing 787-8
for takeoff is 40 knots (gust included)
for landing is 37 knots (gust included).
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The maximum demonstrated crosswind for takeoff / landing 787-9
for takeoff is 33 knots (gust included)
for landing is 40 knots (gust included).
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Severe Turbulent Air below FL 250B
290KIAS
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Severe Turbulent Air above fl250
310 KIAS/.84 Mach (whichever is lower)
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altitude display and field elevation altimeter takeoff the maximum allowable difference between Captain's or First
75 feet
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autopilot must not be engaged below a minimum engage altitude
of 200 feet AGL after takeoff.
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Autoland capability may only be used for operations into runways at or below
8400 feet airport field elevation
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787-8
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below
100 feet AGL
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787-9
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below
135 feet AGL
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With LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees, the autopilot must be disengaged below
100 feet AGL.
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If the glidepath angle for approach is greater than 3.77 degrees, the autopilot must be disengaged no later than
50 feet below DH/MDA.
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Low Visibility (HUD) Maximum wind component speeds when takeoff
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Automatic Landing
Maximum wind component speeds when landing
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Oil temperature must be greater than .....for engine start.
40 C
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Fuel Temperature
Maximum tank fuel temperature at takeoff is
49° C
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Inflight fuel temperature is limited to
65° C
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Tank fuel temperature prior to takeoff must not be less than.?
-29° C
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Autoland capability may be used with flaps
20, 25, or 30, with both engines operative or with one engine inoperative
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CAT II Minima,
RVR 300 DH 100
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CAT IIIA Minima,
RVR 200 DH 50
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Weather report RVR 200 - 100 – 75, at airport approved with CAT IIIB,
What approach you can plan? & what will be the reversion capability?
CAT III B, Reversion to CAT IIIA
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B787 approved for LVTO take RVR not less than:
150m
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LVP standard calls for Alert Height, PM Calls ‘’ ALERT HEIGHT’’ , PF Calls:
CONTINUE
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What PBN approaches we approve to do at WY?
RNAV (GNSS) – RNAV (GPS) – RNP 0.3 WITH LNAV & LNAV/VNAV MINIMA
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For cold weather OAT below charted minima can we do RNAV approach?
YES, RNAV approach with LNAV minima
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Is there any correction on vertical profile & MDA? Where we get the corrections from?
Yes, FCOM SP.16.10
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