A 747-400 MAINTENANCE MANUAL
 China Southern Airlines ~........................................................................................................
 | PAGE DATE CODE | PAGE DATE CODE | PAGE DATE CODE || | | || |07-11-04 | ||CHAPTER 07 TAB | 201 JUN 10/97 01 | || | 202 JUN 10/97 01 | ||LIFTING AND SHORING | 203 JUN 10/97 01 | || | 204 FEB 10/92 01 | || | 205 JUN 10/97 01 | ||7-CONTENTS | 206 JUN 10/97 01 | || 1 FEB 18/02 GUN | | || 2 BLANK |07-11-05 | || | 201 JUN 10/97 01 | ||07-11-00 | 202 JUN 10/97 01 | || 1 JUN 10/93 01 | 203 JUN 10/97 01 | || 2 JUN 10/93 01 | 204 FEB 10/92 01 | || | | ||07-11-01 |07-11-06 | || 201 FEB 15/99 01 | 201 FEB 10/92 01 | || 202 JUN 10/97 01 | 202 JUN 10/97 01 | || 203 OCT 15/98 01 | 203 FEB 10/92 01 | || 204 FEB 15/99 01 | 204 JUN 10/97 01 | || 205 FEB 10/92 01 | | || 206 FEB 10/92 01 |07-11-07 | || 207 JUN 18/00 01 | 201 JUN 15/98 01 | || 208 JUN 18/00 02 | 202 OCT 10/92 01 | || 209 JUN 18/00 01 | 203 JUN 15/98 01 | || 210 JUN 18/00 01 | 204 JUN 15/98 01 | || 211 JUN 18/00 01 | 205 JUN 15/98 01 | || 212 JUN 18/00 01 | 206 BLANK | || | | ||07-11-02 |07-11-08 | || 201 OCT 18/01 02 | 201 FEB 18/01 03 | || 202 OCT 18/01 02 | 202 FEB 18/01 02 | || 203 OCT 18/01 02 | 203 FEB 18/01 03 | || 204 JUN 10/97 01 | 204 FEB 18/01 04 | || 205 JUN 18/99 01 | 205 FEB 18/01 04 | || 206 JUN 18/99 01 | 206 FEB 18/01 03 | || 207 FEB 15/99 01 | 207 FEB 18/01 04 | || 208 JUN 18/99 01 | 208 BLANK | || 209 FEB 15/99 01 | | || 210 OCT 18/01 03 |07-20-00 | || 211 OCT 18/00 01 | 201 OCT 18/99 01 | || 212 OCT 18/01 02 | 202 JUN 10/97 01 | || 213 FEB 15/99 01 | 203 FEB 15/99 02 | || 214 FEB 15/99 01 | 204 FEB 10/92 01 | || | 205 FEB 15/99 01 | ||07-11-03 | 206 FEB 10/92 01 | || 201 OCT 10/95 01 | 207 FEB 10/92 01 | || 202 FEB 10/92 01 | 208 BLANK | || 203 FEB 10/92 01 | | || 204 OCT 10/97 01 | | || 205 OCT 10/96 01 | | || 206 JUN 10/97 01 | | || 207 JUN 10/97 01 | | || 208 OCT 10/96 01 | | || 209 JUN 10/97 01 | | || 210 JUN 10/93 01 | | || 211 JUN 10/97 01 | | || 212 JUN 10/97 01 | | || 213 JUN 10/97 01 | | || 214 JUN 10/97 01 | | |2..................................…..................................…..................................1
 R = REVISED, A = ADDED OR D = DELETED CHAPTER 07 F = FOLDOUT PAGE EFFECTIVE PAGES E1 PAGE 1 FEB 18/02 LAST PAGE
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400 MAINTENANCE MANUAL
 CHAPTER 07 - LIFTING AND SHORING
 TABLE OF CONTENTS
_________________
 Chapter
 Section Subject_______ Subject ____ Effectivity
_______ Page ___________
 JACKING 07-10-00
_______
 LIFT AIRPLANE FOR MAINTENANCE 07-11-00
 Description and Operation 1 ALL
 JACK AIRPLANE 07-11-01
 Maintenance Practices 201 ALL
 JACKING AIRPLANE AXLES 07-11-03
 Maintenance Practices 201 ALL
 JACKING AIRPLANE FOR FUEL LEAK 07-11-04
 TEST
 Maintenance Practices 201 ALL
 JACKING AIRPLANE NOSE 07-11-02
 Maintenance Practices 201 ALL
 JACKING AN ASYMMETRIC AIRPLANE 07-11-07
 Maintenance Practices 201 ALL
 MOVE LANDING GEAR ABOVE PIT 07-11-06
 Maintenance Practices 201 ALL
 SUPPORTING AIRPLANE WITH ENGINES 07-11-05
 REMOVED
 Maintenance Practices 201 ALL
 TAIL SUPPORT - CARGO AND FUEL 07-11-08
 LOADING
 Maintenance Practices 201 [*]
 [*] AIRPLANE RM852 REQUIRES 65B16363-1M-556087F STANCHION SUPPORT
 FITTING BE INSTALLED PRIOR TO ADAPTER
 SHORING 07-20-00
_______ Maintenance Practices 201 ALL
 7-CONTENTS
 GUN Page 1 Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 LIFT AIRPLANE FOR MAINTENANCE - DESCRIPTION AND OPERATION
_________________________________________________________
 1.  General
_______
 A.  The airplane is provided with three primary jack points and five stabilizing jack points. Primary jack points are at left and right wing to body junction and at the tail. The five stabilizing jack points are at the nose, center of each wing, and at each wingtip. The jack at each wingtip is a lift point to raise the wing for maintenance functions. In addition, there is a jack point under the nose gear axle and two jack points under each main gear truck. Maximum allowable loads specified in individual procedures should not be exceeded. An adapter is required at some jack points.
 B.  Any jack or jack system which satisfies the jacking requirements may be used to jack the airplane. Currently, systems produced by Regent Malabar, Columbus, Hydro-Geratebau, and Skyhi are among those systems. Operate jacks in accordance with the manufacturer's instructions.
　
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