Subtask 27-54-52-865-052 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV Subtask 27-54-52-710-050 E. Test (1) Do the operational test of the flap system (Ref. TASK 27-54-00-710001). (2) Make sure that there are no leaks and that no fluid comes out of the seal drain line (10). 5. Close-up ________ Subtask 27-54-52-860-053 A. Put the aircraft back to the serviceable condition. (1) Make sure that the level of the fluid in the relevant hydraulic reservoir is correct. Add fluid as necessary (Ref. TASK 12-12-29-611001) or (Ref. TASK 12-12-29-611-002). (2) Remove the container from below the PCU (1). (3) Remove the access platform(s). Subtask 27-54-52-410-050 B. Close the main doors of the main gear (Ref. TASK 32-12-00-410-001).
EFF : CES
ALL
27-54-52
Page 416 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 18_部分10.pdf
EFF : CES
ALL
27-54-52
Page 416 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 18_部分10.pdf
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