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be completed if suitable visual reference is established. Be alert for the mistrim
condition that may exist on some airplanes. With multiple autopilots engaged, 3
units of up trim may be introduced to prevent a hard landing if a flare fault occurs.
October 31, 2004
767 Flight Crew Training Manual
Approach and Missed Approach
Copyright © The Boeing Company. See title page for details.
5.22 FCT 767 (TM)
If a go-around is initiated with the autopilot disengaged, press the GA switch. If
the GA switch is not pressed, the flight directors remain in the approach mode.
Pilot Response to Approach, Landing, and Go-Around Alerts
Note: All other EICAS messages are dealt with according to QRH procedures.
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
AUTOTHROT
DISC (Caution)
*Continue with
manual thrust
control (if Cat
IIIb-***)
*** N/A Continue with
manual thrust
control
SPEEDBRAKES
EXT (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 (as installed)
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.
October 31, 2004
767 Flight Crew Training Manual
Approach and Missed Approach
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 5.23
ILS Approach/Landing Geometry
The following diagrams use these conditions:
• data is based on typical landing weight
• airplane body attitudes are based on flaps 30, VREF 30 + 5 and should be
reduced by 1° for each 5 knots above this speed
• pilot eye height measured at point when main gear crosses threshold
• airplane ILS antenna crosses threshold at 50 feet.
Non-Normal Operations (ILS or GLS)
This section describes pilot techniques associated with engine inoperative
approaches. Techniques discussed minimize workload, improve crew
coordination, and enhance flight safety. However, a thorough review of applicable
Non-Normal Checklists associated with engine inoperative flight is a prerequisite
to understanding this section.
Model Glide Path
(deg)
Airplane
Body
Attitude
(deg)
Main Gear
(feet)
Pilot Eye
Height
(feet)
Threshold to
Main Gear
Touchdown
Point - No Flare
(feet)
767
- 200
2.5 2.8 30 54 678
3.0 2.3 30 53 565
767
- 300
2.5 2.7 29 53 660
3.0 2.2 29 53 550
767
- 400
2.5 2.9 26 53 604
3.0 2.4 26 52 503
Threshold
ILS Antenna ILS Glide Path Pilot Eye Height
Height
Glide Slope
Transmitter
Threshold
Touchdown
Main Gear
(No Flare)
954 ft. (3° GS)
to
1145 ft. (2.5° GS)
Touchdown Point
October 31, 2004
767 Flight Crew Training Manual
Approach and Missed Approach
Copyright © The Boeing Company. See title page for details.
5.24 FCT 767 (TM)
One Engine Inoperative
AFDS management and associated procedures are similar to those used during the
normal ILS approach. Flight director (manual) or autopilot may be used. Weather
minima for an ILS with one engine inoperative are specified in the applicable
AFM and/or the operators Operational Specification or equivalent.
During a multiple autopilot approach, the pilot must use rudder pedal pressure to
control yaw, followed by rudder trim to maintain an in-trim condition until LAND
2 or LAND 3 annunciates. When LAND 2 or LAND 3 annunciates, rudder inputs
are controlled by the autopilots. Directional control (yaw) is not affected by rudder
　
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