|
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
g) Replace the defective components or contact the manufacturer for repair. h) Install control wheels, upper rods (12) and (14) and pylon assy - refer to 27-30-02. 6) If control wheel-to-aileron slack is out-of-tolerance, perform the following operations : a) Perform steps 4) and 5). b) Remove lower rod (23) and measure the slack of ball joints : max. permissible slack value, 0.003 in (0.08 mm) per ball joint. Replace if necessary. c) If lower rod (23) is within the tolerances, remove torque rod (18) and measure the slack of the gimbal joint : max. permissible slack value, 0.0078 in (0.2 mm) around the gimbal joint. Replace if necessary. D. Check of roll control in fuselage (Figures 203 and 204) 1) Inspect the control wheel assembly for : - slack and friction points in roll control. 2) Inspect the pylon assembly for : - cracks, distortions and corrosion, - binding, slack and wear of the bearings, ball joints and gimbal joints, - correct tightening of the attachment nuts of intermediate levers (13) and (17) and lower levers (20) and (22), WA Validity : S / N 1 - 9999 27 10 00Page 207 (BA) SEP 04 - correct tightening of nuts (16) attaching the gimbal joints to control wheel tubes, - correct tightening of nut (19) attaching the gimbal joint to torque rod (18), - cracks and slack on the taper pins attaching gimbal joints to upper levers (15), - cracks and slack on the taper pin attaching the lower gimbal joint, - correct safetying of the attachment nuts of upper rods (12) and (14) and lower rod (23) with cotter pins, - correct safetying of attachment nuts (21) of lower levers (20) with cotter pins, - correct safetying of nuts (11) attaching control wheel tube assemblies to the pylon with cotter pins. 3) Inspect torque rod (18) for : - cracks, buckling and corrosion, - cracks and distortions on attachment plate (33), - correct tightening of nuts (32) attaching lever (34) to attachment plate (33), - correct tightening of attachment nuts (35) of half-bearings (31), - binding, slack and wear of the ball joints of lever (34), - excessive slack [higher than 0.02 in (0.5 mm)] between torque rod (18) and half-bearings (31), - correct tightening of the attachment nuts of adjustable stops (36) and condition of the attachment rivet, - cracks and distortions on the contact surface between lever (34) and adjustable stops (36). NOTE : If the roll / yaw interconnection system is installed (TB 200 Std, TB 9 and TB 10 Opt), refer to chapter 27-20-02. E. Check of roll control in wings (Figures 205 and 206) 1) Inspect rods (41) and (43) for : - cracks, buckling and corrosion, - correct safetying of nuts (42) of attachment bolts with cotter pins. 2) Inspect bellcranks (45) 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(13) |
