曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
asymmetric thrust conditions.
[From FLIGHT CONTROL MODE checklist.]
Continued on next page
[]LNAV BANK ANGLE LIM
[]NAV AIR DATA SYS
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 11.5
11.5
Continued from previous page
Note: Use flaps 20 and VREF20 for landing.
[From FLIGHT CONTROL MODE checklist. Ensures sufficient pitch
control for landing.]
Note: Avoid speedbrake use in flight.
Note: Do not arm speedbrake lever.
[From AUTO SPEEDBRAKE checklist. Prevents inadvertent inflight
extension.]
Note: Manually extend speedbrakes after landing.
[From AUTO SPEEDBRAKE checklist.]
Do not accomplish the following checklists:
AUTO SPEEDBRAKE
FLIGHT CONTROL MODE
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
11.6
11.6
Condition: Backup source for airspeed is being used instead of
air data.
Avoid abrupt control inputs.
[From FLIGHT CONTROL MODE checklist. Airplane response is changed
by simplified elevator feel and rudder ratio systems.]
Note: Airspeed is calculated using angle of attack. Airspeed
errors of up to 15 KIAS may exist at approach speeds.
GND PROX FLAP OVRD . . . . . . . . . . . . . . . . . . . . . . . . . OVRD
[From FLIGHT CONTROL MODE checklist.]
Note: Inoperative items:
• envelope protection functions
• autopilot
• flight directors
• autothrottles
• PFD flap maneuvering speeds; refer to Flap
Maneuvering Speed table in Performance-Inflight
chapter.
[Inoperative items envelope protection functions and autopilot from
FLIGHT CONTROL MODE checklist.]
Note: Yaw damper is degraded.
[From FLIGHT CONTROL MODE checklist.]
Note: Manual control inputs are required to compensate for
asymmetric thrust conditions.
[From FLIGHT CONTROL MODE checklist.]
Note: Use flaps 20 and VREF20 for landing.
[From FLIGHT CONTROL MODE checklist. Ensures sufficient pitch
control for landing.]
Note: Avoid speedbrake use inflight.
Note: Do not arm speedbrake lever.
[From AUTO SPEEDBRAKE checklist. Prevents inadvertent inflight
extension.]
Note: Manually extend speedbrakes after landing.
[From AUTO SPEEDBRAKE checklist.]
Continued on next page
[]NAV AIRSPEED DATA
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 11.7
11.7
Continued from previous page
Do not accomplish the following checklist:
AUTO SPEEDBRAKE
FLIGHT CONTROL MODE
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
11.8
11.8
Condition: IRS is not capable of providing valid attitude,
position, track and groundspeed.
GPS continues to provide position and track information.
ND map display orientation changes from heading up to
track up.
[ND Map Heading-Up.]
TRANSPONDER ALTITUDE SOURCE selector . . . . . . . .ALTN
TRANSPONDER selector . . . . . . . . . . . . . . . . . . . . . . . .RIGHT
Note: Inoperative items:
• FMC VNAV pages
• FMC performance predictions
• PFD flap maneuvering speeds; refer to Flap
Maneuvering Speed table in Performance-Inflight
chapter
• ND wind direction/speed and wind arrow
• autobrake.
Note: Inoperative AFDS modes:
• LNAV
• VNAV
• TO/GA
• LOC
• GS
• FPA
• TRK HOLD/SEL.
Note: Crosscheck heading periodically for drift with the
magnetic compass. If magnetic compass information
is unreliable or unavailable, track information may be
used.
Note: VOR course deviation is available in the ND VOR
mode. ILS localizer and glideslope deviation raw data
is available on both the PFD and ND.
Continued on next page
[]NAV INERTIAL SYS
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 11.9
11.9
Continued from previous page
Note: If GPS is unavailable, the following additional items
are inoperative:
• ND map mode
• active leg course and distance
• direct to waypoint function
• alternate page DIVERT NOW function
• navigation radio autotuning.
Condition: Navigation performance does not meet required
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
787QRH快速检查单(48)
