CONDITION TIRE SIZE
H31X13-12
A B
NORMAL INFLATION 10.3 (26.2) 10.0 (25.4)
TWO FLAT TIRES 6.5 (16.5) 3.5 (8.9)
ON WHEEL RIMS 4.5 (11.4) 14.1 (35.8)
ON A JACK FOR A TIRE CHANGE, TIRES INFLATED 15.4 (39.1) 10.5 (26.7)
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Figure 3-34 MODEL 757-200 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 FU-SELAGE A 26,900 395.0 R 56.5 169.8 106.0 142.0 *[3] B07001-7
REAR WING SPAR AFT FUSELAGE B C 93,000 93,000 1109.2 1109.2 L R 241.3 241.3 192.6 192.6 130.0 162.0 *[3] F80060-6
(STABILIZING D *[5]4,000 1777.7 0.0 180.8 123.0 154.0 *[3] B07002-1
POINT)*[4]
MAIN GEAR AXLE *[6]*[7] NOSE GEAR AXLE *[9] E F 51,900 51,900 51,900 51,900 1088.8 1088.8 1133.8 1133.8 L R L R 144.0 144.0 144.0 144.0 VAR VAR VAR VAR 4.9 *[8] 16.0 NONE REQUIRED
G 31,100 385.0 0.0 VAR 4.5 *[8] 16.0 NONE REQUIRED
*[1] INCLUDES 35 KNOT WIND LOADS *[2] INCLUDES 2 INCH TIRE CLEARANCE. *[3] FOR NEW SEAL INSTALLATION OVER TOP OF OLEO INNER CYLINDER ADD 22.0 INCHES *[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 12,000 LB. *[6] JACK POINT BODY STATIONS ARE FOR GEARS IN THE STATIC TAXI POSITION. MAIN GEAR JACK POINT WILL VARY WITH DIFFERENT OLEO EXTENSIONS. *[7] INITIAL LOAD: 51,900 WITH 221,000 LB MTW
INCREASE TO 54,000 WITH 231,000 LB MTW
INCREASE TO 54,400 WITH 241,000 LB MTW
INCREASE TO 57,900 WITH 251,000 LB MTW
*[8] WHEELS ON RIMS
*[9] INITIAL LOAD: 31,100 WITH 221,000 LB MTW
INCREASE TO 31,700 WITH 231,000 LB MTW
INCREASE TO 31,900 WITH 241,000 LB MTW
INCREASE TO 33,200 WITH 251,000 LB MTW
NOTE: WEIGHTS ARE IN POUNDS
DIMENSIONS ARE IN INCHES
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JACK POINT LOCATIONS
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Figure 3-35 MODEL 757-200 JACKING LIMIT LOADS (METRIC WEIGHTS AND MEASURES)
JACK POINTS MAX JACK LOAD KG*[1] LOCATION JACK HEIGHT JACK ADAPTER FITTING 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 Airplane Recovery Document 飞机恢复文件(74)
