NSN 3040-01-430-2130
Part Details | MANUAL CONTROL LEVER
3040-01-430-2130 A rigid item of various shapes and cross-sections, specifically designed to manually actuate and/or regulate a variety of mechanisms. It usually has an integral handgrip, knob, or the like, or provisions for the mounting of the same. It may have accommodations for locking and/or positioning. The point of fulcrum may be an integral shaft perpendicular to the axis or a through hole to provide a definite means of securing, and usually has additional accommodation(s) for attachment of CONNECTING LINK,RIGID; WIRE ROPE ASSEMBLY,SINGLE LEG; and CLEVIS,ROD END; and the like. Excludes ARM (as modified); LEVER,REMOTE CONTROL; AND BELL CRANK.
Alternate Parts: 17P2C15531, 17P2C1553-1, 3040-01-430-2130, 01-430-2130, 3040014302130, 014302130
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | APR 24, 1996 | 01-430-2130 | 61447 ( LEVER, MANUAL CONTROL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 3040-01-430-2130
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17P2C1553-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 3040-01-430-2130
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | MAIN LANDING GEAR C-17 ACFT |
| MATERIAL | ALUMINUM |
| SURFACE TREATMENT | ANODIZE |
| OVERALL LENGTH | 7.300 INCHES NOMINAL |
| OVERALL WIDTH | 0.265 INCHES NOMINAL |
| SPECIAL FEATURES | ALUMINUM,ANODIZED;7.300 IN.LG:0.250IN. W.;PIVOT HOLE 0.4375 IN.DIA. |