757 Airplane Recovery Document 飞机恢复文件(75)

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BODY STA INCH  BODY BUTTOCK LINE INCH  BODY WATER LINE INCH  ROLL UNDER HEIGHT  EXTENDED HEIGHT MAXIMUM *[2] 
FWD FUSELAGE  A  12200  395.0  R  56.5  169.8  269.2  360.6 *[3]  B07001-7 
REAR WING SPAR  B  42184  1109.2  L  241.3  192.6  330.2  411.5 *[3]  F80060-6 
C  42184  1109.2  R  241.3  192.6 
AFT FUSELAGE *[4] 
(STABILIZING  *[5]1814  1777.7  0.0  180.8  312.4  391.2 *[3]  B07002-1 
POINT)  D 
MAIN GEAR AXLE  E  23540  1088.8  L  144.0  VAR 
*[6]*[7] 
F  23540 23540  1088.8 1133.8  R L  144.0 144.0  VAR VAR  12.5 *[8]  40.6  NONE REQUIRED 
NOSE GEAR AXLE *[9]  23540  1133.8  R  144.0  VAR 
G  14106  385.0  0.0  VAR  11.4 *[8]  40.6  NONE REQUIRED 

*[1] INCLUDES 35 KNOT WIND LOADS *[2] INCLUDES 5 CM TIRE CLEARANCE *[3] FOR NEW SEAL INSTALLATION OVER TOP OF OLEO INNER CYLINDER ADD 56CM *[4] WARNING: JACK POINT "D" IS A STABILIZATION POINT AND IS NOT TO BE USED WHILE RAISING OR
LOWERING THE AIRPLANE. POINT "D" SHOULD BE ENGAGED ONLY AFTER PRIMARY JACKS ARE SECURED IN FINAL POSITION. *[5] THIS VALUE IS LIMITED BY THE FORWARD FUSELAGE ALLOWABLE JACK LOAD. LOCAL STRUCTURAL ALLOWABLE IS 5443 KG. *[6] JACK POINT BODY STATIONS ARE FOR GEARS IN THE STATIC TAXI POSITION. MAIN GEAR JACK POINTS WILL VARY WITH DIFFERENT OLEO EXTENSIONS. *[7] INITIAL LOAD: 23540 WITH 100000 KG MTW
INCREASE TO 24494 WITH 104782 KG MTW
INCREASE TO 24676 WITH 109318 KG MTW
INCREASE TO 26263 WITH 113854 KG MTW
*[8] WHEELS ON RIMS
*[9] INITIAL LOAD: 14106 WITH 100000 KG MTW

INCREASE TO 14379 WITH 104782 KG MTW
INCREASE TO 14470 WITH 109318 KG MTW
INCREASE TO 15060 WITH 113854 KG MTW
NOTE: LOCATIONS ARE IN INCHES
WEIGHTS ARE IN KILOGRAMS
HEIGHTS ARE IN CENTIMETERS
3-30-4

JACK POINT LOCATIONS
Page 3-61 Jul 01/2005 D623N004
 

757
AIRPLANE RECOVERY DOCUMENT
Figure 3-36 MODEL 757-300 JACKING LIMIT LOADS (ENGLISH WEIGHTS AND MEASURES)

JACK POINTS  MAX JACK LOAD LB *[1]  LOCATION  JACK HEIGHT  JACK ADAPTER FITTING 
BODY STA INCH  BODY BUTTOCK LINE INCH  BODY WATER LINE INCH  ROLL UNDER HEIGHT  EXTENDED HEIGHT MAXIMUM *[2] 
FWD FUSELAGE *[3]  A  26600  395.0  R  56.5  169.8  107.0  144.0 *[4]  B07001-7 
REAR WING 
SPAR *[3]  B  108400  1109.2  L  241.3  192.6  131.0  164.0 *[4]  F80060-6 
C  108400  1109.2  R  241.3  192.6 
　
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