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
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本文鏈接地址：TB 20 MAINTENANCE MANUAL 07 LIFTING AND SHORING TB20飛機(jī)維護(hù)手冊 07 頂起和支撐
