R Inspection/Check of the Fan-Outlet Guide Vanes (OGV) Figure 603/TASK 72-23-00-991-310- 13 (SHEET 1)
 F 『 EEFF : ALL E Page 61672-23-00
 E E Aug 01/05 E E ECES E F 『 E C F M E E E E 56-5B E
R Inspection/Check of the Fan-Outlet Guide Vanes (OGV) Figure 603/TASK 72-23-00-991-310- 23 (SHEET 2)
 F 『 EEFF : ALL E Page 61772-23-00
 E E Aug 01/05 E E ECES E F 『 E C F M E E E E 56-5B E
R Inspection/Check of the Fan-Outlet Guide Vanes (OGV) Figure 603/TASK 72-23-00-991-310- 33 (SHEET 3)
 F 『 EEFF : ALL E Page 61872-23-00
 E E Aug 01/05 E E ECES E
 F 『
 E C F M E
 E E
 E 56-5B E
 E E
 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
C. Wear, fretting,  If 0.02 in. (0,5 mm)  10 cycles serviceable 
 chafing on the top  max. width and 0.8 in.  extension is allowed. 
 of flange holes.  (20 mm) max. length. 
 D. Washer impression  If 0.032 in. (0,81 mm)  10 cycles serviceable 
 around flange  max. depth and 0.60 in.  extension is allowed. Do 
 holes  (15,25 mm) max.  blending (Ref. TASK 72-21- 
diameter.  00-320-003) until high 
 metal is removed. 
 3. Fan inlet case on B1 
 upstream bracket 
 location 
 (Ref. Fig. 604/TASK 
 72-23-00-991-328) 
 A. Wear on B1 flange 
 radius.  
R  |__X___|__A___| ..  
R  |__X___|__A___|  
R  
R  | 0,50 | 2,00 | ..  
R  | 6,50 | 0,68 |  
R  
R  | 1,00 | 1,90 | ..  
R  | 7,00 | 0,57 |  
R  
R  | 1,50 | 1,82 | ..  
R  | 7,50 | 0,48 |  
R  
R  | 2,00 | 1,74 | ..  
R  | 8,00 | 0,39 |  
R  
R  | 2,50 | 1,66 | ..  
R  | 8,50 | 0,32 |  
R  
R  | 3,00 | 1,59 | ..  
R  | 9,00 | 0,25 |  
R  
R  | 3,50 | 1,49 | ..  
R  | 9,50 | 0,19 |  
R 
 F EEFF : ALL  『E  Page 61972-23-00 
 E  E  Aug 01/05 
 E  E 
 ECES  E
 F 『 E C F M E E E E 56-5B E
R  Fan Inlet Case on B1 upstream bracket location Figure 604/TASK 72-23-00-991-328 
 F EEFF : E E ECES  ALL  『E 72-23-00EEE Page 620 May 01/05
 F 『
 E C F M E
 E E
 E 56-5B E
 E E
 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
R  | 4,00 | 1,35 | ..  
R  | 10,0 | 0,14 |  
R  
R  | 4,50 | 1,19 | ..  
R  | 10,5 | 0,10 |  
R  
R  | 5,00 | 1,04 | ..  
R  | 11,0 | 0,10 |  
R  
R  | 5,50 | 0,91 | ..  
R  | 11,5 | 0,10 |  
R  
R  | 6,00 | 0,79 | ..  
R  | 12,0 | 0,10 |  
R 
 4. Fan rotor blades for: 
 (Ref. Fig. 605/TASK 
 72-23-00-991-325, 
 606/TASK 72-23-00- 
991-326) 
 A. Cracks or tears 
 (1) Operational  
cracks  
(2) FOD caused  
cracks or  
tears. 
F  『 
 EEFF :  ALL  E  
E  E 
 E  E 
 ECES  E
Not serviceable. 
Not serviceable. 
Replace pair of matchedblades (Ref. TASK 72-21-00-300-028)
Do blending procedure(Ref. TASK 72-21-00-320-003) until all indications are removed. Do a spot fluorescent-penetrant inspection to make sure that all indications are removed (Ref. TASK 70-51-00-230-002). Remove 0.010 in. (0.25 mm) additional material. Total blend must agree with the max repair limits as defined in figure
72-23-00Page 621 
Aug 01/05
F 『 E C F M E E E E 56-5B E
R  Fan Rotor Blades - Blend Limits Figure 605/TASK 72-23-00-991-325 
 F EEFF : E E ECES  ALL  『E 72-23-00EEE Page 622 May 01/05
 F  『 
 E  C F M  E 
 E  E 
 E  56-5B  E 
 E  E
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM ENGINE 发动机 1(142)