| MRC | Name | Details |
|---|
| AGAV | Item Identification | C13-2 and TC13-2 catapults for aircraft carriers |
| MATT | Material Composition | Aluminum alloy |
| CRTL | Criticality Code Justification | FEAT (Feature Emphasized for Technical Acceptance) |
| FEAT | Special Features and Capabilities | This item is used in a system supporting aircraft launch and recovery, essential for performance or operation, or preservation of life or safety. It's a Critical Application Item (CAI). |
| CXCY | Agency-Assigned Part Name | 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 | Additional Features and Requirements | The material must meet ASTM B148 or ASTM B271/B271M standards, with a minimum Brinell hardness of 200HBW. Fillets and corner radii should be .25 R unless otherwise noted, and surface roughness in micro inches is to be interpreted according to ASME B46.1. |
| SUPP | Supplementary Features and Requirements | The material must meet ASTM B148 or ASTM B271/B271M standards, with a minimum Brinell hardness of 200HBW. Fillets and corner radii should be .25 R unless otherwise noted, and surface roughness in micro inches is to be interpreted according to ASME B46.1. |
| ZZZK | Specifications and Standards Data | ASME Y14.100 Professional/Industrial Association Standard and 05047-Y14.5M-1982 Professional/Industrial Association Standard |
| SPCL | Special Test Features and Characteristics | Material: aluminum bronze, casting: nominal stock size, unit weight: 488 pounds. |
| ABHP | Overall Length and Dimensions | 11.06 inches nominal |