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A
747-400 MAINTENANCE MANUAL
 (b)  Push the LSK that is adjacent to START TEST>.
 NOTE: IN PROGRESS shows during the test.
____
 S 755-041
 (2)  When IN PROGRESS goes out of view, look for PASS or FAIL> adjacent to <ADF-L or <ADF-R.
 NOTE: If a PASS indication shows, no failures occurred during the
____
 test.

 (a)  If FAIL> shows: 1) Push the LSK that is adjacent to FAIL> to see the GROUND TEST MSG pages for the failure. 2) Push the NEXT PAGE key until you find all the GROUND TEST MSG pages. 3) Make a list of all CMCS messages, CMCS message numbers, and ATA numbers that show on the GROUND TEST MSG pages.
 4)  Go the the CMCS Message Index of the Fault Isolation Manual (FIM) to find the corrective action for each CMCS message.
 F.  Put the Airplane in Its Usual Condition
 S 865-031
 (1)  Remove the electrical power if it is not necessary
 (Ref 24-22-00/201).

 TASK 34-57-00-715-035
 3.  ADF System - Operational Test
_____________________________
 A.  References
 (1)  AMM 24-22-00/201, Manual Control
 B.  Access
 (1)  Location Zones
 129 Keel Beam
 221 Control Cabin, LH
 222 Control Cabin, RH

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747-400 MAINTENANCE MANUAL
 (2)  Access Panels
 125B Center Electronics Access Door

 C.  Procedure
 S 865-036
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 745-051

 (2)  
Do the BITE self-test for the ADF Receivers.

 (a)  
Push either the right or left TEST switch on the applicable ADF receiver.

 (b)  
Make sure this sequence occurs on the ADF receiver LCD display: 1) TEST IN PROGRESS is displayed on the ADF front panel one second after the test switch is pressed.

 2)  TEST IN PROGRESS is displayed for four seconds with a moving thermometer along the bottom of the front panel display indicating the progress of the test from one to five seconds.
 3)  TEST COMPLETE, NO FAILURES is displayed on the front panel display.
 S 865-039
 (3)  Remove electrical power if it is not necessary (AMM 24-22-00/201).
 TASK 34-57-00-735-040
 4.  ADF System - System Test________________________
 A.  Standard Tools and Equipment
 (1)  Headphone
 B.  References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 32-09-02/201, Air/Ground Relays

 C.  Access
 (1)  Location Zones
 125 Center Equipment Center
 221 Control Cabin, LH
 222 Control Cabin, RH

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (2)  Access Panel
 125B Center Electronics Access Door

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

 S 865-006

 (2)  
Close these circuit breakers:

 (a)  P7 Overhead Circuit Breaker Panel:
 1) 7B9, NAV RADIO ADF L
 2) 7B20, NAV RADIO ADF R

 E. Air Mode ADF System
 S 865-025
 (1)  Prepare the airplane for air mode (AMM 32-09-02/201).
 S 865-033
 WARNING: MAKE SURE THAT YOU HAVE PREPARED THE AIRPLANE FOR AIR
_______ MODE BEFORE YOU OPEN THE CIRCUIT BREAKER THAT FOLLOWS. AUTOMATIC OPERATION OF AIRPLANE SYSTEMS IN THE AIR MODE CAN CAUSE INJURY OR DAMAGE.
 (2)  Open this circuit breaker and attach DO-NOT-CLOSE tag:
　
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