|
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
(BA) SEP 04 B. Procedure 1) Apply a very thin coat of petrolatum (TB 04-012) to the bearing face of arm assemblies (1) and (5). 2) Apply sealant (TB 09-916) to the bearing face of arm assemblies (1) and (5) and to bolts (2) - refer to 20-00-09. 3) Position arm assemblies (1) and (5) and secure them with bolts (2), washers (3) and new nuts (4). 4) Wipe off excess sealant with a clean lintfree cloth moistened with cleaning agent (TB 11-003). 5) Connect the external gage connector and the electrical wiring of the heated pitot tube, if installed. 6) Make sure all the tools and materials are removed and the work area is clean and free from debris. 7) Install the inspection doors 512 [612] and 516 [616] - refer to 52-40-00. 8) Install the flaps - refer to 57-50-00. 3. REMOVAL OF THE ARMS FITTED WITH AILERONS (Figure 401) A. Tools and consumable materials - Cleaning agent (TB 11-003) - Spatula - Clean linffree cloths B. Procedure 1) Remove the ailerons - refer to 57-60-00. 2) Remove the inspection door 516 [616] - refer to 52-40-00. 3) Remove the wing tip - refer to 57-30-00. 4) Disconnect the electrical wiring of stall warning device - refer to 27-30-04. 5) Remove harness holding clips (8) and clear electrical harness (9) to gain access to the work area. 6) Unrivet and remove coverplate (7) - refer to 51-40-02. 7) Check the type of attachment of the arm assemblies (with rivets or bolts). Attachment with rivets 8) Remove the rivets carefully - refer to 51-40-02. 9) Remove arm assemblies (6) and (10). 10) Apply a protection treatment to the sections bared during removal - refer to 20-00-04. NOTE : During installation, replace the rivets with bolts, washers and nuts - refer to the Illustrated Parts Catalog. Attachment with bolts 8) Remove and discard nuts (13), remove washers (12) and bolts (11). 9) Disengage and remove arm assemblies (6) and (10). 10) Remove the sealant with a spatula and clean the surfaces with a clean lintiree cloth moistened with cleaning agent (TB 11-003). AAAA Validity : S / N 1 - 9999 57 20-00Page 402 (BA) SEP 04 4. INSTALLATION OF THE ARMS FITTED WITH AILERONS (Figure 401) A. Tools and consumable materials - Sealant (TB 09-916) - Petrolatum (TB 04-012) - Cleaning agent (TB 11-003) - Clean lintfree cloths - Rivets P / N Z00.N5536342404 - Rivets P / N Z00.N5553368406 B. Procedure 1) Apply a very thin coat of petrolatum (TB 04-012) to the bearing face of arm assemblies (6) and (10). 2) Apply sealant (TB 09-916) to the bearing face of arm assemblies (6) and (10) and to bolts (11) - refer to 20-00-09. 3) Position arm assemblies (6) and (10) and secure them with bolts (11), washers (12) and new nuts (13). 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址：TB20 MAINTENANCE MANUAL 57 机翼 TB20飞机维护手册(25) |
