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10) Position the central attachment spacers against the tunnel front face. 11) Measure the gap between spacers (4) and the tunnel rear face. 12) Install suitable shims (3) - refer to Table, Figure 401 (2/2). 13) Install washers (1) and bolts (2). Post-MOD. 167 14) Measure the dimension between the tunnel and bolt (2). 15) Install thrust washer (7) according to the recommended assembly - refer to Table, Figure 401 (2/2). S / N 1 - 9999 16) Install washers (5) and new locknuts (6). Torque - refer to 20-00-01. 17) Measure the gaps on front fittings (frame C1). 18) Install suitable shims (10) - refer to Table, Figure 401 (2/2). 19) Install bolts (11), washers (9) and new locknuts (8). Torque - refer to 20-00-01. ADAA Validity : S / N 1 - 9999 57 00-00Page 403 (EA) JUN 02 20) Install bolts (12), washers (13) and new locknuts (14). Torque - refer to 20-00-01. 21) Remove the two padded supports under the wings and the hoisting device. 22) Connect the flap control rods to the main bellcrank - refer to 27-50-00, install new cotter pins. 23) Remove the blanking plugs. Connect the main landing gear actuator hoses - refer to 20-00-02. 24) Replenish the landing gear hydraulic system - refer to 12-13-03. 25) Connect the wing electrical circuits at wing / fuselage junction. 26) Connect the dynamic system and install the three-way union of the static system. 27) Remove the blanking plugs. Connect the high and low pressure hoses of the air conditioning system, if installed - refer to 20-00-02. 28) If installed, replenish the air conditioning system - refer to 12-15-01. 29) Connect the aileron control rods to the lever. Install new cotter pins. 30) Remove the blanking plugs. Connect the fuel system at wing / fuselage junction - refer to 20-00-02. 31) Remove the blanking plugs. Connect the brake system at wing / fuselage junction — refer to 20-00-02. 32) Replenish then bleed the brake hydraulic system - refer to 12-13-01. 33) Replenish the fuel tanks - refer to 12-11-01, and check the fuel supply for correct operation - refer to 28-20-01. 34) Check hydraulic unions and fuel unions for leaks. 35) Mark with a red paint line the hydraulic unions, the fuel unions and the bolts and nuts securing the wings to the fuselage. 36) Inspect the anti-skid coating for condition, replace if necessary - refer to Page 301. 37) Install front and rear bulkheads of the wheel housings. Pre-MOD. 151 38) Make sure all the tools and materials are removed and the work area is clean and free from debris. 39) Check the landing gears for correct operation (Normal - Emergency) - refer to 32-30-00. 40) Check the roll control linkage for correct operation - refer to 27-10-00. 41) Install the front junction fairings and the cowlings under hull. 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(8) |
