(2)  
The installation of the airborne vibration monitor (AVM) indicator.

 TASK 77-31-04-004-008-C00
 2. AVM Indicator Removal
_____________________
 A. Access
 (1)  Location Zone
 101, 102 Control Cabin

 B. Procedure
 S 864-009-C00
 (1)  Open this circuit breaker and attach a DO-NOT-CLOSE tag:
 (a)  P6 Load Control Center
 1) ENG VIBRATION MONITOR

 S 024-010-C00
 (2)  Do these steps to remove the AVM indicator:
 (a)  
Loosen the clamp adjustment screw for the AVM indicator on the center instrument panel (P2).

 (b)  
Pull the AVM indicator out from the panel so you can get access to the electrical connector.

 CAUTION: CLEARLY IDENTIFY CONNECTIONS BEFORE YOU DISCONNECT THEM.
_______ CROSS-CONNECTION OF THE TACHOMETER INDICATOR (ON THE P2 INSTRUMENT PANEL) IS A POSSIBILITY WHEN YOU WORK WITH THIS COMPONENT.
 (c)  Disconnect the electrical connector from the AVM indicator.
 TASK 77-31-04-404-011-C00
 3. AVM Indicator Installation
__________________________
 A. References
 (1) AMM 77-31-00/501, Airborne Vibration Monitoring (AVM) System
 B. Access
 (1)  Location Zone
 101, 102 Control Cabin

 C. Procedure
 S 424-012-C00
 (1)  Do these steps to install the AVM indicator:
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EIS ú

 77-31-04
 ú ú C02 Page 401 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CAUTION: POSITIVELY IDENTIFY CONNECTIONS BEFORE YOU CONNECT THEM
_______ AND DO FUNCTION CHECK UPON COMPLETION OF CONNECTION. CROSS CONNECTION OF THE AVM INDICATOR (ON THE P2 INSTRUMENT PANEL) IS A POSSIBILITY WHEN YOU WORK WITH THIS COMPONENT.
 (a)  
Connect the electrical connector to the AVM indicator.

 (b)  
Put the AVM indicator in the opening of the center instrument panel (P2).

 (c)  
Tighten the clamp adjustment screw for the AVM indicator on the center instrument panel (P2).

 S 864-013-C00
 (2)  Remove the DO-NOT-CLOSE tag and close this circuit breaker:
 (a)  P6 Load Control Center
 1) ENG VIBRATION MONITOR

 S 714-014-C00
 (3)  Do the operational test for the AVM system (AMM 77-31-00/501).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EIS ú

 77-31-04
 ú ú C02 Page 402 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.