737-300 400 500 AMM 飞机维护手册 动力装置 POWER PLANT 1(78)

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 71-00-00
 ALL  ú ú C11 Page 571 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TEST NO. 9 - REPLACEMENT ENGINE TEST (PRETESTED)________________________________________________
 (l) (m)  2) Open these circuit breakers on the panel, P18. a) FLIGHT RECORDER AC b) FLIGHT RECORDER DCIf the FLIGHT RECORDER light does not operate correctly, do a check of the flight recorder system (AMM 31-24-00/501).Connect the CSD (AMM 24-11-11/501).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú C10 Page 572 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TEST NO. 10 - REPLACEMENT ENGINE TEST (UNTESTED)
________________________________________________
 TASK 71-00-00-725-019-C00
 11. Test No. 10 - Replacement Engine Test (Untested)
________________________________________________
 A. General
 (1)  
This test gives the data after a new installation of an untested engine.

 (2)  
An untested engine is one that has not been tested in an approved test cell after one of these maintenance actions:

 (a)  
Separation of any major module-to-major module flange (Fan Module, Core Module, LPT Module)

 (b)  
Separation of any minor module flange (HPC Top or Bottom Case, Fan and Booster Module, No. 1/2 Bearing Support Assembly, Inlet Gearbox, LPT Frame).

 

 NOTE: It is not necessary to do Test No. 10 after an LRU
____ removal/replacement if the removed engine had been tested in an approved test cell or on-wing before the LRU removal/replacement.
 B. Equipment
 (1)  
Container - 1 quart (1 liter) capacity,
 suitable for oil

 C.
Consumable Materials

 (1)  
Oil - Engine (Ref 70-10-01)

 D.
References

 (1)  
AMM 12-13-11/301, Engine Oil Servicing

 (2)  
AMM 12-13-21/301, Constant Speed Drive Servicing

 (3)  
AMM 12-13-41/301, Engine Starter Servicing

 (4)  
AMM 24-11-11/501, Generator Constant Speed Drive

 (5)  
AMM 24-11-11/601, Generator Constant Speed Drive

 (6)  
AMM 30-21-00/501, Inlet Cowl Anti-Icing System

 (7)  
AMM 31-24-00/501, Flight Recorder System

 (8)  
36-11-05/501, Engine Bleed Air Distribution System

 (9)  
AMM 71-00-00/201, Power Plant

 (10)
 AMM 71-00-54/101, Power Plant (Engine Indicating)

 (11)
 AMM 73-11-02/401, Fuel Filter Cartridge

 (12)
 AMM 78-31-00/201, Fan Thrust Reverser System

 (13)
 AMM 79-00-00/601, Oil

 (14)
 AMM 79-21-03/401, Oil Supply Filter Element

 (15)
 AMM 79-21-04/401, Scavenge Oil Filter Element

 E.
Access

 (1)  
Location Zones
 506 Engine No. 1
 606 Engine No. 2

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 71-00-00
 ALL  ú ú C12 Page 573 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TEST NO. 10 - REPLACEMENT ENGINE TEST (UNTESTED)
________________________________________________
 (2)  
Access Panels
 5737L/5837R Fan Cowl Assy
 5746L/5846R Fan Cowl Assy
 5738L/5838R Thrust Reverser Cowl Assy
 5739L/5839R Thrust Reverser Cowl Assy

 F.  
Procedure

 S 725-020-C00
 (1)  
Do the Replacement Engine Test

 (a)  
Prepare the engine for the (normal) engine operation
 (AMM 71-00-00/201).
　
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