|
|
|
National Stock Number: 3040-01-183-3769
Federal Supply Class: 3040
National Item Identification Number: 011833769
Description: LEVER,REMOTE CONTROL
Detail: 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.
|
Manufacturer Information:
| 208-4061-3 | 72429 | MISSION SYSTEMS DAVENPORT INC. | | 232539-1 | F0553 | ZODIAC AEROTECHNICS |
|
Techincal Specification:
| BORE DIAMETER | 0.626 INCHES NOMINAL | | BORE LENGTH | 0.250 INCHES NOMINAL | | BORE TYPE | PLAIN STRAIGHT | | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 5.000 INCHES NOMINAL | | FEATURES PROVIDED | KEYWAY | | KEYWAY LENGTH | 0.103 INCHES NOMINAL | | KEYWAY WIDTH | 0.190 INCHES NOMINAL | | LINK END HOLE DIAMETER | 0.264 INCHES NOMINAL | | LINK END THICKNESS | 0.250 INCHES NOMINAL | | OVERALL WIDTH | 1.500 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5, T4 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SHAFT END THICKNESS | 0.250 INCHES NOMINAL | | SHAFT SECURING METHOD | KEYWAY | | STYLE DESIGNATOR | FLAT, ONE HOLE LINK END | | SURFACE TREATMENT | ANODIZE |
|
|