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26) Install new tie-wraps to attach control (7). NOTE : If necessary, put protection tape (TB 05-938) on engine mount and landing gear mount before installing the tie-wraps. 27) Apply sealant (TB 09-904) to grommet (20) to seal the passage of control sheaths in the firewall. 28) Lubricate control (7) - refer to 12-21-01. 29) Make sure all the tools and materials are removed and the work area is clean and free from debris. 30) Install inspection doors 211L and 235R. 31) Install the engine cowlings - refer to 71-10-01. 32) Perform a test run-up - refer to 05-30-02. Perform a propeller regulation test and adjust the governor if necessary - refer to 61-20-01. ACAA Validity : S / N 1 - 9999 61-20-02Page 403 (EA) JUN 02 1 - Control lever 2 - Fork end 3 - Clevis pin 4 - Washer 5 - Cotter pin 6 - Jam nut 7 - Control 8 - Nut 9 - Lockwasher 10 - Pedestal bulkhead 11 - Lockwasher 12 - Nut 13 - Nut 14 - Washer 15 - Bolt 16 - Clamp 17 - Clamp 18 - Blind rivet 19 - Washer 20 - Grommet 21 - Sealant 22 - Nut 23 - Bracket 24 - Nut 25 - Protective sleeve 26 - Swivel rod end 27 - Lever 28 - Jam nut 29 - Boot 30 - Washer 31 - Bolt 32 - Washer 33 - Washer 34 - Nut 35 - Inspection hole Propeller governor control — Removal / Installation Key to Figure 401 ACAA Validity : S / N 1 - 9999 61-20-02 Page 404 (EA) JUN 02 ACAA Validity : S / N 1 - 9999 61-20-02Page 405 (EA) JUN 02 PAGE INTENTIONALLY LEFT BLANK ACAA Validity : S / N 1 - 9999 61-20 02Page 406 (EA) JUN 02 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址：TB20 MAINTENANCE MANUAL 61 螺旋桨 TB20飞机维护手册(25) |
