A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 19_部分9.pdf350页

4. Procedure _________ **ON A/C 001-001, 051-052, (Ref. Fig. 401/TASK 28-42-16-991-001) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Post SB 28-1077 For A/C 001-001,051-052,

(Ref. Fig. 401A/TASK 28-42-16-991-001-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Subtask 28-42-16-420-052 A. Preparation for Installation (1) Clean the component interface and the adjacent areas with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026). (2) Do an inspection of the component interface and/or the adjacent area. (3) Make sure that the parts retained from the removed component are clean and in the correct condition. Subtask 28-42-16-560-050 B. Preparation of a Replacement Component (Ref. Fig. 402/TASK 28-42-16-991-003) (1) Remove the transport pin (10) from the cadensicon (1) if installed. ____ NOTE : The transport pin (10) is only installed on cadensicon part number 796-809-6A. Cadensicon part numbers 796-809-5 and 796-809-6 do not have a transport pin installed.

R

EFF : 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, CES

28-42-16

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