曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專(zhuān)營(yíng)店坑蒙拐騙欺詐消費(fèi)者

Baro Altitude
Odometer
Outline
Deviation
altitude alert
1 second delay,
then blinks as
long as alert is
active.
1 second delay,
then color
changes to amber.
Minimums
Baro bug,
readout and
legend
Baro altitude
descends
below Baro
mins (M)DA.
Blinks for 3
seconds, then
steady.
Color changes to
amber and blinks
for 3 seconds,
then steady.
Minimums
Radio readout
and legend
Radio altitude
descends
through
selected DH.
Blinks for 3
seconds then
steady.
Color changes to
amber and blinks
for 3 seconds,
then steady.
MAG/TRU
Annunciation
highlight box
TRU and a
certain
altitude
descent rate is
achieved.
Blinks for 10
seconds then
steady.
Blinks for 10
seconds, then
steady.
Airspeed Feature
Symbol PFD Full
Symbology
HUD
Decluttered
Symbology
HUD
787 Flight Crew Operations Manual
Flight Instruments, Displays -
Head-Up Display System
Description
Boeing Proprietary 10.22.15
Localizer
Deviation
scale and
pointer
Localizer
deviation
warning or
localizer not
captured
warning or
ground
excessive
deviation
Pointer blinks as
long as warning is
active.
Scale changes
color to amber,
pointer blinks.
Glideslope
Deviation
scale and
pointer
Glideslope
deviation
warning.
Pointer blinks as
long as warning is
active.
Scale changes
color to amber,
pointer blinks.
Ground
Excessive
Deviation
arrows
Low visibility
takeoff
deviation
from center
line.
Arrow shown
shall blink as long
as deviation
condition exists.
N/A
Airspeed
Odometer
outline
Airspeed low
alert.
Blinks as long as
alert is active.
Color changes to
amber.
Symbol Picture Condition 787 HUD
Behavior/Timing
787 PFD
Behavior/Timing
787 Flight Crew Operations Manual
Flight Instruments, Displays -
Head-Up Display System
Description
10.22.16 Boeing Proprietary
TCAS
Advisory
diagonal lines
–Vertical
speed exceeds
advisory
–Flight Path
is in unsafe
zone between
angled lines
Blink as long as
condition persists
N/A
LNAV
ANP/RNP
bars and
pointer
Alert
condition -
Flight
Technical
Error (FTE)
has been
exceeded for
5 seconds
Bars change in
aspect to hollow
while bars,
indices, and
pointer blink for 3
seconds, then bars
and indices
steady. Pointer
continues to blink
for 7 seconds,
then steady (total
sequence time is
10 seconds). Bars
remain hollow as
long as alert is
active.
Bars and indices
change to amber
and deviation
pointer blinks for
10 seconds, then
steady.
VNAV
ANP/RNP
bars and
pointer
Alert
condition -
Flight
Technical
Error (FTE)
has been
exceeded (for
5 seconds).
Bars change in
aspect to hollow
while bars,
indices, and
pointer blink for 3
seconds - then
bars and indices
steady. Pointer
continues to blink
for 7 seconds,
then steady (total
sequence time is
10 seconds). Bars
will remain
hollow as long as
alert is active.
Bars and indices
change to amber
and deviation
pointer blinks for
10 seconds, then
steady.
Symbol Picture Condition 787 HUD
Behavior/Timing
787 PFD
Behavior/Timing
(Before Alert)
(After Alert)
Before After
787 Flight Crew Operations Manual
Flight Instruments, Displays Chapter 10
Primary Flight Displays (PFDs) Section 30
Boeing Proprietary 10.30.1
10.30 Flight Instruments, Displays-Primary Flight Displays (PFDs)
Introduction
The PFDs present a dynamic color display of all the parameters necessary for
flight path control. The PFDs provide the following information:
The Mini-MAPs present a tactical display map with a fixed range of 20 nautical
miles. They provide immediate target and threat information and are placed below
the PFDs directly in front of each pilot. The Mini-MAPs display the flight plan
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：787機(jī)組操作手冊(cè)Flight Crew Operations Manual 2(110)