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时间:2011-04-13 08:00来源:蓝天飞行翻译 作者:航空
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 34-24-01
 ALL  ú ú 01 Page 403 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 STATIC INVERTER/ILS PROCESSOR - REMOVAL/INSTALLATION
____________________________________________________
 1.  General_______
 A.  This procedure contains two tasks. The first task is for the removal of the static inverter/ILS processor. The second task is for the installation of the inverter/ILS processor.
 B.  The B339 static inverter/ILS processor is installed in the main equipment center on shelf No. 3 of the E1 electronics equipment rack.
 TASK 34-24-02-004-001
 2.  Remove The Static Inverter/ILS Processor________________________________________
 A.  References
 (1)  
AMM 06-09-01/201, Body Section 41 Access Doors and Panels

 (2)  
AMM 20-11-22/401, Electrical/Electronic Black Box


 B.  Access
 (1)  
Location Zones 117 Electrical and Electronics Compartment, LH

 (2)  
Access Panels
 117AL Electronics Compartment Access Door

 

 C.  Remove the Static Inverter/ILS Processor
 S 864-002
 (1) Open these circuit breakers and attach the DO-NOT-CLOSE tags:
 (a)  P7 Overhead Circuit Breaker Panel
 1) 7A6 NAV RADIO ILS L
 2) 7B24 STBY INSTR ILS IND
 3) 7B25 STBY INSTR ATTD IND

 S 014-014
 (2)  Open the 117AL access door to the electronics compartment to get to the static inverter/ILS processor (AMM 06-09-01/201).
 S 024-013
 CAUTION: DO NOT TOUCH THE STATIC INVERTER/ILS PROCESSOR BEFORE YOU
_______ CONNECT THE GROUND STRAP BETWEEN YOUR WRIST AND THE ELECTROSTATIC GROUND JACK. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE STATIC INVERTER/ILS PROCESSOR.
 (3) Remove the static inverter/ILS processor (AMM 20-11-22/401).
 TASK 34-24-02-404-004
 3.  Install The Static Inverter/ILS Processor_________________________________________
 A.  References
 (1)  
AMM 06-09-01/201, Electronics Compartment Access Doors and Panels

 (2)  
AMM 20-11-22/401, Electrical/Electronic Black Box

 (3)  
AMM 24-22-00/201, Manual Control


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 34-24-02
 ALL  ú ú 01 Page 401 ú Oct 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (4)  AMM 34-31-00/501, ILS Navigation System
 B. Access
 (1)  
Location Zones
 117 Electrical and Electronics Compartment, LH


 (2)  
Access Panels
 117AL Electronics Compartment Access Door

 

 C. Install the Static Inverter/ILS Processor
 S 864-005
 (1)  Make sure these circuit breakers are open with the DO-NOT-CLOSE-TAGS attached:
 (a)  P7 Overhead Circuit Breaker Panel
 1) 7A6 NAV RADIO ILS L
 2) 7B24 STBY INSTR ILS IND
 3) 7B25 STBY INSTR ATTD IND

 S 404-011
 CAUTION: DO NOT TOUCH THE STATIC INVERTER/ILS PROCESSOR BEFORE YOU
_______ CONNECT THE GROUND STRAP BETWEEN YOUR WRIST AND THE ELECTROSTATIC GROUND JACK. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE STATIC INVERTER/ILS PROCESSOR.
 (2)  
Install the static inverter/ILS processor (AMM 20-11-22/401).

 S 864-007

 (3)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:


 (a)  P7 Overhead Circuit Breaker Panel
 1) 7A6 NAV RADIO ILS L
 2) 7B24 STBY INSTR ILS IND
 3) 7B25 STBY INSTR ATTD IND

 S 864-008
 (4)  
Supply the electrical power (AMM 24-22-00/201).

 S 714-009

 (5)  
Do a test of the static inverter/ILS processor:

 (a)  
Tune to an ILS frequency (AMM 34-31-00/501).

 (b)  
Set the mode selector switch on the standby attitude/ILS indicator to APP.

 (c)  
Do a left ILS receiver self-test (AMM 34-31-00/501)

 (d)  
Make sure the conditions that follow occur on the standby attitude/ILS indicator: 1) G/P and LAT flags show for approximately 3 seconds. 2) G/P and LAT flags retract from view for approximately 2
 
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