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21 20 Rudder pedals - Removal / Installation Figure 201 ACAA Validity : S / N 1 - 9999 27 20 01Page 203 (DA) MAR 00 Interconnection rod - Removal / Installation Figure 202 ACAA Validity : S / N 1 - 9999 27 20-01Page 204 (DA) MAR 00 3. ADJUSTMENT / TEST None 4. INSPECTION / CHECK - RUDDER PEDALS A. Tools and consumable materials None B. Check of rudder pedals (Figure 203) The installation of the rudder pedals must be followed by a check of their alignment and a systematic check of nose wheel alignment and rudder adjustment. Table AV Front table a) :12 --- . acu 0_ as o cu ' c (i) 4.. ,... cy (ir IT ii c- -,,, cyp, 5 -2 S' (, (2 0 ci / / c-- cz) -0 cei ii-ry cig) / (Z / ,z... Plancher Floor 300 mm 11.8 in Rudder pedals - Inspection / Check Figure 203 PAGE INTENTIONALLY LEFT BLANK ACAA Validity : S / N 1 - 9999 27 20 01 (DA) Page MAR 00 206 RUDDER TRIM TAB CONTROL MAINTENANCE PRACTICES 1. SERVICING None 2. REMOVAL / INSTALLATION - RUDDER TRIM TAB CONTROL A. Tools and consumable materials - Grease (TB 04-004A) - Oil (TB 03-900A) - Stainless steel lockwire, dia. 0.02 in (0.6 mm) - Adhesive tape (TB 08-917) B. Removal of rudder trim tab control (Figure 201) 1) Remove the pedestal - refer to 25-14-00. 2) Remove the tunnel - refer to 25-15-00. 3) Remove screws (43), inspection door 312 (42). 4) Remove and discard cotter pin (41). 5) Remove nut (40), washer (39) and bolt (36). 6) Loosen jam nut (29) and clear control rear section (32) from support (25). 7) Partially loosen nut (16) from clamp (13) at frame C5. NOTE : Clamp (13) secured to battery tray support (14) cannot be accessed easily and should not be removed. 8) Remove and discard nuts (22). 9) Remove washers (23), bolts (2), stop (3) and both washers under stop (3). 10) Make sure the control is clear all over its length and that no element is secured on it. 11) Disengage bolt assy (6) from support (4) ; remove retaining ring (20) and washer (19) and remove bolt assy (6). NOTE : To remove retaining ring (20), the control must be pulled forward or backward depending on support (4) type. 12) Unscrew rack (8) from flexible control assy (10). 13) Loosen nut (9) and while unscrewing nut (18), clear housing (7) from flexible control assy (10) ; remove nut (9). 14) Attach lockwire (19.7 ft (6 m) approximately) to control end on pedestal side. 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(23) |
