AIR FORCE MS22004 REV C-1986 ADJUSTER LAP AIRCRAFT SAFETY BELT《飞机安全带系带调节器》.pdf

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1、MS22009 REV C 3b m 7777932 0008972 7 m R FORCE- 82 TILE ADJUSTER, LAP, AIRCRAFT SAFETY BELT herbst NAVY-AS KKUREMENT SPECIFICATIOH SUPERSEOES: NONE USAF DRAWING 51A3697 AND NAF DRAWING 311926-2A 9-09 27 MIL IT A UY ST AH DA UD MS 22004 SHEET I OF I FED. SUP CLASS 1680 ,094 RAD- .O62 RAD 1 h“ I 9 1i7

2、 +.o16 -.o00 RAD I PLATE SECTION A-A LMFRS NAME OR IADEHARK AND t.E PART NO. HERE -1.P53 ,- PLATE 12500 LBS 1 I I r, t I . hbi 1 .rlATEEIAL: PLATE; STEEL, SPECIFICATION MIL-S-5626, OR MIL-S-6049, OR M1L-S- I8729 HEAT TREATIIEKT: PLATE; SPECIFICATIO!I KIL-H-6875. ROCKWELL C3 M Ch2. DECARBIIRIZATION S

3、HALL NOT EXCEED .010. FIIXSH: -1 CAOHIUM PLATE PEP CQ-P-416, TYPE 1, CLASZ 1 REMOVE ALL BURRS AND SHARP EDGES. ADJUSTERS SHALL BE SMOOTH AW FREE FROX FINS AIU PITS. DItENSIONS IN INCHE. ADJUSTERS SHALL BE SUBJECTED TO THE PROuF LOADS FPECIFID HEREON AS INDICATED BY THE ARROdS. -2 PHOSPHATE COATING P

4、ER DOO-P-16232, TYPE 3., CLASS 4 FOLLOWED BY WAX EMULSION MIL-W-3688 UNLESS OTHER%rTSE SPECIFIED, TOLERANCES: DECIMALS 2.016. hEBBIKG, tYU)N, SPECIFICATION MIL-W-LO, TYPE M,SHALL BE UTILIZED DURIWG PROOF LOADINOS. OF 30,000 LE PER .?QUARE INCH PER MINUTE, IN ACCORDANCE WITH SPECIEICATION OQ-tl-11. P

5、ROOF MADS SHALL BE APPLIED AT THE RATE THIS STANDARD TAKES PRECEDENCE OVER WCUhENTS REFEREWED HEREII. REFERENCED DOCUMENTS SHALL BE OF THE ISSUE A EFirTCT ON DATE OF INVITATIONS FOR BID. . ENP ITEM EXAPINATIIIN -, P. CRITICAL DIEEHSIONC: AS SHCWN * c/ E. CRITICAL FUNCTIONSL TEST: BAR SHALL )!OVE FRE

6、ELY, C. PPOOF LOAD METHOD: AS SHfii! - USIYG SUITABLE TIXTURES. C. MANLIFACTURE IR ACCDROAYCE I!ITH MIL-H-7195. AMSC N/A . U c U DD 672-1 (Coordin*t-d) “DISTRIBUTION STATEMENT A. Approved for pub1 ic release; distr c unlimited.“ -L, *US. GOVERNMENT PRINTING-OFFICE 1986 - 605-036143877 Licensed by Information Handling Services

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