1、Ci-J;.-l O POUNDS TO 5,000 POUNDS IN 5 SECONDS; TO THE TIRE SHALL THEN BE TAXIED AT 30 MPH AND THE TEST C PERIPHERAL SPEED OF 34.5MPH AND UNLANDED AFTER A DISTANCE OF 300 FEET HAS BEEN COVERED. OF 375 PSI ADJUSTED FOR FLYWHEEL CURVATURE SHALL BE USED. CATAPULT TAKEOFF - THE TIRE SHALL BE LANDED AT
2、A LOAD OF 45,000 POUHDS AGAINST THE FLYWHEEL ROTATING AT A AN INFLATION PRESSURE EMIRE STANDARD REVISED .A. TITLE I MILITARY STANDA YAVY - AS Dther Cust GCUREMENT SPECIFICATION MIL-T-5041 TIRE, PNEUMATIC, AIRCRAFT, 28 X 9.0, TYPE VI1 (NAVY) MS90443(AS PROJECT NDi 2620-N240 PREVIOUS EDITIONS OF THIS
3、FORM ARE OBSOLETE. DDl“1672-1 (Limited cmrdination) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-FED.SUPCLASS 2620 TEST D TAKEOFF CAMBER Dl PERFORM THE TEST A SPECTRUM WITH THE PLANE OF THE TIRE INCLINED INBOARD AT AN ANGLE OF 5 DEGREES. D2 PERFOR
4、M THE TEST A SPECTRUM WITH THE PLANE OF THE TIRE INCLINED OUTBOARD AT AN ANGLE OF 5 DEGREES. TEST E LANDING CAMBER El PERFORM THE TEST B E2 PERFORM THE TEST B SPECTRUI WITH THE PLANE OF THE TIRE INCLINED INBOARD AT AN ANGLE OF 5 DEGREES SPECTRUM WITH THE PLANE OF THE TIRE INCLINED OUTBOARD AT AN ANG
5、LE OF 5 DEGREES. TEST F UNTIL THE TIRE FAILS. It4 THE QUALIFICATION REPORT. BURST TEST - THE TIRE SHALL BE SUBJECTED TO A HYDROSTATIC BURST TEST. THE PRESSURE SHALL BE INCREASED THE FAILING PRESSURE, DESCRIPTION OF FAILURE AND LOCATION OF FAILURE SHALL BE REPORTED AIR RETENTION - THE TUBELESS TIRE S
6、HALL BE INFLATED TO A PRESSURE OF 375 PSI AND ALLOWED TO STAND FOR A PERIOD OF 24 HOURS AT WHICH TIME THE PRESSURE DROP DUE TO GROUTH SHALL BE REPLACED. ADDITIOIAL 24 HOURS AT WHICH TIME THE PRESSURE SHALL BE MEASURED AND THE TIRE IHSPECTEO. THE AIR PRESSURE LOSS SHALL NOT EXCEED 5 PERCENT AND THE T
7、IRE SHALL NOT REVEAL ANY APPEARANCE AND PERFORMING DEFECTS SUCH AS SIDEWALL BLISTERS, TREAD SEPARATION, ETC. THE TIRE SHALL THEN STAND FOR AN QUALIFICATION TEST REPORT - THE QUALIFICATION TEST REPORT SHALL LIST THE RESULTS OF ALL QUALIFICATION TESTS AND THE COXTRUCTION DETAILS OF THE QUALIFICATION T
8、EST SAMPLE IN THE GENERAL FORM SHOWN IN FIGURES 2 AND 3 OF MIL-T-5041. IN ADDITION, THE ACTUAL TIRE DIMENSIONS WHEN INFLATED TO 375 PSI SHALL BE LISTED. SHALL INDICATE THE MANUFACTURERS TEST NUMBER. HEoATA_AHD_IYTERIAL_SPECFI-ED ABOVE-A!O IN MIL-T-5041 SHALL BE SUBMITTED TO THE NAVAL AIR SYSTEMS COM
9、MAND. THE REPORT TWO (2) COPIES OF THE QUALIFICATION TEST REPORT, ALONG WITH WHHlNtiIUN, U.L. ZWbI Al Ili: AlikS3UJZ. NOTES: 1. REFERENCED DOCUMENTS SHALL BE OF THE ISSUE It4 EFFECT ON DATE OF INVITATION FOR BIDS OR REQUEST FOR PROPOSAL EXCEPT THAT REFERENCED INDUSTRY STANDARDS SHRLL GIVE THE DATE O
10、F THE ISSUE WPTED. 2. FOR DESIGN FEATURE PURPOSES, THIS STANDARD TAKES PRECEDENCE OVER PROCUREMENT DOCUMENTS REFERENCED HEREIN, .341 ,625 +- FIG. 1 RIM DATA I 11.943 I LEDGE DIA. MEASURED AT .625 DIM. FROM FLANGE. .A. lther Cuct AVY - AS TITLE TIRE, PNEUMATIC, AIRCRAFT, 28 X 9.0, TYPE VI1 (NAVY) U i
11、1 L L MILITARY STANDARD h I I 2 OF 2 ROCUREMENTSPECIFICATION SUPERSEDES: SHEET MIL-T-5041 PRNIOUSEDITIONSOFTHIS FORM AREOBSOLETE. DD,“,672-1 (Limited cmfdinatian) - -e- -. *US. GOVERNMENT PRINTING OFFICE: 1985 - 505-038/24012 2P6f Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
