This item will be used as part of a system supporting the launch and/or recovery of aircraft, essential to system performance or operation, or preservation of life or safety of operating personnel; Item is critical application item (CAI)
CXCY
III Part Name Assigned by Controlling Agency
Guide Piston Assembly Launching Engine
CXCY
PART NAME ASSIGNED BY CONTROLLING AGENCY
Guide Piston Assembly Launching Engine
MARK
Special Markings and Identification
"Cage code, part number, contract number, serial number"
ADAV
Overall Diameter
19.50 inches nominal
SUPP
III Supplementary Features and Requirements
"Material shall be in accordance with ASTM B148 or ASTM B271/B271M, alloy C95500 (HT), with a minimum Brinell hardness of 200HBW; all fillets and corner radii shall be 0.25 R unless otherwise noted; surface roughness in micro inches shall be interpreted in accordance with ASME B46.1"
SUPP
SUPPLEMENTARY FEATURES
"Material shall be in accordance with ASTM B148 or ASTM B271/B271M, alloy C95500 (HT), with a minimum Brinell hardness of 200HBW; all fillets and corner radii shall be 0.25 R unless otherwise noted; surface roughness in micro inches shall be interpreted in accordance with ASME B46.1"
ZZZK
SPECIFICATION/STANDARD DATA
05047-ASME Y14.100 Professional/Industrial Association Standard and 05047-Y14.5M-1982 Professional/Industrial Association Standard