| MRC | Name | Details |
|---|
| AGAV | End Item Identification | C13-2 and TC13-2 catapults for aircraft carriers |
| MATT | Material Composition | Aluminum alloy |
| CRTL | Criticality Code Justification | FEAT |
| FEAT | Special Features and Requirements | This item will be used as part of a system supporting the launch and/or recovery of aircraft and is essential to system performance or operation, or the preservation of life or safety of operating personnel; it is critical application item (CAI) |
| CXCY | Assigned Part Name 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, and serial number |
| ADAV | Overall Diameter and Dimensions | 19.50 inches nominal |
| SUPP | 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 .25 R unless otherwise noted; surface roughness in micro inches shall be interpreted in accordance with ASME B46.1 |
| SUPP | 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 .25 R unless otherwise noted; surface roughness in micro inches shall be interpreted in accordance with ASME B46.1 |
| ZZZK | Specification/Standard Data and Compliance | 05047-ASME Y14.100 professional/industrial association standard and 05047-Y14.5M-1982 professional/industrial association standard |
| SPCL | Special Test Features and Requirements | Material: aluminum bronze; casting: nominal stock size; unit weight: 488lbs |
| ABHP | Overall Length and Dimensions | 11.06 inches nominal |