CONTINUOUS AXIAL CRACK 
INNER COMBUSTION CHAMBER 
BULKHEAD 
FWD 
OUTER COMBUSTION CHAMBER 
INDIVIDUAL AXIAL CRACK BURNEDLOUVER LIP GAP AREAS DISCOLORED OR MILDLYCLOSURE AND BURNING BURNED AREA 
CONTINUOUS AXIAL CRACKS (MORE THAN 3 LOUVERS),  
YOU MUST DO AN OD (COLD SIDE) INSPECTION.  IF  1ST-STAGE  L-A3324 (0395)  
YOU CAN NOT DO AN OD INSPECTION, THIS CRACK  HPT VANES  
IS NOT PERMITTED. 
FWD BENT, BUCKLED OR DISTORTED
BULKHEAD LOUVERS 
INNER COMBUSTION CHAMBER 
BURN STREAK 
OUTER COMBUSTION CHAMBER 
MISSING LOUVER CHIPPED COATING,  1ST-STAGE HPT VANES
LIP MATERIAL COATING LOSS  L-A3328 
VIEW IN THE CIRCUMFERENTIAL DIRECTION 
Inner and Outer Combustion Chamber Distress Figure 619 (Sheet 1) 
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú N02 Page 682L ú Jun 18/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
CONTINUOUS AXIAL CRACK
INDIVIDUAL AXIAL CRACKS, THESE CRACKS CAN BE A CONTINUOUS CRACK ON THE ID SIDE 
LOUVER KNUCKLE 
OD (COLD SIDE) VIEW OF OUTER COMBUSTION CHAMBER 
L-B0742 (0000)  
PW V 
Inner and Outer Combustion Chamber Distress  
Figure 619 (Sheet 2) 
F69414
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú N02 Page 682M ú Jun 18/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
COMBUSTION CHAMBER 
VIEW LOOKING CIRCUMFERENTIALLY 
L-A3325
CRACK 
LENGTH
L-A3327 
Inner and Outer Combustion Chamber Distress Figure 619 (Sheet 3) 
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú N02 Page 682N ú Jun 18/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
0.43 INCH (10.922 mm) INNER FACE WIDTH (REF)
FUEL INJECTOR 
ENDCAP SEGMENTS
SEE
COMBUSTION CHAMBER BULKHEAD 
Combustion Chamber Bulkhead and Fuel Injector Guide Heatshield Distress 
Figure 620 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú N02 Page 682O ú Jun 18/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
0.30 INCH (7.62 mm) 
FROM EDGE OF INNER FACE
EXPOSED 
TO OUTER FACE AT I.D LOCATION 
OUTER HEATSHIELD FACE (PERIMETER) 
INNER HEATSHIELD FACE 
OUTER HEATSHIELD FACE EROSION (DECREASED TIME INSPECTION LIMIT) 
EROSION OF OUTER HEATSHIELD FACE 
L-A3321 
TO OUTER FACE AT O.D LOCATION 
FUEL INJECTOR GUIDE HEATSHIELD
CIRCUMFERENTIAL CRACKS CRACKS 
RADIAL 
END CAP SEGMENT LIBERATION (BROKEN AWAY) FUEL INJECTOR ENDCAP SEGMENTS
IMPINGEMENT 
HOLES (EXAMPLE)
A-A Combustion Chamber Bulkhead and Fuel Injector Guide Heatshield DistressFigure 620 (Sheet 2) 
C15899
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 72-00-00
 ALL  ú ú N02 Page 682P ú Jun 18/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
No. 16 - Combustion Chamber Inspection
______________________________________
 (a)  These conditions of damage occur in the inner and outer combustion chamber assembly: 1) The conditions that follow are examples of burned or eroded
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 发动机 ENGINE 1(73)