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flight deck is designed so that a quick analysis and decision can be made for
virtually all non-normal or fault situations using the crew alerting system and
autoland status annunciation.
October 31, 2006
777/787 Flight Crew Training Manual
Approach and Missed Approach
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 5.21
If the flight crew is aware of the airplane equipment requirements for the
approach, the following can be used for any AFDS fault indication:
Above Alert Height
Immediately after recognizing the fault from the crew alerting system, instrument
flags, or engine indications, check autoland status annunciation.
• if the autoland status annunciation has not changed, and the equipment is
not required for the approach or can be switched, (e.g., flight director),
continue the approach
• if the autoland status annunciation has changed, or the equipment is
required for the approach, adjust to the appropriate higher minimums or
go-around.
At or Below Alert Height
For any EICAS alert, continue the approach to an automatic landing and rollout
unless the alert is accompanied by a master caution. The pilot should not intervene
unless it is clearly evident that pilot action is required.
A thorough fault analysis was included as a part of the fail operational
certification. Below 200 feet AGL a safe landing and rollout can be made with any
probable failure conditions.
Flight crew alerts (messages, lights, or aurals) may occur at any time during the
approach. Below alert height, multiple autopilots protect against any probable
system failure and will safely land the airplane. The pilot should not intervene
below AH unless it is evident that pilot action is required. If a fault affects the
autobrakes, assume manual control of braking. Accomplish related procedures for
system faults after rollout is complete and manual control of the airplane is
resumed.
If the autopilot is unintentionally disengaged below alert height, the landing may
be completed if suitable visual reference is established.
If a go-around is initiated with the autopilot disengaged, press the TO/GA switch.
If the TO/GA switch is not pressed, the flight directors remain in the approach
mode.
October 31, 2006
777/787 Flight Crew Training Manual
Approach and Missed Approach
Copyright © The Boeing Company. See title page for details.
5.22 FCT 777/787 Preliminary (TM)
Pilot Response to Approach, Landing, and Go-Around Alerts
Note: A master caution light and aural below AFDS alert height, while in IMC
conditions, require a go-around. If suitable visual reference is established,
Alert Above 200 ft.
AGL
Below 200
ft. AGL
During
Rollout
During
Go-Around
Master Warning/Caution Lights with EICAS Messages (see note)
AUTOPILOT DISC
(Warning)
*Execute
manual
go-around
**Execute
manual
go-around
Execute
manual rollout
Execute manual
go-around
AUTOPILOT
(Caution)
*Execute
go-around
**Execute
go-around
Disengage
autopilot and
execute a
manual rollout
Disengage
autopilot and
execute a manual
go-around
AUTOTHROTTLE
DISC (Caution)
*Continue with
manual thrust
control (if Cat
IIIb-***)
*** N/A Continue with
manual thrust
control
ENGINE FAIL L, R
ENGINE THRUST
L, R (Caution)
Continue
approach
****
Continue
approach
Continue
rollout
Continue
go-around
SPEEDBRAKE
EXTENDED
(Caution)
Retract
speedbrakes
**Execute
go-around
N/A Retract
speedbrakes
Autoland Status Annunciation
NO LAND 3
or
LAND 2
*Continue
approach
(if Cat IIIbgo-
around)
N/A
(message
inhibited)
N/A N/A
NO AUTOLAND *Execute
go-around
**Execute
go-around
N/A N/A
Flashing G/S or LOC Indicators
ILS Deviation Alert *Execute
go-around
**Execute
go-around
N/A N/A
* If suitable visual reference is not established.
** If suitable visual reference is established, land.
***Refer to the AFM or approved procedures for recommended pilot response.
**** Master caution light and aural inhibited during approach below 200 ft. AGL.
October 31, 2006
777/787 Flight Crew Training Manual
Approach and Missed Approach
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 5.23
　
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