|
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
3) Position lower assembly (19) in the pedestal and connect connector (12). 4) Install dust-proof plate (3), protective device (2) and screws (1). 5) Install flap indicator. 6) Make sure all the tools and materials are removed and the work area is clean and free from debris. 7) Install the side pedestal covers - refer to 25-14-00. 8) Connect the battery - refer to 24-30-02. 9) Check the flap travels and indicating - refer to 27-50-00. S / N 548 - 552, 580 - 9999 and S / N 1 - 547. 553 - 579 Post-Kit OPT10 911600 D. Removal of wing flap control (Figure 201A) 1) Disconnect the battery - refer to 24-30-02. 2) Remove screws (4) and clear selector assembly (17). 3) Disconnect and tape the wire outside the pedestal with adhesive tape (TB 08-919A). Remove selector assembly (17). 4) If necessary, disassemble selector assembly (17). a) Remove bolts (8) and grommets (7). b) Remove plate (1) and 0-ring (3). c) Mark inverter (13) or (14) direction in relation to bracket (10). Pre-MOD. 143 (Detail B) d) Mark wires (11) on inverter (13) tabs and disconnect them. Post-MOD. 143 (Detail C) d) Mark wires (11) on inverter (14) tabs and disconnect them. e) If inverter (14) has to be replaced, remove shunt (12). All f) Remove nut (16) or sealed nut (15), bracket (5), protective device (6), tab washer (9) and bracket (10) from inverter (13) or (14). ADAC Validity : S / N 1 - 9999 27 50 02Page 402 (EA) MAR 00 E. Installation of wing flap control (Figure 201A) 1) If disassembled, reassemble selector assembly (17). a) Lubricate inverter (13) or (14) lever and bolt (8) smooth section with petrolatum (TB 04-012). b) Check condition of components. Replace if necessary. c) Engage inverter (13) or (14), as identified during removal, on bracket (10). d) Install tab washer (9), protective device (6) and bracket (5). NOTE : Make sure the washer tab is correctly seated in protective device (6) hole. e) Coat inverter (13) or (14) thread, plate (1) holes (2) with loctite (TB 08-013). CAUTION : CORRECTLY SUPERIMPOSE THE TRAVEL PLANES OF INVERTER LEVER AND PLATE (1) TO PRECLUDE STRESS. THE PLATE / LEVER ASSEMBLY MUST MOVE FREELY WITHOUT INTERFERING WITH PROTECTIVE DEVICE WALLS. f) Install nut (16) or sealed nut (15), 0-ring (3) (check condition, replace if necessary) and plate (1). g) Install grommets (7) and bolts (8). h) Make sure inverter (13) or (14), protective device (6) and plate (1) are correctly aligned without stress or friction. i) Connect wires (11), as identified during removal, on inverter (13) or (14). Post-MOD. 143 (Detail C) j) If inverter (14) has been replaced, install shunt (12). All 2) Connect and secure selector assembly (17) with screws (4). 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(70) |
