(3) Remove the spinner rear cone (Ref. TASK 72-21-00-000-006).

 (4) Record location of each blade to be replaced and of each blade opposite.

 (5) Remove fan blades (Ref. TASK 72-21-00-000-007)

 (6) Write moment weight on base of blades that you remove using temporary marking (Material No. CP5061). (Ref. Fig. 407/TASK 72-21-00-991-341)

 NOTE : Grease deposits can mask the moment weight indication. If
____
R necessary, clean blade base with isopropyl alcohol (Material
R No. CP1041) or acetone (Material No. CP1039) or stoddard
R solvent (Material No. CP2011) or ardrox 552 (Material No.
R CP2559) or turco ind 79 (Material No. CP2560) or mag-chem
R teksol (Material No. CP2566) or degreasol 99 R (Material No.
R CP2584) or mag-chem skysol (Material No. CP2656).
 F 『 EEFF : ALL E Page 42872-21-00
 E E May 01/05 E E ECES E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E

R R  Diagram for Fan Blade Change Figure 406/TASK 72-21-00-991-327
 F EEFF : E E ECES  ALL  『E 72-21-00EEE Page 429 Nov 01/98

R R  Fan Blade Replacement Figure 407/TASK 72-21-00-991-341
 F EEFF : E E ECES  ALL  『E 72-21-00EEE Page 430 Nov 01/98

R R  Replacement of Several Pairs of Fan Blades Figure 408/TASK 72-21-00-991-342
 F EEFF : E E ECES  ALL  『E 72-21-00EEE Page 431 Nov 01/98

R Fan Blades, Balance Screw Location Chart and Vectorial Diagram R Figure 409/TASK 72-21-00-991-343
 F 『 EEFF : ALL E Page 43272-21-00
 E E Nov 01/98 E E ECES E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

 INTENTIONALLY BLANK

 F 『 E E Page 43372-21-00
 E E Nov 01/98 E E ECES E F 『 E C F M E E E E 56-5B E

R Various Balance Screw Arrangements for Given Moment Weights R Figure 410/TASK 72-21-00-991-344- 12 (SHEET 1)
 F 『 EEFF : ALL E Page 43472-21-00
 E E Nov 01/98 E E ECES E F 『 E C F M E E E E 56-5B E

R Various Balance Screw Arrangements for Given Moment Weights R Figure 410/TASK 72-21-00-991-344- 22 (SHEET 2)
 F 『 EEFF : ALL E Page 43572-21-00
 E E Nov 01/98 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E
 Subtask 72-21-00-420-081

 B. Record moment weight on base of spare blades.
 CAUTION : FOR EACH PAIR OF FAN BLADES, INSTALL THE HEAVIER SPARE BLADE AT
_______ THE POSITION OF THE HEAVIER BLADE TO BE REMOVED.
R (1) Write the moment weight on base of the spare blades with temporary R marking (Material No. CP5061).
 (2) Install spare blades (Ref. TASK 72-21-00-400-007).
 Subtask 72-21-00-820-053
 C. Determine the balance screws to be installed.
 (1) Determine the resultant vector length and direction, then select balance screws to provide a correction returning the fan to its initial balance condition as follows.
 NOTE : It is advisable to limit the number of balance screws on the
____ spinner due the complexity and the risk of confusion when performing further corrections, and to install only one set of balance screws. This requires the construction of a vector diagram for determining the sum of the corrections. An example is given in (Ref. TASK 72-21-00-300-009).
 (a) Assume the following blades with the moment weights indicated are to be removed: No. 01: 164832 cm.g (64894 in.g) No. 36: 163245 cm.g (64270 in.g) No. 03: 162510 cm.g (63980 in.g) No. 35: 164185 cm.g (64640 in.g)

 (b) Assume the moment weights of the opposite blades are as follows: No. 19: 164647 cm.g (64823 in.g) No. 18: 163405 cm.g (64333 in.g) No. 21: 162650 cm.g (64035 in.g) No. 17: 164160 cm.g (64630 in.g)

 (c) Calculate differences between moment weights as below: D1: (No. 01/19) = 164832 - 164647 = 185 cm.g (73 in.g) D2: (No. 18/36) = 163405 - 163245 = 160 cm.g (63 in.g) D3: (No. 21/03) = 162650 - 162510 = 140 cm.g (55 in.g) D4: (No. 35/17) = 164185 - 164160 = 025 cm.g (10 in.g)

 F 『 EEFF : ALL E Page 43672-21-00
 E E Feb 01/00 E E ECES E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E 

R (d) Calculate moment weight differences corresponding to spare fan
R blades as below:
R D'1: (No. 01/19) = 162905 - 162730 = 175 cm.g (69 in.g)
R D'2: (No. 18/36) = 161205 - 161185 = 020 cm.g (08 in.g)
R D'3: (No. 21/03) = 164570 - 164545 = 025 cm.g (10 in.g)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM ENGINE 發動機 1(89)