787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Preface -
Revision Record
Copyright © The Boeing Company. See title page for details.
0.4.12 D615Z003-TBC
6.20.8 - Removed "is a dedicated equipment cooling system" from the PECS
reference. It also cools part of the ICS system.
Electrical Load Management
6.20.9 - No technical change. Grammatical change only.
Modes of Operation
6.20.9 - Corrected "wing and tail position lights" to "navigation lights".
6.20.10 - No technical change. Grammatical change only.
6.20.11 - Removed word "trim" from "stabilizer trim" citation in note under
the "In-Air Rat Only Operation" mode (standby power). Stabilizer is
inoperative, but trim can still be accomplished through elevator.
STABILIZER procedure gives further guidance.
Load Inhibit and Load Shedding
6.20.12 - No technical change. Grammatical change only.
Section 30 - EICAS Messages
Electrical System
6.30.1 - Changed MAIN BATTERY DISCH condition based on procedural
validation.
Chapter 7 - Engines, APU
Section 10 - Controls and Indicators
EICAS Display
7.10.2 - Separated GE and RR into separate items.
In–Flight Start Envelope
7.10.10 - Added "necessary" to sentence for clarity.
Oil Pressure Indications
7.10.16 - Added reference to N2 RPM.
Section 20 - Engine System Description
Overspeed Protection
7.20.7 - Revised description of Redline and Overspeed Protection. Expanded
information and separated into unique paragraphs for each type of protection.
Thrust Ramping
7.20.7 - Added information on thrust ramping.
Thrust Control Malfunction Accommodation
7.20.8 - Added information on Thrust Control Malfunction Accommodation.
February 15, 2010
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