NSN 3040-01-422-5526
Part Details | REMOTE CONTROL LEVER
3040-01-422-5526 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: 17P1F61981, 17P1F6198-1, 3040-01-422-5526, 01-422-5526, 3040014225526, 014225526
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | DEC 04, 1995 | 01-422-5526 | 22099 ( LEVER, REMOTE CONTROL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 3040-01-422-5526
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17P1F6198-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 3040-01-422-5526
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225 TO 9, ALLOY 7075, T7351 FED SPEC SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT | ANODIZE |
| OVERALL WIDTH | 0.834 INCHES NOMINAL |
| BORE TYPE | SERRATED |
| MAJOR DIAMETER | 0.195 INCHES NOMINAL |
| MINOR DIAMETER | 0.161 INCHES NOMINAL |
| SHAFT SECURING METHOD | SERRATIONS |
| FEATURES PROVIDED | COUNTERBORE |
| SERRATION QUANTITY | 21 |
| SPECIAL FEATURES | OFFSET HEIGHT: 0.065 IN. NOMINAL |
| END ITEM IDENTIFICATION | AIRCRAFT, AIRLIFTER C-17A |