1、LVAEP. lO8OA (Rev. 5-51) !%C 5305 (c) DRILLED HOLE TO BE ON CENTER APPROXIWTELY AT RIGHT ANGLES TO THE SLOT BLI mST NOT BW THROUGH (d) FOR MCHINE SCREWS 2 INCHES LOHG ANC SHORTER, COHPLETE TdREADS SHAW EKES2 T WITHIH 2 THREADS MEAD. ?HE BASE OR TOP (SPHERICAL PORTION) OF THE HEAD. A HINIHW COIFLETE
2、IHREAD LENGTH OF 1-3/L INCHES. OF IHE BmING SUWACE OF THE HEAD OR CLOSER IF PRACTICABLE. SCFZWS OF LONGER LENGTH SHALL HAVE FOR DEFINITION AX3 APPLICATION OF DRAWING STATUS NOTES. SEE WD-D-1000. (e) Au FILLISTER HEAD SCWS WITH LYlDRILLED HEADS INACTIVE FOR DESIGA AFTER 12 HAY 1950. (f) REFEREHCE DIH
3、EHSIONS lJcE FOR DESIGN PWOSES ONLY AND ARE NOT A!: INSPECTION REQVIREHENT. y&) NM PREFERRED FOR AI- USE. TERIAL: (2) CARBON STEEL. W-S-637 TYPE FS1010. 60.000 PSI MNIMM TENSILE STREHCTH OR “HER STEEL )IEETItKi YE-SAXE F?3SICAr REQ:IRE!ENTS. mm *. . . . _ (1) CORROSON RESISTMI STEEL. FEDERAL STANDAR
4、D NO. 66, TYPE 302, 306, 316, AND 303 SE 8 (1) BRASS, CaDIERClAL. 55,000 PSI KINI!fLW ULTIMATE TENSILE STRENGTH. FINISH: CARBON STEEL, CADIIiUH PLATE, PQ-P-hl6, TYP6 I. CUSS 3. CORROSION RESISTAtiT SlXEL. PASSIVATE. USAGE. 0 REINSTATED As W 12 NOVEMBER 1980. PROCUREMENT AIR FORCE- NAVY AERONAUTICAL STANDARD SPECIFICATION AN500 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
