1、MS34225 26 9999932 0008392 3 = I PED. SC CLAU 2620 niE TIRE SWL BE M AOMlIIlUHCE WIT T:;iHI,K, IliKN i.1NYAIIi.Y 1Hi:HIASKII Win1 TiHli Ti1 51011 IillRII1S AT BE TAXIfD Ow iHE FLYWHEEL WR 9OOO FEET AT 34.5 HPH WITH 5100 POUND WAD. CONVMTIONAL LANDING/TAXI. i“. THE FLYWEEL SPEED SHALL BE DECREASED UN
2、TIL A ROLL DISTANCE OF 6680 FEE US DEEN COVERED. DECELERATION RATE SHALL BE 5.39 FT/SEC/SEC BEWEEN 183 WH AND O WH. IHE TXRF, W SULL 8E LINPABLY MCREASED WITH TIHE FROM O TO Zoo0 PCWDS AT 7 SKUIDS. IIIEH LINWUY MCRFASED TO 4000 POUNDS AT 24.5 SECONDS, IHHM LINEARLY INCREASED To 4800 PCUNDS AT THE eM
3、, OF ME TOTAL LANDING TLW. OF APPWXWTELY 50 SECONOS. YIM 5100 rom uuo. SHORT LANDING/EXTMDED TAXI. 118 WH. AVERAGE DECELERATIOH RATE SHALL BE 5.76 FT/SEC/SEC FRW 111 HPH TO O HPH. 2000 POUNDS IN 3.1 SECOHDS. THEN LINEARLY INCREASED WITH TIME To 5100 ?WNDS AT TllE END OF mE TOTAL LANDING TIW OF APPRO
4、XIMTELY 30 SECONDS. AT 34.5 WH FOR 13.200 FEEI WITH 5100 POIRID LMD. ILIECRD TAKE-OFF. MEDIATELY BY LANDING THE TIRE AGAINST iHE PLYIMEEL ROTATING AT A PERIPHERAL SPEED OP 138 WH AND AN WUTE TIRE WING OF 4750 POUNDS. 3600 FEET US BEEN COVERED. Me INITIAL LOAD OF 4750 POUHDS SHALL BE LINEARLY INCREAS
5、ED WIT8 TIEiHER UI“ THE DATA AND I44TERIAL SPECIFIED ABOVE AKD IN m-r-smi 20 IRE NAVAL AIR SYSTEM com. MSIIINCT, D.C. 0361. AZNTION: AIR 53032. lImcs 7 1. OHALL BE OF TUE ISSUE IN erpecT ON MTE OF INVIUTION roP BIDS, 01 U!QUFST FOR PROPOSAL Rm lAT -CE IawsRY SIANMRDS SLULL GIVE ME MTE OF ME ISSUE AWPED. 2. mr MSICLI mnm mszs, m1s SrAmAm ms DrnCE otw PIOCULVHWT MCUIIPHZS ReFxRmcED HEREIN. . -. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
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