1、20. I 2620 - 20.60MAX I 1 50.39 MAX 57.10 MAX 54.30 MIN DIA v 1 lop I look. APPLIED CARRIAGE LOAD 57,000 LBS INBOARD OUT BOAR D FLYWHEEL -ECWNCS AFTER LANDING AN HELD AT THIS LOAD LNTIL THE TOTAL RML DISTANCE Of 6.0116 FEET HAS BEEN COVEREG .N APPROXIMATELY 43 SECDNDS. IVERAGE DECELERATION OF 4.5 FT
2、/SEC!SEC FR34 160 MPH TO 30 MPH. THE LOAE SHALL INCREASE LINEAqLY FROM ZERO THE TIRE SHALL THEN BE TAXIED AT 30 MPH FOR 13.506 FEET AT 27. OGO POUND LOAD. :. “C“ TAXI AND CAMBER: 1) ACCELERATE THE FLYHEEL TO 30 MPH ANO MAINTAIN THIS SEE THROUGHMIT THF TEST, (2) LAND THE TIRE ON THE FLYHEEL IN A POSI
3、TION OF IO“ CAMBER. (3 i INCREASE THE CARRIAGE LOAO LINEARLY WITH TIME FROM ZERO TO 57, OOC LRS. FOR DETAIL A. OR 17900 LBS FOR MTAIL B. WITHIN 1 10 SECONDS AFTER LANCING AND MAINTAIN THIS LOAO UNTIL A RELL DISTANCE IF 2300 FEET HAS BEEN COVERED (II i THERE SHALL BE 30 CYCLES OF THE ABOVE TEST COMPL
4、ETED AT IO“ CAMBER INBOARC AND 30 CYCLES AT Co CWER WTBOARD. . LSO BE MARKED AS REWIRED BY MIL-R-7726. AU IDENTIFICATION MARKINGS CIF THE IXIGINAL TIRE UILL BE MAINTAINED ANU THE REBUILT TIRE KILL *us. GOVERNMENT PR1NTiN.G OFFICE: 1977-703.122/6367 I 2 OF2 WET AF DWG NO. 68029335 XUIEYNT SPECIFUTION WPERtEMS: MIL- R-7726 DO 672-1 (L1mit.l mr41li;tl.m) .011(0.01t eUUAV H VID. -. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
