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
7、 FLYLXEEL SPEED CiLS BE DECREASED LXTIL A ROLL DISTILXCE OF 3800 FEET HAS BEEN COVERED. WH. ME INITIAL LOA Or li50 POL3DS SUL1 BE LISEARLY IXCRWSEI! KlTH TIX TO 1280 POLSDS AT ME EID OF MIS TEST SHALL COiiSlST OF THE PROCEDCRE OF TEST “A“ TO SI!4TLATE TAKE-OFF, FOLLORD THE AVERAGE DECELERATIOS RATE
8、SHALL BE 5.39 FTISECISEC BEIhEEX 138 WH AND O ME TOTAL UNDING 11% OF APPROXIXTELY 37 SECOXDS. IIEDLATELY AFTER LANDXSG, THE TIRE SHALL BE TAXIED ON HE FLYWEEL AT 34.5 WH FOR 9000 FEET um 1150 POWD LOAD. nlRSING TAY1 (LEFT). KPH FOR 300 FEET KIM 4520 P0GSJ:;IS VERTICAL LOAC ASO YITH PLILSE OF TIW. YA
9、RD LEFT AT M ANGLE OF 7.0 DECREE! THE TIRE SUL1 BE USDED AGAXST A FLYWEEL ROTATING AT A PERIPHERAL SPEED OF 34.5 AND MIBERED OUTBOAFZJ A1 &.O DEC!.EF.S. - K2 TES1 L ILIWING TAW (RIGHT). MYE AS K, EXCEPT:EITH PUSSE OF TIRE YAWED RIGHT AT AS ANGLE OF 7.0 DEGIZES AND CMIERED ISGOARD AT 4.0 DECREES.“ BU
10、RST TEST. THE TIRE SHALL BE SUBJECTED TO A HYDROSTATIC BURST TEST. ME PRESSURE SHALL BE INCREASED UNTU ME TIRE FAILS. IH THE QUALIFICATION TEST REPORT. THE FAILIIIG PRESSCRS, DESCRiPTiOS OF FAILURE, ASD LOCATION OF FAILURE SMI BL REPORTED ZtsT 1 BRUISE TEST. ROND BAR STOCK OR ARRESTING GEAR CABLE VI
11、M A VERTICAL LOAD OF 7500 POL7(TiS. RELEASE OF THIS LOAD THE TIRE SiULL BE SW.IECTE9 TO ME SAXE LOADISG COSDITIOS AT A LOCATION 188 DECREES IN ROTATIOS FRON ME INITIXL PCIST OF LOADISG. A TIRE INFLATED TO 135 PSI SHALL BE LOADED AGAINST A 1-3/8 nCJl DIAWTER LENGTH OF PLAIN IIMEDIATTELY FOLLOWING ME
12、I MILITARY STANDARD- NAVY -AS kcr, TITLE I- TIRE, PNEIMATIC. AIRCRATT 13.5 X 6.00-4 (NAVY) I I *OCUIIEMNT YLCHCTKW LUCERSDES: WET F HXL-1-504 1 a Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. MS14224 26 M 7777732 0008373 3 M Q H s w U N OD QI d E Y e c U 4 a a I MILITARY STANDARD A IAW-AI m OIhb Tim, ?NZUIUTIC, ACRAF 13.5 X 6.00-4 (MAW) UV-B VLC) MS14224(AS) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
