NSN 5340-01-144-0115
Part Details | MANUAL CONTROL LEVER
5340-01-144-0115 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: 74A8006112029, 74A800611-2029, 5340-01-144-0115, 01-144-0115, 5340011440115, 011440115
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | DEC 13, 1982 | 01-144-0115 | 61447 ( LEVER, MANUAL CONTROL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5340-01-144-0115
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 74A800611-2029 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 5340-01-144-0115
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367, COMP 7075 COND T7351 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 18.025 INCHES NOMINAL |
| SPECIAL FEATURES | QUADRANT ASSEMBLY,POWER CONTROL,AFT COCKPIT |