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767 Flight Crew Training Manual
Landing Chapter 6
Table of Contents Section TOC
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 6.TOC.1
6.TOC Landing-Table of Contents
Preface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.1
Landing Configurations and Speeds . . . . . . . . . . . . . . . . . . . . . . . . . 6.1
Maneuver Margin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.1
Non-Normal Landing Configurations and Speeds . . . . . . . . . . . . . . . 6.1
Non-Normal Landing Distance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.1
Visual Approach Slope Indicator (VASI/T - VASI) . . . . . . . . . . . . . 6.2
Three Bar VASI/T - VASI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.3
VASI Landing Geometry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.4
Precision Approach Path Indicator (PAPI) . . . . . . . . . . . . . . . . . . . 6.6
PAPI Landing Geometry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.6
Landing Geometry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.6
Visual Aim Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.6
Landing Runway Markings (Typical) . . . . . . . . . . . . . . . . . . . . . . . . 6.8
Threshold Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.9
Flare and Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.9
Landing Flare Profile . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.9
Bounced Landing Recovery . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10
Go-Around after Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.11
Normal Touchdown Attitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.11
Body Clearance at Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.15
Pitch and Roll Limit Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.18
After Touchdown and Landing Roll . . . . . . . . . . . . . . . . . . . . . . . . 6.22
Speedbrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.22
Directional Control and Braking after Touchdown . . . . . . . . . . . . . 6.23
October 31, 2004
767 Flight Crew Training Manual
Copyright © The Boeing Company. See title page for details.
6.TOC.2 FCT 767 (TM)
Landing -
Table of Contents
Factors Affecting Landing Distance . . . . . . . . . . . . . . . . . . . . . . . . 6.23
Wheel Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.27
Reverse Thrust Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.30
Crosswind Landings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.34
Landing Crosswind Guidelines . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.34
Crosswind Landing Techniques . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.35
Overweight Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.36
Overweight Autolands Policy . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.37
October 31, 2004
767 Flight Crew Training Manual
Landing Chapter 6
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 6.1
6. Landing- Preface
This chapter outlines recommended operating practices and techniques for
landing, rejected landings and landing roll. Techniques are provided to help the
pilot effectively utilize approach lighting, control the airplane during crosswind
landings and maintain directional control after landing. Additionally, information
on factors affecting landing distance and landing geometry is provided.
Landing Configurations and Speeds
For normal landings use flaps 30. This provides additional aft body clearance from
the runway compared to a flaps 25 landing.
Maneuver Margin
Flight profiles should be flown at, or slightly above, the recommended
maneuvering speed for the existing flap configuration. These speeds approximate
maximum fuel economy and allow full maneuvering capability (25° bank with a
15° overshoot).
Full maneuver margin exists for all normal and non-normal landing procedures
whenever speed is at or above the maneuver speed for the current flap setting. Full
maneuver margin exists with flaps 20 at VREF 30 + 5 during a go-around at
go-around thrust.
Airspeeds recommended for non-normal flight profiles are intended to restore
near normal maneuvering margins and/or aerodynamic control response.
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767机组训练手册Flight Crew Training Manual (FCTM)767(88)
