NSN 2990-00-363-8093
Part Details | REMOTE CONTROL LEVER
2990-00-363-8093 A rigid item usually in the form of an arm of various shapes and cross sections, containing two or more holes so spaced that one serves as a pivot with or without hubs and must have a definite means for securing to a shaft (such as threaded hole for set-screw, keyway(s), splines, serrations or some clamping device). The other hole(s) connect(s) to CONNECTING LINK, RIGID; WIRE ROPE ASSEMBLY, SINGLE LEG; or CLEVIS, ROD END; to provide transmission of movement to other parts of the mechanism. See also BELL CRANK. For manually operated items see LEVER, MANUAL CONTROL.
Alternate Parts: 2990003638093, B5151519, 5158432, 5154158BPC5151519, N24304PC2, NX12290PC2, 5154158BPC5151519, N24304PC2, NX12290PC2, K5151519, K-5151519, 5158432, 5151519, PC5151519, 5151519, 2990-00-363-8093, 00-363-8093, 2990003638093, 003638093
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 29 | JAN 01, 1963 | 00-363-8093 | 22099 ( LEVER, REMOTE CONTROL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2990-00-363-8093
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2990003638093 | A00AM | E.C.A ETABLISSEMENT CENTRALDESAPPROVISIONNEMENTS DES FORCES |
| B5151519 | 7U177 | FEDERAL-MOGUL CORPORATIONDBA FEDERAL-MOGUL DIV FP DIESEL |
| 5158432 | 24617 | GENERAL MOTORS CORP |
| 5154158BPC5151519 | 24617 | GENERAL MOTORS CORP |
| N24304PC2 | 24617 | GENERAL MOTORS CORP |
| NX12290PC2 | 24617 | GENERAL MOTORS CORP |
| 5154158BPC5151519 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| N24304PC2 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| NX12290PC2 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| K-5151519 | 18954 | KORODY-COLYER CORPA CR INDUSTRIES CO |
| 5158432 | 72582 | MTU AMERICA INC. |
| 5151519 | 72582 | MTU AMERICA INC. |
| PC5151519 | C7432 | POWER COMPONENTS (DEUTSCHLAND) GMBH |
| 5151519 | K4285 | TEREX EQUIPMENT LIMITEDDBA CONSTRUCTION EQUIPMENT |
Technical Data | NSN 2990-00-363-8093
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | BSAE 1117$CSAE 1118 AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ALL MATERIAL RESPONSES |
| OVERALL WIDTH | 0.875 INCHES NOMINAL |
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.250 INCHES NOMINAL |
| SHAFT END THICKNESS | 0.344 INCHES NOMINAL |
| LINK END THICKNESS | 0.319 INCHES MINIMUM AND 0.320 INCHES MAXIMUM |
| LINK END HOLE DIAMETER | 0.311 INCHES MINIMUM AND 0.314 INCHES MAXIMUM |
| BORE TYPE | PLAIN STRAIGHT |
| BORE DIAMETER | 0.500 INCHES MINIMUM AND 0.503 INCHES MAXIMUM |
| BORE LENGTH | 0.500 INCHES NOMINAL |
| SHAFT SECURING METHOD | KEYWAY |
| FEATURES PROVIDED | KEYWAY |
| KEYWAY WIDTH | 0.095 INCHES MINIMUM AND 0.105 INCHES MAXIMUM |
| KEYWAY LENGTH | 0.094 INCHES NOMINAL |
| SPECIAL FEATURES | OFFSET HEIGHT: 0.375 IN. NOMINAL |
| END ITEM IDENTIFICATION | GRUMMAN AIRCRAFT,MODEL A10 AND GENERAL MOTORS CORP,LIGHT ARMORED VEHICLE MODEL LAV-25; GOVERNOR, DIESEL ENGINE |