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时间:2011-04-13 08:03来源:蓝天飞行翻译 作者:航空
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Figure 102 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F00199
A
747-400 MAINTENANCE MANUAL
 GLOBAL POSITIONING SYSTEM - ADJUSTMENT/TEST
___________________________________________
 1. General
_______
 A. This procedure has two tasks.
 (1)  This first task is an operational test of the Global Positioning System (GPS). The second task is a system test of the GPS.
 NOTE: The airplane must be moved to a position where the GPS
____ antennas have a clear view of the GPS satellites.
 TASK 34-58-00-715-001
 2. Operational Test - Global Positioning System
____________________________________________
 A. General
 (1)  This task does a GPS position check.
 B. Reference
 (1)  AMM 24-22-00/201, Manual Control
 C. Access
 (1)  Location Zones
 221 Control Cabin, LH
 222 Control Cabin, RH

 D. Prepare for the Test
 S 865-002
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 865-003

 (2)  
Make sure these circuit breakers are closed:


 (a)  On the overhead circuit breaker panel, P7: 1) 7A06 MMR L 2) 7B17 MMR R
 E. Procedure
 S 585-004
 (1)  
Move the airplane to a position where the GPS antennas have a clear view of the GPS satellites.

 S 715-007

 (2)  
Make sure there are no GPS failure indications on the top EICAS display.

 S 715-008

 (3)  
Do these steps to see the GPS position on an FMC CDU:

 (a)  
Push the INIT/REF key on one of the CDUs.

 (b)  
Push the line select key (LSK) that is adjacent to <INDEX.

 


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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (c)  
Push the LSK that is adjacent to <POS.

 (d)  
Push the PREV PAGE key on the CDU. 1) Make sure the GPS R position is shown on the line above <INDEX.


 2)  Make sure the GPS L position is shown on the line above the GPS R position.
 NOTE: As much as 10 minutes of time can be necessary for
____ the positions to show on the CDU.
 TASK 34-58-00-735-009
 3.  System Test - Global Positioning System
_______________________________________
 A.  General
 (1)  This task does a GPS interface check.
 B.  Reference
 (1)  AMM 24-22-00/201, Manual Control
 C.  Access
 (1)  Location Zones
 221 Control Cabin, LH
 222 Control Cabin, RH

 D.  Prepare for the Test
 S 865-010
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 865-019

 (2)  
Make sure these circuit breakers are closed:


 (a)  On the overhead circuit breaker panel, P7: 1) 7A06 MMR L 2) 7B17 MMR R
 E.  Procedure
 S 585-011
 (1)  
Move the airplane to a position where the GPS antennas have a clear view of the GPS satellites.

 S 715-012

 (2)  
Make sure there are no GPS failure indications on the top EICAS display.


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 ALL  ú ú 07 Page 502 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 715-016
 (3)  Do these steps to do a check of the IRS/GPS data busses:
 (a)  
 
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