1、- MS22005 REV E Lb = 7777732 0008473 9 M 3 -0ci - e127 ROCUREMENT SPECIFICATION SUPERSEDES: USAF DRAWINGS 44A9571 AND 5lA3782 NONE NAF DEANINQ 311926-5 AND 311926-6 I FED. SUP CLAS! SHEET 1 OF I ic Lo31 RAD KNURL SHALL NOT BE RROUQHT UP SHARP, KNURLING -I- SHALL EXTEND FULL LENGTH OF CYLINPRICALPO.R
2、IION- KNURLING- SHALL IFCREASE DIAMETER BY AT LEAST .-_- . .IO INCH. BEFORE KNURLING /375 I MS PART NO. IA I +.o800 I I FINISH I -.O16 CADMIUM I MS22005-4 I 3.875 I 3.062 I .406 I ZINC I MATERIAL I STEEL, SPECIFLCATION MIL-S-5626, MIL-S-6049, MLL-S-6758 OR ASTM A331-74, A331 -81 . HEAT TREATMENT : 1
3、70,000 TO 190,000 Ibs./aq.in. TENSILE STRENGTH. VERIFY BY DETERMINING HARDNESS RCX-42. FINISH : CADMIUM PLATE PER 90-P-416 ,TYPE I, CLASS I ZINC FLAKE COAT PER MIL-C-87115 , TYPEU. REMOVE ALL BURRS AND SHARP EDGES. DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED, TOLERANCES : DECIMALS f .O16 . THESE
4、 PARTS ARE USED IN THE MANUFACTURE OF ADJUSTERS, MS22007 AND MS22004. THM SHALL NOT BE FURNISHED TO SERVICE ACTIVITIES AS A SEPERATE ITEM . CHECK HARDNESS BY TESTING CORE SAMPLE PER ASTM E18 AND MIL-H-7195 WITHIN AREA BOUNDED Byp- . MANUFACTURE IAW MIL-H-7195. - - - FOR DESIGN FEATURE PURPOSES , THI
5、S STANDARD TAKES PRECEDENCE OVER PROCUREMENT DOCUMENTS REFERENCED HEREIN. REFERENCED DOCUMENTS SHALL BE OF THE ISSUE IN EFFECT ON DATE OF INVITATIONS FOR BID. .A. Ait . Force- 82 TITLE I MILITARY STANDARD BAR. ADJUSTER, LAP AIRCRAFT SAFETY BELT Ihn Gist Navy - AS AF - 99 * MS22005 DD ,!E, 672-1 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
