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Left Aft Fuselage
Aft outflow valve ........................................................................... Check
Doors and access panels (not in use) ...........................................Latched
Left Main Wheel Well
Wheel well ..................................................................................... Check
Left Main Gear
Tires, brakes and wheels ................................................................ Check
Verify that the wheel chocks are in place as needed.
If the parking brake is set, the brake wear indicator pins must extend
out of the guides.
Gear strut, actuators and doors ...................................................... Check
Hydraulic lines...............................................................................Secure
Gear pins ..................................................................................As needed
787 Flight Crew Operations Manual
Normal Procedures -
Amplified Procedures
NP.21.8 Boeing Proprietary
Left Wing Tip and Trailing Edge
Navigation and strobe lights ..........................................................Check
Static discharge wicks ....................................................................Check
Aileron, flaperon, and trailing edge flaps.......................................Check
Fuel jettison nozzle ........................................................................Check
Fuel tank vent .................................................................................Check
Left Wing and Leading Edge
Wing Surfaces ................................................................................Check
Fuel tank vent .................................................................................Check
Leading edge slats ..........................................................................Check
Access panels .............................................................................. Latched
Left Engine
Exhaust area and tailcone ...............................................................Check
Thrust reverser ............................................................................. Stowed
Probes, sensors, ports, vents, and drains (as applicable) ................Check
Access panels .............................................................................. Latched
Fan blades, probes, and spinner .....................................................Check
Left Wing Root, Pack, and Lower Fuselage
Probes, sensors, ports, vents, and drains (as applicable) ................Check
Exterior lights .................................................................................Check
Pack inlet and pneumatic access doors ......................................... Secure
Negative pressure relief vents ....................................................... Closed
Positive pressure relief valves ....................................................... Closed
Leading edge flaps .........................................................................Check
Forward outflow valve ...................................................................Check
Preflight Procedure – First Officer
787 Flight Crew Operations Manual
Normal Procedures -
Amplified Procedures
Boeing Proprietary NP.21.9
The first officer normally does this procedure. The captain may do this
procedure as needed.
HEADING REFERENCE switch.................................................NORM
PRIMARY FLIGHT COMPUTERS
DISCONNECT switch ........................................................Guard closed
Verify that the DISC light is extinguished.
ELECTRICAL panel ...........................................................................Set
BATTERY switch – ON
Verify that the OFF light is extinguished.
IFE/PASS SEATS power switch – ON
Verify that the OFF light is extinguished.
CABIN/UTILITY power switch – ON
Verify that the OFF light is extinguished.
APU GENERATOR switches – ON
Verify that the OFF lights are extinguished.
ENGINE GENERATOR switches – ON
Verify that the OFF lights are illuminated.
Verify that the DRIVE lights are illuminated.
APU selector (as needed) ............................................. START, then ON
Do not allow the APU selector to spring back to the ON position.
Verify that the FAULT light is extinguished.
L HUD BRIGHTNESS control ........................................................... IN
L WIPER selector ............................................................................. OFF
TOWING POWER switch...................................................Guard closed
Verify that the ON BAT light is extinguished.
FLIGHT DECK DOOR POWER switch ...........................................ON
　
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