在线看免费❗_美女网站黄www._.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
0 '7 LIFTING AND SHORING
LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE CHAPTER 07-LEP (EA) 1 JUN 01 2 JUN 01 07-TC (EA) 1 JUN 01 2 JUN 01 07-00-00 (CA) 1 JUN 01 2 JUN 01 07-10-00 (CA) 201 JUN 01 202 JUN 01 07-20-00 (CA) 201 JUN 01 202 JUN 01 203 JUN 01 204 JUN 01
ADAA Validity : S / N 1 - 9999 07 LEP(EA) Page 1 JUN 01 PAGE INTENTIONALLY LEFT BLANK ADAA Validity : S / N 1 - 9999 07-LEP (EA) Page 2 JUN 01 TABLE OF CONTENTS SUBJECT CHAPTER PAGE VALIDITY LIFTING AND SHORING 07-00-00 (CA) 1 1 - 9999 DESCRIPTION AND OPERATION 1 1. GENERAL 1 2. LOCATION 1 JACKING 07-10-00 (CA) 201 1 - 9999 MAINTENANCE PRACTICES 201 1. SERVICING - JACKING 201 A. Tools and consumable materials 201 B. Jacking procedure 201 C. Reconditioning 201 HOISTING 07-20-00 (CA) 201 1 - 9999 MAINTENANCE PRACTICES 201 1. SERVICING - HOISTING 201 A. Tools and consumable materials 201 B. Hoisting procedure for the fuselage equipped with the power plant 201 C. Reconditioning 202
ADAA Validity : S / N 1 - 9999 07 TC(EA) Page 1 JUN 01 PAGE INTENTIONALLY LEFT BLANK ADAA Validity : S / N 1 - 9999 07 TC (EA) Page 2 JUN 01 LIFTING AND SHORING DESCRIPTION AND OPERATION 1. GENERAL Lifting the aircraft is accomplished by using jacks placed at the 3 lifting points provided - refer to 07-10-00. Each of these 3 points can accommodate : - either a jack rest centering cup with "concave contact area" for a ball-head jack, dia. 0.98 in (25 mm). - or a jack rest centering cup with "convex contact area" for a concave head jack. Hoisting device is necessary for hoisting - refer to 07-20-00. 2. LOCATION (Figure 1) 3 lifting points are provided on the aircraft : - 1 point under each wing (outboard side of main gear leg) at 70.86 in (1800 mm) from aircraft centerline. - 1 forward point located on the firewall at 11.81 in (300 mm) from aircraft centerline. A - FWD lifting point B - Firewall C - Rear lifting point www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：TB 20 MAINTENANCE MANUAL 07 LIFTING AND SHORING TB20飞机维护手册 07 顶起和支撑
