C. Procedure
 S 865-113
 (1) Make sure you did the Prepare For Input Parameter Test task.
 S 865-364
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)
Supply hydraulic power for systems A and B (AMM 29-00-00/201).

 S 735-362

 (3)  
Do this test of the position signals from the stabilizer:

 (a)  
Set the portable tester to SUBFRAME 0, WORD 23.

 (b)  
Put the horizontal stabilizer in the positions shown in the table (AMM 27-41-00/501).

 (c)  
Make sure the portable tester displays agree with the values in the table.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 BEJ 101-112, 114-999; ú  31-24-02
 ú ú 14 Page 525 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ~........................................................... | | TEST | | | PARAMETER | CONDITION | TESTER DISPLAY | ............................................................. | STABILIZER| 41.57" Dim B | 7705 to 0074 (nominal 0000) | | | (3 units trim) | | | | 27.16" Dim B | 0440 to 0660 (nominal 0545) | | | (13 units trim) | | 2...........….................….............................1
 S 825-118
 (4)  
Adjust the stabilizer position sensor if it is necessary (AMM 27-41-00/501).

 S 865-119

 (5)  
Remove the hydraulic power if it is not necessary (AMM 29-00-00/201).

 S 865-120

 (6)  
If you will do no more tests, then do this task: "Put the Airplane to its Usual Condition."

 TASK 31-24-02-735-238
 16. Airborne Vibration Monitor Signals Test_______________________________________
 A. Special Tools and Equipment
 (1)  Interface Technology model 429 test set
 B. Reference
 (1)  AMM 77-31-03/401, Airborne Vibration Monitoring (AVM) System
 C. Access
 (1)  Location Zones
 101 Control Cabin - Left
 102 Control Cabin - Right

 D. Procedure
 S 865-239
 (1)  
Make sure you did the Prepare For Input Parameter Test task.

 (2)  
Do this test of the signals from the airborne vibration monitor:

 S 735-240
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 BEJ 101-112, 114-999; ú  31-24-02
 ú ú 12 Page 526 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 NOTE: Some ARINC 429 transmitters do not produce enough current to
____ generate the desired test results. Instead, the ARINC 429 transmitter can cause a value of 3000 to show on the portable tester. If you get a value of 3000, use a different tester and do the test again.
 (a)  
Open this circuit breaker:

 1)  P6 Panel
 a) ENG VIB MON

 (b)  
Remove the Anti-Vibration Monitor (AVM) signal conditioner from the E1-2 electronics shelf in the main equipment center (AMM 77-31-03/401).

 (c)  
Connect the (A) side of the ARINC 429 test set to pin C6 on connector D3228A.

 (d)  
Connect the (B) side of the ARINC 429 test set to pin D6 on connector D3228A.

 (e)  
Close this circuit breaker:

 1)  P6 Panel
 a) ENG VIB MON

 (f)  
Set the 429 test set to transmit on channel 1 at low speed.

 (g)  
Set the ARINC 429 test set as follows:
 1) LABEL 354
 2) update rate is 200ms

 (h)  
Set the ARINC 429 test set to these bit conditions:

 NOTE: The FLS setting is only applicable to the Interface
____
 Technology model 429A test set.

 ~............................................................. | FLS | 31  | 30  | 29  | 28  | 27  | 26 thru 11  | 10  |  9  | ............................................................... | L |  1  |  1  |  0  |  1  |  1  | 0 | 0 | 1 | 2.....….....….....….....….....….....….............….....….....1
　
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