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时间:2011-04-08 11:53来源:蓝天飞行翻译 作者:航空
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(1)  This task gives instructions to do an inspection and replace CFMI engine tubes and hoses. These instructions are not applicable to Boeing supplied parts.
 B.  Consumable Materials
 (1)  
G02353 Lubricant, petrolatum (CP2854) - VV-P-236

 (2)  
D00599 Oil, engine (CP2442) - CFMI SB 79-001

 (3)  
G02345 Lockwire (CP8001)

 (4)  
G02345 Lockwire (CP8006)


 C.  References
 (1)  
AMM 73-11-05/601, Fuel Manifold

 (2)  
AMM 70-30-01/201, Seals (Preformed Packings and O-rings) and Gaskets

 (3)  
AMM 71-00-00/501, Power Plant


 D.  Access
 (1)  Location Zones
 410 No. 1 Engine
 420 No. 2 Engine

 E. Procedure ú ú S 212-060-C00 ú         ú
CAUTION: USE THESE INSTRUCTIONS FOR CFMI SUPPLIED PARTS ONLY.
_______ DO NOT
 ú  USE THESE INSTRUCTIONS FOR BOEING SUPPLIED PARTS. DAMAGE TO
 ú  EQUIPMENT COULD OCCUR.
 ú
 (1)  Do the steps that follow if you see damage on a tube, hose or fitting on the engine (Fig. 203):
 NOTE: The limits in this table are general and do not replace
____ the limits on components given in other locations in this manual.
 For the inspection of the fuel manifold, do this task: Fuel Manifold Inspection (AMM 73-11-05/601).
 (a)  Tubing for:
 1)  Splits, cracks or kinks:
 a) Not serviceable.
 b) Replace the tube.

 2)  Dents or flat areas:
 a)  Any amount is permitted when the contour is not more than 20 percent of the original tube outside diameter (OD).
 b)  If the damage is more than 20 percent, replace the tube.
 3)  Nicks or scores on drain lines, drain shrouds, and scavenge lines, but does not include the aft sump oil scavenge line: a) The maximum permitted depth is not more than 0.010 inch
 (0.25 mm) after blending. b) Blend the nicks or scores.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú C01.1 Page 208 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

SEATING SURFACES OF SEATING SURFACES OF
SPHERICAL SEAT FITTINGS

TUBE/HOSE FERRULE

GMM-1130351-00-A
Tube and Hose Fitting Seating Surfaces Figure 203 (Sheet 1)
 F40773
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú C01 Page 209 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

SURFACE B
GMM-1130356-00-A
Tube and Hose Fitting Seating Surfaces Figure 203 (Sheet 2)
F40822
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú C01 Page 210 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

(2.5 x D)  (2.5 x D)
HOSE ASSEMBLY

GMM-1130355-00-A
Tube and Hose Fitting Seating Surfaces Figure 203 (Sheet 3)
 F40833
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú C01 Page 211 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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