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Slide/Raft Deployed
TO INFLATE
FOR DITCHING
USE ONLY
LIFT PULL FLAP HANDLE
Door Frame
Raft Deploy Controls and Instructions
For ditching use only
Lift flap - Pull handle
Manual Inflation Handle
Used to manually inflate the
not inflate automatically
slide/raft if the slide/raft does
TYPICAL
INTERIOR
VIEW
787 Flight Crew Operations Manual
Airplane General, Emergency
Equipment, Doors, Windows -
Systems Description
1.40.16 Boeing Proprietary
Evacuation Slide/Rafts
Cargo Doors
There are three cargo doors; one forward, one aft, and one bulk. The forward and
aft cargo doors are located on the right side of the airplane while the bulk cargo
door is on the left side. The cargo doors all open upward. The forward and aft
cargo doors open outward and the bulk cargo door opens inward.
PRELIMINARY
787 Flight Crew Operations Manual
Airplane General, Emergency
Equipment, Doors, Windows -
Systems Description
Boeing Proprietary 1.40.17
Both forward and aft cargo doors are normally operated electrically from an
exterior or interior fuselage mounted control panel located with each door. A
control panel light indicates cargo door latching. Forward and aft cargo door
locking is accomplished manually. If necessary, the forward and aft cargo doors
may be operated manually.
The bulk cargo door is manually opened and closed, and is counterbalanced for
ease of operation.
Flight Deck Seats
The flight deck has three seat types:
• pilot seats (captain and first officer)
• first observer seat
• second observer seat.
787 Flight Crew Operations Manual
Airplane General, Emergency
Equipment, Doors, Windows -
Systems Description
1.40.18 Boeing Proprietary
Pilot Seats
Lumbar Control
In/Out
Control
Manual Horizontal
Vertical Power
Horizontal and
Controls
Harness Reel
Lock Control
Power Cutoff
Switch
Adjustable Headrest
Captain’s Seat - Inboard Side View
Seat Pan Tilt
Control
Harness
PRELIMINARY
787 Flight Crew Operations Manual
Airplane General, Emergency
Equipment, Doors, Windows -
Systems Description
Boeing Proprietary 1.40.19
The pilot seats:
• recline
• adjust vertically
• adjust forward and aft
• adjust for thigh support
• adjust for lumbar support
• adjust for seat pan tilt angle.
WARNING: Seat pan tilt must be rotated fully forward except
during cruise.
The seats also have:
• adjustable armrests
• crotch straps
• inertial–reel shoulder harnesses with manual locks
Recline Control
Lumbar Control
Up/Down
Manual Vertical
Control
Thigh Support
Control
Captain’s Seat - Outboard Side View
Armrest Adjustment
Control
Horizontal
Power Control
2 Life Vest
Stowage
PRELIMINARY
787 Flight Crew Operations Manual
Airplane General, Emergency
Equipment, Doors, Windows -
Systems Description
1.40.20 Boeing Proprietary
• lap belts
• adjustable headrests.
The seats move outboard during the last two inches of aft travel. Electric and
manual controls provide forward, aft, and vertical adjustment. A guarded
secondary fore/aft power control is provided in the upper seat back near the
headrest for easier seat access. Manual levers provide other adjustments.
Lumbar and thigh pad support can be adjusted using the manual control wheels.
Armrest pitch can be adjusted using the control knob under the armrest. The
armrests can be stowed vertically for easier seat access. The headrest can be
adjusted vertically by pulling up or pushing down. The headrest angle can be
adjusted by moving the cushion to the right and rotating it.
Adjust the seat to obtain the optimum eye position as shown on the following
illustration.
Pilot Seat Adjustment
1. Adjust the seat to the
upright position; sitting up
straight, looking straight
ahead.
3. Adjust the seat until:
• the top of the glareshield
appears as the edge of a plane,
and
• the crosshairs on the top of
the rudder pedal adjustment
crank housing line up with the
top of the control column.
4. The control column must be
in the neutral position.
2. The seat pan tilt must be
rotated fully forward.
787 Flight Crew Operations Manual
Airplane General, Emergency
Equipment, Doors, Windows -
Systems Description
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本文链接地址：
787机组操作手册Flight Crew Operations Manual 1(113)
