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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
B. Equipment
(1)
Trim Balance Kit - 856A2633G05 (ELECMA), CFM International, P.O. Box 15514, Cincinnati, OH 45215
(2)
Trim Balance Kit - 856A2605G22/G21/G18/G17/G13 (ELECMA), CFM International (optional to 856A2633G05)
(3)
Trim Balance Kit - 856A2605G21/G20/G12
(Spectral Dynamics), CFM International
(optional to 856A2633G05)
(4)
Trim Balance Kit - 856A2636G01 (ELECMA), CFM International (optional to 856A2633G05)
(5)
Trim Balance Kit - PBS 4100,
Mechanical Technology Inc,
968 Albany-Shaker Rd,
Latham, New York, 12110-1401
(6)
FFCCV Vibration Sensor Kit - 335-202-601-0, CFM International
NOTE: The FFCCV vibration sensor is necessary
____ when the No. 1 bearing vibration sensor does not funtion correctly.
(7)
Protective Mats (two required) - Rubber Manufacturer's Association, Grade SC43, neoprene sponge, 1 inch thick, approximately 3 x 4 feet with warning streamer attached.
(8)
Optional Equipment:
NOTE: The optional tool is used in the
____ computerized calculation of trim balance weight, quantity, and position.
(a) Multi-Engine Trim Balance Program -856A2678P01 CFM International P.O. Box 15514, Cincinnati, OH 45815
NOTE: To use this program, refer to
____ the Ground Support Equipment Manual (GSEM). CFMI-TP-GS.10 is available from CFM International.
NOTE: Trim Balance programs 856A2623 G2,
____ 856A2641, and 856A2650 replaced by 856A2678P01, Multi-Engine Trim Balance program.
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72-31-00
ALL ú ú C04 Page 507 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(9) Optional Support Equipment:
(a)
Software GW Basic 2.01 - Microsoft
Corporation, 10700 Northrup Way, Box
97200, Bellevue, WA 98009
(b)
IBM computer, PC convertible, or any IBM
compatible computer with graphic option -IBM World Trade Corporation, 821 United
Nations Plaza, New York, NY 10017
C. Consumable Materials
(1)
Tape - Speed
(2)
Grease - Graphite, CP2101
D. References
(1)
AMM 52-21-00/401, Emergency Exit Hatch
(2)
AMM 71-00-00/201, Power Plant - General
(3)
AMM 71-00-01/201, Power Plant - Trim Tables
(4)
AMM 71-00-47/101, Trouble Shooting - Misc. Observed Problems
(5)
AMM 71-11-02/201, Fan Cowl Panels
(6)
AMM 75-24-02/201, High Pressure Turbine Clearance Control Timer
(7)
AMM 77-31-00/001, Airborne Vibration Monitoring (AVM) System
(8)
AMM 77-31-01/401, Alternate No. 1 Bearing (NOB) Vibration (FFCCV)
Sensor
(9)
AMM 78-31-00/201, Thrust Reverser System
E. Access
(1) Location Zones
506 No. 1 Engine
606 No. 2 Engine
F. FOR KITS 856A2633G05, 856A2605G22/G21/G18/G17/G13, 856A2605G20/G12 and PBS 4100; Prepare For The Trim Balance Procedure (Fig. 501):
NOTE: FOR P85 4100 REFER TO THE MANUFACTRUERS DOCUMENTATION.
____
S 865-001-C00
CAUTION: USE CAUTION WHEN YOU INSTALL THE TRIM BALANCE EQUIPMENT AND THE
_______
RELATED TEST LEADS. IF THE EQUIPMENT OR LEADS ARE NOT
INSTALLED CORRECTLY, IT CAN BE NECESSARY TO OPERATE THE ENGINE
TOO MANY TIMES.
(1) To install the kit on the engine, do the steps that follow (optional to the installation in the E/E bay).
WARNING: DO THE DEACTIVATION OF THE THRUST REVERSERS TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
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