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3) Connect the battery - refer to 24-30-02. 4) Check the flap travels and indicating - refer to 27-50-00. ADAC Validity : S / N 1 - 9999 27-50 02Page 403 (EA) MAR 00 1 - Screw 2 - Protective device 3 - Dust-proof plate 4 - Nut 5 - Washer 6 - Bolt 7 - Rotary switch 8 - Tab 9 - Pad 10 - Bolt 11 - Washer 12 - Connector 13 - Washer 14 - Nut 15 - Screw 16 - Selector 17 - Nut 18 - Grommet 19 - Lower assembly Wing flap control - Removal / Installation Key to Figure 201 - S / N 1 - 547, 553 - 579 Pre-Kit OPT10 911600 ADAC Validity : S / N 1 - 9999 27 50 02 (EA> Page 404 MAR 00 Wing flap control - Removal / Installation Figure 201 - S / N 1 - 547. 553 - 579 Pre-Kit OPT10 911600 1 - Plate 2 - Hole 3 - 0-ring 4 - Screw 5 - Bracket 6 - Protective device 7 - Grommet 8 - Bolt 9 - Tab washer 10 - Bracket 11 - Wire 12 - Shunt 13 - Inverter 14 - Inverter 15 - Sealed nut 16 - Nut 17 - Selector assembly Wing flap control - Removal / Installation Key to Figure 201A - S / N 548 - 552, 580 - 9999 and S / N 1 - 547, 553 - 579 Post-Kit OPT10 911600 ADAC Validity : S / N 1 - 9999 27 50 02 (EA> Page 406 MAR 00 Wing flap control - Removal / Installation Figure 201A - S / N 548 - 552, 580 - 9999 and S / N 1 - 547, 553 - 579 Post-Kit OPT10 911600 ADAC Validity : S / N 1 - 9999 27-50-02Page 407 (EA) MAR 00 PAGE INTENTIONALLY LEFT BLANK ADAC Validity : S / N 1 - 9999 27 50-02Page 408 (EA) MAR 00 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(71) |
