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7 - Shim 8 - Ruler 9 - Clinometer 10 - Shim 11 - Input rod 12 - "Nose down" stop (elevator) 13 - "Nose up" stop (elevator) 14 - Support assembly ® Pitch control - Travel adjustment Figure 201 - Without travel jiq ABAA Validity : S / N 1 - 9999 27 30-00Page 203 (CA) MAR 00 1 - Control wheel tube 2 - "Nose up" stop (wheel) 3 - Guide 4 - "Nose down" stop (wheel) 5 - Control wheel 6 - Travel jig 7 - Attachment pin 8 - Rigging pin 9 - Pin 10 - Knurled nut 11 - Knurled nut 12 - "Nose up" mark 13 - TB20 index 14 - "Nose down" mark 15 - Graduated section 16 - "Nose up" stop (elevator) 17 - "Nose down" stop (elevator) 18 - Support assembly Pitch control - Travel adjustment Key to Figure 201A - With travel jig SOCATA MAINTENANCE MANUAL TB 20 MODEL Pitch control - Travel adjustment Figure 201A - With travel jig ABAA Validity : S / N 1 - 9999 27-30-00Page 205 (CA) MAR 00 17) Remove travel jig (6). 18) Make sure all the tools and materials are removed and the work area is clean and free from debris. 19) Install inspection doors 211L and 211R (if installed) or reposition and lock the instrument panel, then install the covers. 20) Install the sheath clip securing rear light wiring. 21) Install tail cone 222 - refer to 53-20-00. 4. INSPECTION / CHECK - PITCH CONTROL A. Tools and consumable materials - Ruler 5.9 ft (180 cm) - Clamps - Dial gage - Cleaning agent (TB 11-002) - Clean lintfree cloths - Inside micrometer - Palmer - Grease (TB 04-004A) B. Preliminary steps 1) Make sure that the main switch-breaker is open. 2) Install the warning sign prohibiting main switch-breaker operation. WARNING DO NOT OPERATE MAINTENANCE WORK IN PROGRESS 3) Remove the cowling under hull 218. 4) Remove tail cone 222 - refer to 53-20-00. 5) Open baggage compartment door 219 and remove baggage compartment bottom door 242. 6) Remove inspection doors 211L and 211R (if installed). Otherwise, remove the covers forward of the instrument panel and tilt the latter. 7) Remove inspection doors 235L and 235R. C. Check of elevator control (Figure 202) 1) Inspect control wheel assembly for : - slack and friction points in pitch control, - security of "Nose up" (1) and "Nose down" (2) stops. ABAA Validity : S / N 1 - 9999 27-30-00Page 206 (CA) SEP 04 2) Inspect rods (3) for : 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址：TB20 MAINTENANCE MANUAL 27 FLIGHT CONTROLS TB20飞机维护手册 飞行操纵(31) |
