NSN 1710-01-483-0702 · NIIN 014830702 · FSC 1710
NO DASHES 1710014830702
In Stock
GUIDE,PISTON ASSY
Aircraft Landing Equipment
Application: C13-2 AND TC13-2 CATAPULTS (AIRCRAFT CARRIERS)
Technical characteristics
11 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES NOMINAL 11.06 |
| ADAV | OVERALL DIAMETER | INCHES NOMINAL 19.50 |
| AGAV | END ITEM IDENTIFICATION | C13-2 AND TC13-2 CATAPULTS (AIRCRAFT CARRIERS) |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | GUIDE PISTON ASSEMBLY LAUNCHING ENGINE |
| FEAT | SPECIAL FEATURES | 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; ITEM IS CRITICAL APPLICATION ITEM (CAI) |
| MARK | SPECIAL MARKINGS | CAGE CODE,PART NUMBER,CONTRACT NUMBER, SERIAL NUMBER |
| MATT | MATERIAL | ALUMINUM ALLOY |
| SPCL | SPECIAL TEST FEATURES | MATERIAL: ALUMINUM BRONZE; CASTING: NOMINAL STOCK SIZE; UNIT WEIGHT: 488LBS |
| SUPP | SUPPLEMENTARY FEATURES | MATERIAL SHALL BE I/A/W 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 I/A/W ASME B46.1 |
| ZZZK | SPECIFICATION/STANDARD DATA | PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD 05047-AS-E Y14.100 AND PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD 05047-Y14.5--1982 |
Cross-references
10 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.