Boeing 787-8 - Page 39

787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Preface -
Revision Record
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC 0.4.15
Actuator Control Electronics (ACE)/Hydraulic Power Distribution
9.20.4 - Added control and power sources for leading and trailing edge
devices.
Normal Mode
9.20.6 - Added color to graphic.
Flight Control System Secondary Mode
9.20.7 - Added conditions under which the flight control system reverts to
secondary mode.
Secondary Mode
9.20.7 - Added color to graphic.
Direct Mode
9.20.8 - Added color to graphic.
Normal Mode Pitch Control
9.20.9 - Changed "dependant" to "dependent".
Alternate Pitch Trim
9.20.10 - Added sentence - "Alternate pitch trim switches are inhibited when
the autopilot is engaged."
Pitch Envelope Protection
9.20.11 - Added "caution" to sentence.
9.20.11 - Revised cross reference for standardization.
Rudder Trim
9.20.16 - Added "during takeoff roll" to sentence for clarification.
Secondary and Direct Mode Yaw Control
9.20.17 - Removed "/modal" from sentence.
Autodrag
9.20.19 - Added "assist in", "/glidepath" and " the vertical" to sentence for
clarification.
Flap/Slat Load Relief
9.20.21 - Changed "knots" to "KIAS".
Slat Autogap and Slat Pregap
9.20.21 - Changed "knots" to "KIAS" and defined functions for autogap trip
threshold.
9.20.21 - Changed "knots" to "KIAS".
February 15, 2010