• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-29 11:36来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

When the localizer frequency goes invalid, the frequency/ identifier line goes out of view. The localizer and glideslope pointers and scales go out of view.
ILS Course
When the ILS course input goes invalid, these are the displays that go out of view:
*
CRS display and ILS course

*
Localizer deviation indication and scale

*
Glideslope deviation pointer and scale

*
Course pointer.


Localizer Deviation
When the localizer deviation is invalid, the localizer deviation bar and scale go out of view. The LOC flag shows when all ILS receivers fail.
Glideslope Deviation
When the glideslope deviation is invalid, the glideslope deviation pointer and scale go out of view. The G/S flag shows when all ILS receivers fail.
EFFECTIVITY BEJ ALL  34-31-00 
Page 58 
D633W101-BEJ  Sep 05/2002 

 

777 AIRCRAFT MAINTENANCE MANUAL


ILS -ND ILS INVALID DISPLAY

EFFECTIVITY BEJ ALL  34-31-00 
Page 59 
D633W101-BEJ  Jan 05/2002 


ILS -PFD AND ND ILS TEST DISPLAYS

General
Use the maintenance access terminal (MAT) to do a test of the multi-mode receivers (MMRs). The MAT sends the test command to the left AIMS cabinet. The central maintenance computer function of the left AIMS cabinet sends the command to the MMR.
Test Sequence
The receivers start their test sequence when the test command comes from the AIMS cabinet. This is the sequence:
*
Invalid data for the first three seconds

*
NCD data for approximately two seconds

*
Valid data -glideslope pointer up one dot, localizer pointer left one dot for 3 seconds

*
Valid data -glideslope pointer down one dot, localizer pointer right one dot for 3 seconds

*
Back to pretest displays.


The AIMS cabinets change the ILS display source when a receiver goes invalid. For this reason, the LOC and G/S flags do not show while the receiver test sequence goes invalid. To see the flags in the test sequence, the receivers that are not in test must be in a failed condition or power removed.
When the test sequence goes NCD, the localizer pointers and glideslope pointers go out of view.
EFFECTIVITY BEJ ALL  34-31-00 
Page 60 
D633W101-BEJ  Sep 05/2002 

 

777 AIRCRAFT MAINTENANCE MANUAL


ILS -PFD AND ND ILS TEST DISPLAYS

EFFECTIVITY BEJ ALL  34-31-00 
Page 61 
D633W101-BEJ  Jan 05/2002 


ILS -FRONT PANEL TEST

Description
Push the test switch on the front of the receiver to start a test of the receiver.
The receiver does a lamp test for the first three seconds then goes to an NCD condition for the next three seconds.
The receiver then does a check of the internal receiver circuits. Test results show on the status LEDs.
Training Information Point
The maintenance manual and the fault isolation manual do not have a task for the line maintenance technician to do a test from the front panel of the multi-mode receiver (MMR). You must do all tests for the MMR from the MAT or a PMAT.
Many LRUs on the 777 are compatible with other model airplanes that do not have a central maintenance computing system (CMCS). For that reason, these LRUs have a front panel test feature.
EFFECTIVITY BEJ ALL  34-31-00 
Page 62 
D633W101-BEJ  Sep 05/2002 

 

777 AIRCRAFT MAINTENANCE MANUAL


ILS -FRONT PANEL TEST

EFFECTIVITY BEJ ALL  34-31-00 
Page 63 
D633W101-BEJ  Jan 05/2002 


ILS -GROUND TEST

General
You can do a test of the ILS system from the MAT. These are the tests that are available from the operational test selection on the MAT:
*
Center instrument landing system

*
Left instrument landing system

*
Right instrument landing system.


Operational Test
The operational test make sure that the instrument landing system is serviceable.
EFFECTIVITY BEJ ALL  34-31-00 
Page 64 
D633W101-BEJ  Sep 05/2002 

 

777 AIRCRAFT MAINTENANCE MANUAL


ILS -GROUND TEST

EFFECTIVITY BEJ ALL  34-31-00 
Page 65 
D633W101-BEJ  Jan 05/2002 

 

777 AIRCRAFT MAINTENANCE MANUAL

THIS PAGE IS INTENTIONALLY LEFT BLANK

34-32-00

Page 1 D633W101-BEJ Jan 05/2002
BOEING PROPRIETARY -Copyright # -Unpublished Work -See title page for details.

MARKER BEACON SYSTEM -INTRODUCTION

Purpose
The marker beacon system supplies visual and aural indications when the airplane flies over marker beacon transmitters.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:777 AMM 飞机维护手册 导航 Navigation 1(30)