| BORE DIAMETER | 17.0000 MILLIMETERS NOMINAL |
| BORE SHAPE | STRAIGHT |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| INTERNAL CLEARANCE | 0.0005 INCHES MINIMUM RADIAL AND 0.0009 INCHES MAXIMUM RADIAL |
| LOAD DIRECTION | RADIAL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6416 ASSN STD SINGLE MATERIAL RESPONSE RETAINER |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6440 ASSN STD SINGLE MATERIAL RESPONSE INNER RING |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6440 ASSN STD SINGLE MATERIAL RESPONSE OUTER RING |
| MATERIAL DOCUMENT AND CLASSIFICATION | SAE 5100 ASSN STD SINGLE MATERIAL RESPONSE BALL |
| MATERIAL | COPPER ALLOY RETAINER |
| MATERIAL | STEEL BALL |
| MATERIAL | STEEL COMP E52100 INNER RING |
| MATERIAL | STEEL COMP E52100 OUTER RING |
| OVERALL OUTSIDE DIAMETER | 30.0000 MILLIMETERS NOMINAL |
| OVERALL WIDTH | 7.0 MILLIMETERS NOMINAL |
| PRECIOUS MATERIAL AND LOCATION | PLATE SILVER |
| PRECIOUS MATERIAL | SILVER |
| RETAINER FABRICATION METHOD | MACHINED |
| SPECIAL FEATURES | ITEM OF SUPPLY IS ESSENTIAL TO WEAPON SYSTEM PERFORMANCE AND OPERATION. A FAILURE COULD CAUSE CATASTROPHIC OR CRITITCAL FAILURE RESULTING IN THE LOSS OF OR SERIOUS DAMAGE TO THE AIRCRAFT OR WEAPON SYSTEM OR AN UNCOMMANDED ENGINE SHUTDOWN THAT JEOPARDIZES SAFETY. |
| SPECIAL TEST FEATURES | MATERIAL: OUTER RING: AMS 6440, HARDNESS: ROCKWELL C-58 MININUM OR EQUIVALENT; INNER RING: AMS 6440, HARDNESS: ROCKWELL C-58 MINIMUM OR EQUIVALENT; BALLS-AMS 6440, HARDNESS: ROCKWELL C-58 MINIMUM OR EQUIVALENT; CAGE: AMS 4616 FORGED SILICON BRONZE; SILVER PLATE AMS 2412 NO STRIKE METAL; REQUIRED BAKE: 475-500 DEGREES FAHRENHEIT FOR 2HRS TO CHECK BOND-PLATE .0005-.0015" THICK ON LAND RIDING SURFACES AND BALL POCKETS; BALLS AND RINGS MUST BE STABILIZED FOR MINIMUM DISTORTION AT 400 DEGREES FAHRENHEIT |
| STANDARD TOLERANCE DESIGNATION | ABEC NO.5 |
| STYLE DESIGNATOR | NON-LOADING GROOVE, NON-SEPARABLE |
| SURFACE FINISH | GROUND |