|
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
8) Connect actuating cylinder (24) to locking bar (10) with screw (23), washer (22) and new locknut (21). 9) Lubricate the hinged strut (9) - refer to 12-21-05. 10) Connect microswitch connector to landing gear mount. WARNING : BEFORE ANY LANDING GEAR RETRACTION OR "NORMAL" OR "EMERGENCY" EXTENSION PROCEDURE, AND / OR LANDING GEAR CIRCUIT-BREAKER CLOSING, MAKE SURE THAT THE LANDING GEAR IMMEDIATE SURROUNDINGS ARE CLEAR (PERSONS OR THINGS). 11) Check landing gear control linkage and indicating system - refer to 32-30-00. 12) Lower the aircraft to ground and remove the jacks - refer to 07-10-00. 13) Install the engine cowlings - refer to 71-10-01. 3. ADJUSTMENT / TEST None 1 - Hook Hinged strut - Manual unlocking Figure 201 AAAA Validity : S / N 1 - 9999 32-30 Page 203 04 (BA) JUN 01 1 - Nut 2 - Washer 3 - Bolt 4 - Cotter pin 5 - Compensating lever 6 - Washer 7 - Cotter pin 8 - Compensating actuator 9 - Hinged strut 10 - Locking bar 11 - Bolt 12 - Washer 13 - Nut 14 - Cotter pin 15 - Front section of hinged strut 16 - Screw 17 - Washer 18 - Nut 19 - Cotter pin 20 - Landing gear leg 21 - Locknut 22 - Washer 23 - Screw 24 - Actuating cylinder Nose landing gear hinged strut - Removal / Installation Key to Figure 202 WA Validity : S / N 1 - 9999 32 30 04 Page 204 (BA) JUN 01 WA Validity : S / N 1 - 9999 Nose landing gear hinged strut - Removal / Installation Figure 202 32-30 04 (BA) JUN 0 Page 205 4. INSPECTION / CHECK - NOSE LANDING GEAR HINGED STRUT A. Tools and consumable materials - Specific material - Common material : 1 surface plate 4 identical supports or vees 1 depth gage 1 set of thickness gages 1 Geneva file Abrasive cloth (TB 05-916B) B. Check method of the nose landing gear hinged strut (Figures 203 and 204) 1) Remove the equipped strut - refer to Paragraph 2. Check and change, if necessary, hinge bolts (G) and (J) and the spacers at the attachment on the mount. 2) Place the four supports or vees (6) onto the surface plate (7). 3) Check with the depth gage the "a" dimensions. Adjust if necessary between the supports and the surface plate with thickness gages. 4) Unlock the hinged strut - refer to Paragraph 1. 5) Remove the hinge bolt (H) of front half-leg and of rear fork. Check bolt condition, change it if necessary. 6) Install at its place the dia. .39 in (10 mm) smooth pin (3). 7) Lock the hinged strut. 8) Place the second dia. .39 in (10 mm) smooth pin (1) onto the front half-leg and the smooth pin (5) onto the rear fork. Make sure of its correct positioning. 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址：TB20 MAINTENANCE MANUAL 32 起落架 TB20飞机维护手册(63) |
