(s)
Connect the electrical plug D3232 to the connector for the TRF vibration sensor.
(t)
Disconnect the test lead from the vibration sensor for the
No. 1 bearing on the fan frame bulkhead (inboard of the
3 o'clock strut).
(u)
Connect the electrical plug D3234 to vibration sensor connector for the No. 1 bearing.
(v)
Remove the test leads.
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS WHEN YOU CLOSE THE THRUST REVERSERS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(w)
Close the thrust reverser halves (AMM 78-31-00/201).
(x)
Close the fan cowl panels (AMM 71-11-02/201).
(y)
Do the deactivation procedure for the thrust reverser
(AMM 78-31-00/201).
(z)
During a subsequent engine run, do a check of the AVM
indications to make sure it operates correctly.
S 085-121-C00
(2) FOR KITS 856A2633G05, 856A2605G22/G18/G17/G13, AND 856A2605G20/G12; To remove the kit from the E/E bay, do the steps that follow (optional to the removal of kits from the engine) (Fig. 501).
(a)
Disassemble the cabin equipment.
(b)
Remove the output cable and tape from the fuselage to the E/E bay.
(c)
Install the emergency exit hatch (AMM 52-21-00/401).
(d)
Disconnect the cables from the SCU.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-31-00
ALL ú ú C02 Page 580H ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(e)
Remove the SCU from the E/E bay.
(f)
Disconnect the trim balance cables for the No.1 bearing and TRF from the AVM connecting case and the SCU.
(g)
Remove the AVM connecting case.
1) Put and keep the AVM connecting case in the storage box for the AVM trim balance equipment.
(h)
Install the AVM box in the AVM rack.
(i)
Close the E/E bay door.
(j)
During a subsequent engine run, do a check of the AVM indications to make sure it operates correctly.
S 085-120-C00
(3) FOR KIT 856A2636G01;
Do these steps to remove the equipment:
(a)
Disconnect the cabin equipment.
(b)
Remove the output cable and tape from the fuselage to the E/E bay.
(c)
Install the emergency hatch (AMM 52-21-00/401).
(d)
Disconnect the cables from the SCU.
(e)
Remove the SCU adapter from the rear of the SCU case.
(f)
Remove the strap from the case support assembly for the ARINC.
(g)
Disassemble the case support assembly for the ARINC.
(h)
Remove the AVM box from the case support assembly for the ARINC.
(i)
Remove the adapter from the rear of the case support assembly for the ARINC.
(j)
Install the AVM box in the AVM rack.
(k)
Close the E/E bay door.
(l)
During a subsequent engine run, do a check of the AVM indications to make sure it operates correctly.
TASK 72-31-00-805-049-C00
5. Phase Angle Matrix Determination
________________________________
A. General
(1)
The different vibration analyzer systems cause each different phase angle to be differently related to the balance screw locations. These differences are because of the electronic circuits, and other unknown causes.
(2)
To do the one shot plot procedure, an accurate phase angle matrix (a table that shows the relation of the phase angle to the balance screw locations at specified rotor speeds) must be made. To make a matrix for a specified cell or vibration system, the two subsequent procedures are recommended.
B. References
(1)
AMM 71-00-00/201, Power Plant - General
(2)
AMM 71-00-01/201, Power Plant - Trim Tables
(3)
AMM 75-24-02/201, High Pressure Turbine Clearance Control Timer
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 ENGINE 發動機 1(107)
