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 3) Make sure that the AVM signal conditioner shows Test OK.
 NOTE: The AVM signal conditioner passed the self test.
____ After Test OK, push and release the NO button to show Fault History? on the front display of the AVM signal conditioner. If the AVM signal conditioner is left alone for 5 minutes, the display will then turn off.
 4)  If the AVM signal conditioner shows XX Faults Display? or is blank, there is a failure of the AVM signal conditioner.
 NOTE: XX is the total number of faults.
____
 a)  If the front display on the AVM signal conditioner is blank, replace the AVM signal conditioner and do the self test again.
 b)  If there are XX Faults Display?, do the system test for the Airborne Vibration Monitoring (AVM) System (AMM 77-31-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 77-31-00
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 (4)  AIRPLANES WITH AN S332T304 AVM;
 Read the fault history in the AVM signal conditioner
 (AMM 77-31-00/201).
 S 975-011-C00
 (5)  AIRPLANES WITH AN S360N021-100 OR -102 AVM;
 Read the fault history in the AVM signal conditioner with the ARINC
 429 reader (AMM 77-31-00/201).
 NOTE:____ If you find fault history, this is the fault history from
 other flights or other engine operations.

 S 975-065-C00
 (6)  AIRPLANES WITH AN S360N021-113, -114, -201, -202 OR -213 AVM; Read the BITE maintenance messages in the AVM signal conditioner (AMM 77-31-00/201).
 NOTE: If you find BITE maintenance messages, these are the BITE
____ maintenance messages from other flights or other engine operations.
 S 865-048-C00
 WARNING: MAKE SURE THE AIRPLANE BRAKES ARE ENGAGED AND THE ENGINE
_______ EXHAUST (JET BLAST) WILL NOT BE DANGEROUS TO PERSONS ON THE GROUND.
 (7)  Do the Power Plant Operation (Normal) procedure to start the engine (AMM 71-00-00/201).
 (a)  
Operate only one engine to do this test.

 (b)  
Operate the engine at idle power or more than idle power.

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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
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 (8)  Monitor the vibration indication on the P2 panel in the flight compartment.
 (a)  
Make sure the vibration indication is more than zero.

 (b)  
Make sure the vibration indication is shown for the engine that you operate.

 (c)  
Slowly move the thrust lever forward to 70% N1.

 (d)  
Let the engine operation become stable for 2 minutes.

 (e)  
Move the thrust lever rearward to idle power.

 S 865-019-C00
 (9)  
Do the Power Plant Operation (Normal) procedure to do the engine shutdown (AMM 71-00-00/201).

 S 975-067-C00

 (10)
 AIRPLANES WITH AN S332T304 AVM; Read the fault history in the AVM signal conditioner (AMM 77-31-00/201).

 S 975-068-C00

 (11)
 AIRPLANES WITH AN S360N021-100 OR -102 AVM; Read the fault history in the AVM signal conditioner with the ARINC 429 reader (AMM 77-31-00/201).

 NOTE: If you find fault history, this is the fault history from
____
 other flights or other engine operations.

 S 975-070-C00
 (12) AIRPLANES WITH AN S360N021-113, -114, -201, -202 OR -213 AVM; Read the BITE maintenance messages in the AVM signal conditioner (AMM 77-31-00/201).
 NOTE: If you find BITE maintenance messages, these are the BITE
____ maintenance messages from other flights or other engine operations.
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