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Message Level Aural Condition
HYD OVERHEAT
C1, C2
Advisory Center pump temperature is high.
HYD OVERHEAT
DEM L, R
Advisory Demand pump temperature is high.
HYD OVERHEAT
PRI L, R
Advisory Center pump output pressure is low when
commanded on.
HYD PRESS C1,
C2
Advisory Pump output pressure is low.
HYD PRESS DEM
L, R
Advisory Demand pump output pressure is low when
commanded on.
HYD PRESS PRI
L, R
Advisory Primary pump output pressure is low.
HYD PRESS SYS
C
Caution Beeper Center hydraulic system pressure is low.
HYD PRESS SYS
L
Caution Beeper Left hydraulic system pressure is low.
HYD PRESS SYS
L+C
Caution Beeper Left and center hydraulic system pressures
are low.
HYD PRESS SYS
L+C+R
Caution Beeper All hydraulic system pressures are low.
HYD PRESS SYS
L+R
Caution Beeper Left and right hydraulic system pressures
are low.
HYD PRESS SYS
R
Caution Beeper Right hydraulic system pressure is low.
HYD PRESS SYS
R+C
Caution Beeper Right and center hydraulic system pressures
are low.
HYD QTY LOW
C, L, R
Advisory Hydraulic quantity is low.
RAT UNLOCKED Advisory Ram air turbine is not stowed and locked.
787 Flight Crew Operations Manual
Hydraulics -
EICAS Messages
13.30.2 Boeing Proprietary
Intentionally
Blank
787 Flight Crew Operations Manual
Landing Gear Chapter 14
Table of Contents Section 0
Boeing Proprietary 14.TOC.0.1
1C4o.0n Ltarnodilnsg aGneadr- TIanbdlei ocfa Ctoonrtesn ts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
14.10.1
Landing Gear Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.10.1
Nose Wheel Steering Tiller . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.10.2
Brake System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.10.3
Rudder/Brake Pedals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.10.3
Parking Brake Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.10.3
Landing Gear System Indications . . . . . . . . . . . . . . . . . . . . . . . 14.10.4
Landing Gear Position Indications . . . . . . . . . . . . . . . . . . . . 14.10.4
Gear Synoptic Display . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.10.5
System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.1
Air/Ground Sensing System . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.1
Landing Gear Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.1
Landing Gear Retraction . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.1
Landing Gear Extension . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.1
Landing Gear Alternate Extension . . . . . . . . . . . . . . . . . . . . 14.20.2
Nose Wheel Steering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.2
Brake System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.3
Electric Brake System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.3
Antiskid Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.3
Autobrake System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.3
Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.5
Brake Temperature Indication . . . . . . . . . . . . . . . . . . . . . . . 14.20.5
Tire Pressure Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.20.5
EICAS Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.30.1
Landing Gear EICAS Messages . . . . . . . . . . . . . . . . . . . . . . . . 14.30.1
Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.30.1
Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14.30.1
787 Flight Crew Operations Manual
14.TOC.0.2 Boeing Proprietary
Landing Gear -
Table of Contents
Intentionally
Blank
787 Flight Crew Operations Manual
Landing Gear Chapter 14
Controls and Indicators Section 10
Boeing Proprietary 14.10.1
14.10 Landing Gear-Controls and Indicators Landing Gear Panel
UP – the landing gear retracts.
DN – the landing gear extends.
OFF – deactivates and resets the autobrake system.
DISARM –
• disengages the autobrake system
• releases brake pressure.
1, 2, 3, 4, MAX AUTO – selects the desired deceleration rate.
　
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本文鏈接地址：787機組操作手冊Flight Crew Operations Manual 3(105)