| MRC | Name | Details |
|---|
| AGAV | END ITEM IDENTIFICATION | C13-2 AND TC13-2 CATAPULTS USED ON AIRCRAFT CARRIERS |
| MATT | MATERIAL SPECIFICATION | Metal alloy made from aluminum |
| CRTL | CRITICALITY CODE JUSTIFICATION REASONING | Fault tolerant system |
| FEAT | SPECIAL FEATURES OF THE ITEM | This item is used as part of a critical support system for the launch and recovery of aircraft. Its use is essential to the preservation of life or safety of operating personnel. |
| 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 ON THE ITEM | "CAGE CODE,PART NUMBER,CONTRACT NUMBER, SERIAL NUMBER" |
| ADAV | AVERAGE OVERALL DIAMETER OF THE ITEM | Nineteen point five inches nominal diameter |
| SUPP | III SUPPLEMENTARY FEATURES AND REQUIREMENTS FOR THE ITEM | "Material specifications: I/A/W ASTM B148 or ASTM B271/B271M, alloy C95500 (HT), with a minimum Brinell hardness of 200HBW. Surface roughness to be interpreted according to ASME B46.1." |
| SUPP | SUPPLEMENTARY FEATURES AND REQUIREMENTS FOR THE ITEM | "Material specifications: I/A/W ASTM B148 or ASTM B271/B271M, alloy C95500 (HT), with a minimum Brinell hardness of 200HBW. Surface roughness to be interpreted according to ASME B46.1." |
| ZZZK | SPECIFICATION/STANDARD DATA FOR THE ITEM | "ASME Y14.100 professional/industrial association standard and Y14.5M-1982 professional/industrial association standard" |
| SPCL | SPECIAL TEST FEATURES OF THE ITEM | Metal: Aluminum bronze; casting nominal stock size; unit weight: 488 pounds |
| ABHP | AVERAGE OVERALL LENGTH OF THE ITEM | Eleven point zero six inches nominal length |