SPD LND HDG VERT
250 ALT SEL SPD
Airplane is descending on intercept heading for localizer with autoland and altitude preselect armed.
2.
SPD LND LOC ALT
165 CAP CAP
Localizer and altitude (preselect) capture have been initiated. Airplane is turning
onto localizer and leveling out on approach altitude.
3.
SPD LND LOC ALT
165 TRK HLD
Localizer and altitude capture have been completed. The airplane is tracking the localizer on a preselected altitude to intercept the glideslope.
4.
SPD LND LOC G/S
165 TRK CAP
Glideslope capture has been initiated. The airplane is tracking the localizer while
establishing a rate of descent to coincide with the glideslope.
5.
SPD LND LOC G/S
135 TRK TRK
Glideslope capture has been completed. Landing flaps selected and appropriate speed selected. Airplane is tracking localizer and glideslope.
6.
SPD AUT AUT AUT
135 G/A LND LND
When both pilot’s NAV and CRS are set to the ILS frequency and runway heading,
all autoland monitors are satisfied, and the radio altitude is 1500 feet or less, the flight guidance system engages into autoland mode.
7.
SPD AUT ALN AUT
135 G/A LND
At approximately 150 feet (radio altitude), align mode is initiated and the transition
from a crab angle to a forward slip begins for crosswind correction.
8.
At approximately 50 feet (radio altitude), the ATS retard mode and AP flare modes
RETD AUT G/A ALN FLAR
are initiated. The throttles are controlled to the retard schedule and the rate of descent is transitioned from glideslope to touchdown.
9.
RETD F/D ROL ROL
G/A OUT OUT
At main gear wheel spin-up, rollout begins and nose lowering is initiated for nosewheel touchdown. Flight director go-around mode is armed and available for 20 seconds.
ROL ROL
OUT OUT
If system does not have the roll out option,
the AP will disengage automatically 5 seconds after nose strut compression. The flight director will revert to basic roll and pitch mode when the autopilot disengages.
MD-80 Sec. 4 Page 147
Flight Manual Continental Rev. 01/01/00 #28
Sec. 4 Page 148 MD-80
Rev. 01/01/00 #28 Continental Flight Manual
Autoland Sheet 2
Autoland Approach Procedures
Note: The autopilot must be disengaged at 50 feet AGL or higher.
If autoland mode is armed but does not engage at 1500 feet AGL the flight crew should confirm that the compass headings and courses in the CRS windows are in agreement. If the autopilot will not engage in autoland mode, the flight crew may wish to cancel autoland mode and switch the autopilot back to ILS mode for a basic autopilot coupled ILS approach. This can be done by momentarily disengaging the autopilot and then re-engaging autopilot in ILS mode. Switching autopilot modes in this manner is only authorized above 1,000 feet. Once below 1,000 feet AGL the autopilot mode may not be switched.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:MD-80 Flight Manual 麦道80飞行手册 2(15)