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speed (amber band) when below 0.82 Mach.
The maximum demonstrated takeoff and landing crosswind is (TBD) knots.
Do not operate weather radar or the HF radio in a hanger or within 50 feet of any
personnel or a fuel spill.
RVSM Operations
Non-AFM Operational Information
Prior to takeoff the maximum allowable difference between Captain’s or First
Officer’s altitude display and field elevation is 75 feet.
The standby altimeter (TBD) altimeter accuracy requirements of RVSM airspace.
# Runway slope +/- 2%
# Maximum Operating Altitude 43,100 feet pressure altitude
# Maximum Takeoff and Landing Altitude (TBD) feet pressure altitude
# Maximum Takeoff and Landing Tailwind
Component
15 knots
787 Flight Crew Operations Manual
Limitations -
Operating Limitations
L.10.2 Boeing Proprietary
Weight Limitations
Door Mounted Power Assists and Escape Slides
# Main door emergency power assists and evacuation slide systems must be armed
with the mode select handle in the ARMED position prior to taxi, takeoff and
landing whenever passengers are carried.
Flight Deck Security Door
Verify that an operational check of the Flight Deck Access System has been
accomplished according to approved procedures once each flight day.
Lower Crew Rest Compartment
# The lower crew rest compartment may not be occupied, and the main entry hatch
must be closed during taxi, takeoff, or landing.
Air Systems
Cabin Pressurization
Autoflight
Autopilot/Flight Director System
# Do not use the autopilot below 100 feet RA at airport pressure altitudes above
8,400 feet.
# The autopilot must not be engaged below a minimum engage altitude of 200 feet
AGL after takeoff.
# The autopilot must be disengaged before the airplane descends more than 50 feet
below the MDA unless it is coupled to an ILS glideslope and localizer or in the
go–around mode.
Weights Pounds
# Maximum Taxi Weight 482,000
# Maximum Takeoff Weight 480,000
# Maximum Landing Weight 465,000
# Maximum Zero Fuel Weight 440,000
Maximum differential pressure (relief valves) (TBD) psi
Maximum allowable cabin pressure differential for takeoff and
landing
(TBD) psi
787 Flight Crew Operations Manual
Limitations -
Operating Limitations
Boeing Proprietary L.10.3
# Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged
below 200 feet AGL.
Automatic Landing
# When landing weather minima are predicated on autoland operations the
following limits apply:
# The maximum glideslope angle is 3.25 degrees.
# The minimum glideslope angle is 2.5 degrees.
# Automatic landings can be made using flaps 20 or 30, with both engines
operative or one engine inoperative. The autopilot flight director system (AFDS)
autoland status annunciation must display LAND 2 or LAND 3.
Communications
Flight Deck Communications Systems (Datalink)
The datalink from the COMPANY format is limited to the transmission and
receipt of messages, which will not create an unsafe condition if the message is
improperly received, such as the following conditions:
• the message or parts of the message are delayed or not received,
• the message is delivered to the wrong recipient, or
• the message content may be frequently corrupted.
However, Pre-Departure Clearance, Digital Automatic Terminal Information
Service, Oceanic Clearances, Weight & Balance, and Takeoff Data messages can
be transmitted and received via the COMPANY format if they are verified per
approved operational procedures.
Engines
Engine Limit Display Markings
Maximum and minimum limits are red.
Caution limits are amber.
Engine Oil System
Oil temperature must be greater than -(TBD) degrees C for engine start and TBD
degrees C before advancing thrust levers to takeoff power.
Headwind 25 knots
Tailwind 15 knots
Crosswind 25 knots
787 Flight Crew Operations Manual
Limitations -
Operating Limitations
L.10.4 Boeing Proprietary
Engine Fuel System
# The use of JP–4 and Jet B fuels is prohibited.
# The maximum tank fuel temperature is 49 degrees C.
# Tank fuel temperature prior to takeoff must not be less than -40 degrees C or 3
degrees C above the fuel freezing point, whichever is higher. In-flight tank fuel
temperature must be maintained at least 3 degrees C above the freezing point of
the fuel being used. The use of Fuel System Icing Inhibitor additives does not
change the minimum fuel tank temperature limit.
Reverse Thrust
# Intentional selection of reverse thrust in flight is prohibited.
　
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