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the pilot may perform a go-around or make a manual landing.
Note: All other EICAS messages are dealt with according to QRH procedures.
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.
777-200 - 777-300ER
Model Glide Path
(deg)
Airplane
Body
Attitude
(deg)
Main Gear
(feet)
Pilot Eye
Height
(feet)
Threshold to
Main Gear
Touchdown
Point – No Flare
(feet)
777
- 200
2.5 2.4 30 58 681
3.0 1.9 30 58 567
777
- 200LR
2.5 1.3 32 58 738
3.0 0.9 32 57 611
777
- 300
2.5 1.9 29 58 669
3.0 1.4 29 57 557
777
- 300ER
2.5 2.2 29 58 674
3.0 1.7 29 58 561
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, 2006
777/787 Flight Crew Training Manual
Approach and Missed Approach
Copyright © The Boeing Company. See title page for details.
5.24 FCT 777/787 Preliminary (TM)
787-8
Non-Normal Operations
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.
One Engine Inoperative
AFDS management and associated procedures are the same as for the normal ILS
approach. Flight director (manual) or autopilot and/or autothrottle may be used.
Weather minima for an ILS with one engine inoperative are specified in the
applicable AFM and/or the operator’s Operational Specification or equivalent.
777-200 - 777-300ER
During a multiple autopilot approach with the TAC inoperative, 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 trim with the autopilot in the LOC or
ROLLOUT modes.
787-8
During a multiple autopilot approach, the flight control system automatically
applies rudder inputs to controls 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 trim with the autopilot in the LOC or
ROLLOUT modes.
777-200 - 777-300ER
Flying an ILS approach with the TAC operating is the same as flying the approach
with the TAC inoperative except that before LAND 2 or LAND 3 is annunciated,
rudder control is automatically accomplished by the TAC. When LAND 2 or
LAND 3 annunciates, rudder inputs are controlled by the autopilots.
Glide Path
(deg)
Airplane
Body
Attitude
(deg)
Main Gear
(feet)
Pilot Eye
Height
(feet)
Threshold to
Main Gear
Touchdown
Point – No Flare
(feet)
2.5 TBD TBD TBD TBD
3.0 TBD TBD TBD TBD
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) 5.25
777-200 - 777-300ER
Refer to the Performance Inflight chapter of the QRH to determine if a flaps 30
landing is permissible. Intercept the localizer with flaps 5 at flaps 5 speed. When
the glide slope is alive, lower the landing gear and extend flaps to 20. If a flaps 20
landing will be made, set final approach speed and decelerate. If a flaps 30 landing
will be made, at glide slope capture, select landing flaps, set final approach speed,
and decelerate.
787-8
Refer to the Performance Inflight chapter of the QRH to determine if a flaps 30
landing is permissible. Intercept the localizer with flaps 5 at flaps 5 speed. When
the glide slope is alive, lower the landing gear and extend flaps to 20. If a flaps 20
landing will be made, set final approach speed and decelerate. If a flaps 25 or 30
　
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