(30) Put the landing (20) in position. (31) Install the bolts (35) and the nuts (21) (Ref. SRM 514211). (32) Apply SEALANTS (Material No. 09-001) to the mating faces of the landing (22) and the aircraft structure. (33) Put the landing (22) in position and install the bolts (24) and the nuts (23) (Ref. SRM 514211). (34) Apply SEALANTS (Material No. 09-001) to the mating faces of the landing (25) and the aircraft structure. (35) Put the landing (25) in position. (36) Install the bolts (27) and the nuts (26) (Ref. SRM 514211). (37) Examine the seals (140) around the pressure-relief panels (9) and (30) for damage and correct condition. Replace damaged seals as follows: (Ref. Fig. 806/TASK 57-41-37-991-014) (a) Remove the damaged length of seal (140) with a non-metallic scraper. (b) Clean the applicable area of the panel with a lint-free cloth made moist with CLEANING AGENTS (Material No. 11-026). R (c) Cut to length a new seal (140). (d) Put the new seal (140) in position on the panel. (e) Cut the corners of the new seal (140) to make a continuous surface at the corner joints. (f) Remove the protective back from the new seal (140) and install the seal on the panel. (g) Use a suitable cutting tool to remove the seal from the holes X. The diameter of the hole X is between 5.75 mm (0.2263 in.) and 6.25 mm (0.2460 in.). (38) Make sure that the work area is clean and clear of tool(s) and other items. (39) Apply release agent, SPECIAL MATERIALS (Material No. 05-064) to the trailing edge of the pressure-relief panel (9).
R
EFF : 106-149, 157-199, 209-299, 301-399, 401-499, CES
57-41-37
Page 840 Aug 01/05
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4.pdf
R
EFF : 106-149, 157-199, 209-299, 301-399, 401-499, CES
57-41-37
Page 840 Aug 01/05
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4.pdf
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