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18) Retain upper half-bearings (1) ; leave bolts (11) in position. C. Installation of rudder pedals (Figures 201 and 202) 1) Lubricate bolts and hinge bolts with grease (TB 04-004A). 2) Position and tape upper half-bearings (1) on bolts (11). Use adhesive tape (TB 08-919A). 3) Position the front and rear rudder pedals through the pylon. 4) While holding the rudder pedals on upper half-bearings (1), install lower half-bearings (1). 5) Secure the half-bearings with washers (3) (or retaining plate) and new nuts (2). 6) Secure the engine controls with clamp (10), washer (9) and a blind rivet (8). 7) Secure the engine controls with clamp (12), bolt (13), washer (14) and new nut (15). 8) Install the Alternate Air control - refer to 76-10-02. 9) Secure lever (7) to the rear rudder pedal tube with bolts (4), washers (5) and new nuts (6). 10) Secure interconnection rods (19) to the rudder pedals with shouldered washers (16) (observe the mounting direction) and nuts (17) ; safety with new cotter pins (18). 11) Secure brake rods (22) at L.H. station pedals with washers (20) and new cotter pins (21). 12) If removed, secure R.H. station master cylinders to their support. NOTE : Ensure a 0.39 in to 0.78 in (1 to 2 mm) clearance between piston rod and control lever roller. 13) If interconnection rods (19) and / or (33) have been removed during rudder pedal removal, observe the mounting direction of bolts (31) and (32) - see Figure 202, Detail B. 14) Check the alignment of the rudder pedals - refer to Paragraph 4. - and the rudder - refer to 27-20-00. 15) Make sure all the tools and materials are removed and the work area is clean and free from debris. 16) Connect the leads to ground terminal block GS 23 (R.H. side). 17) Raise R.H. and L.H. instrument panels and install the visors. 18) If removed, install the transponder and / or the ADF receiver - refer to 34-50-00. 19) Connect the battery - refer to 24-30-02. 20) Install inspection doors 211L and 211R (if installed) and 235L and 235R. 21) Install the front seats - refer to 25-11-00. 22) Remove the warning sign prohibiting main switch-breaker operation. 23) If the R.H. station is equipped with master cylinders, test the brakes while taxiing. ACAA Validity : S / N 1 - 9999 27 20-01 Page 202 (DA) MAR 00 1 - Half-bearing 2 - Nut 3 - Washer 4 - Bolt 5 - Washer 6 - Nut 7 - Lever 8 - Blind rivet 9 - Washer 10 - Clamp 11 - Bolt 12 - Clamp 13 - Bolt 14 - Washer 15 - Nut 16 - Shouldered washer 17 - Nut 18 - Cotter pin 19 - Interconnection rod 20 - Washer 21 - Cotter pin 22 - Brake rod 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(22) |
