R R R R R R R R R R R R R R R R R R R R R R R R R R R R R
Subtask 57-52-00-210-059 B. Detailed Visual Inspection of Inboard Double Slotted Flap, Trunnion Attachment Bracket, LH/RH. (1) Do an inspection of the external surface of the trunnion attachment bracket and the inboard trunnion, where it can be seen. Make sure that: - there is no damage - there is no corrosion - there are no cracks or scores - the surface protection is in the correct condition. ____ NOTE : If necessary, refer to the ASRM (Ref. ASRM 575200) for the correct repair procedure. 5. Close-up ________ Subtask 57-52-00-410-066 A. Close Access (1) Remove the spark-proof lamp from the inspection area. (2) Make sure that the work area is clean and clear of tool(s) and other items. (3) Install the inboard flap seals (Ref. TASK 27-54-61-400-007). (4) Install the applicable access panel: - for the left wing, install 581AT - for the right wing, install 681AT. Subtask 57-52-00-865-085 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV. Subtask 57-52-00-860-051 C. Aircraft Maintenance Configuration (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009).
R
EFF : CES
301-399,
57-52-00
Page 693 May 01/04
飞行翻译公司 www.aviation.cn 本文链接地址：A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 37_部分6.pdf
Subtask 57-52-00-210-059 B. Detailed Visual Inspection of Inboard Double Slotted Flap, Trunnion Attachment Bracket, LH/RH. (1) Do an inspection of the external surface of the trunnion attachment bracket and the inboard trunnion, where it can be seen. Make sure that: - there is no damage - there is no corrosion - there are no cracks or scores - the surface protection is in the correct condition. ____ NOTE : If necessary, refer to the ASRM (Ref. ASRM 575200) for the correct repair procedure. 5. Close-up ________ Subtask 57-52-00-410-066 A. Close Access (1) Remove the spark-proof lamp from the inspection area. (2) Make sure that the work area is clean and clear of tool(s) and other items. (3) Install the inboard flap seals (Ref. TASK 27-54-61-400-007). (4) Install the applicable access panel: - for the left wing, install 581AT - for the right wing, install 681AT. Subtask 57-52-00-865-085 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV. Subtask 57-52-00-860-051 C. Aircraft Maintenance Configuration (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009).
R
EFF : CES
301-399,
57-52-00
Page 693 May 01/04
飞行翻译公司 www.aviation.cn 本文链接地址：A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 37_部分6.pdf
自定义标签： 
