NAVY MS14224-1982 TIRE PNEUMATIC AIRCRAFT 13 5 X 6 00-4 (NAVY) (AV-8B WLG)《13 5 X 6 00-4(NAVY)(AV-8B WLG)飞机汽轮胎》.pdf
《NAVY MS14224-1982 TIRE PNEUMATIC AIRCRAFT 13 5 X 6 00-4 (NAVY) (AV-8B WLG)《13 5 X 6 00-4(NAVY)(AV-8B WLG)飞机汽轮胎》.pdf》由会员分享,可在线阅读,更多相关《NAVY MS14224-1982 TIRE PNEUMATIC AIRCRAFT 13 5 X 6 00-4 (NAVY) (AV-8B WLG)《13 5 X 6 00-4(NAVY)(AV-8B WLG)飞机汽轮胎》.pdf(3页珍藏版)》请在麦多课文档分享上搜索。
1、MS111224 26 7777732 0008387 3 XRE Till5 SUU BE IN rsrmnUieE YI lW AWLICADLE WIlbnrrrS O1 MIL-T-5041 UCD OF THE TOTAL LA!;DINC TI.% OF A?PROXDi%TELY 15 SECONDS. IWDUTELY AFTER UNDING. ME TIRI SHALL BE TAXIED ON THE FLYhHEEL AT 34.5 XPH FOR 9000 FEET WIM 1150 POUND ME TIRE SHALL BE UVDED AGAINST A FLY
2、WHEEL ROTATING AT A PERIPHEPAL SPEED lliE FLYWEEL SPEED SHALL BE DECREASED LTTIL A ROLL DISTASCE OF 775 FEET HAS BEEN COVERED. LOAD. nsT c CONVE!iTIOXAL LANDLVG/TAXI. THE TIRE SHALL BE LILSXD AGAINST A FLYWHEEL ROTATING AT A PERIPHERAL SPEED OF 183 WH. THE FLYWEEL SPEEL! SHALL BE DECREASED LWIL A RO
3、LL DISTA!CE OF 6680 FEET HAS BEEK COVERED. THE AVERAGE DECELERATION RATE SIIALL BE 5.39 FT/SEC/SEC BETUEES 183 KPH ASD O WH. LINEARLY INCRt%SED KITH T1NE FRO! O TO 775 POGNDS AT. 1 SECOSD, MEN LINEARLY INCREASED WIM TIME TO 1025 POUSDS AT TliE EXD OF THE TOTAL UNDING T1tE OF APPROJI?ATELY 50 SECON3S
4、. TIRE SHALL BE TAXIED ON THE PLYWEEL A: 34.5 WH FOR9000 FEET WITH 1150 POUND THE TIRE LOAD SHALL BE II.IEDUTELY AFTER LWDING ME LOAD. SHORT UDISG/ESTENDED TAXI. THE TIRE SHALL BE UVDED AGAINST A FLYUHEEL ROTATING AT A PERIPHERAL SPEED OF llB FIPIi. ME AVERACE DECEI.ERT1ON RATE S!lALI. BE 5.76 FTISE
5、CISEC FROH 118 HPH TO O tPH. nIE LOAD SHALL BE LINURLY 1NCRWSEil hlTIi TI!iC FRO! O TO H4C POCNOS AT 7.6 SECONDS, iIIEs LINEARLY INCREASED WIM TItiE TO 1150 POIRIDS AT TIiE END OF iE TOTAL LANDIST. TILE OF APPROXlL%EL 30 SECOtiDS. SHALL BE TAXIED OS THE FLYWEEL AT 3G.5 HPH FOR 13,200 FEET KIM 1450 P
6、OUXD THE tLhllEEl, SPEED SHALL EE DECREASED mTIL A ROLL DISTANCE Or 2600 FEET HAS BEEN COVERED. IWDUTELY AFTER ME UNDING, IHE TIRE LAD. n!ST J RWECTED TAKE-OFF. IHHEDUTELY BY WSDINC ME TIRE AGAINST ME FLYhXEEL ROTATING AT A PERIPHERAL SPEED OF 138 WH UITH As IIMEDUTE TIRE LOADING OF 1150 POL%DE. THE
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