NSN 3040-01-418-8851
Part Details | REMOTE CONTROL LEVER
3040-01-418-8851 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: 3570158, 357015-8, 3040-01-418-8851, 01-418-8851, 3040014188851, 014188851
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 30 | SEP 07, 1995 | 01-418-8851 | 22099 ( LEVER, REMOTE CONTROL ) |
REFERENCE DRAWINGS & PICTURES
FLAT, TWO HOLE LINK END
Cross Reference | NSN 3040-01-418-8851
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 357015-8 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 3040-01-418-8851
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-18729, COND N MIL SPEC SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | FLAT, TWO HOLE LINK END |
| CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 7.680 INCHES NOMINAL |
| SHAFT END THICKNESS | 1.000 INCHES NOMINAL |
| LINK END THICKNESS | 0.172 INCHES NOMINAL |
| LINK END HOLE DIAMETER | 0.172 INCHES NOMINAL |
| SPECIAL FEATURES | 0.350 IN. WD NOTCH LOCATED 0.610 FROM SHAFT END |
| END ITEM IDENTIFICATION | WEAPONS SYSTEM AIRCRAFT, HERCULES C-130 |