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National Stock Number:
5365-00-856-7295
Federal Supply Class:
5365
National Item Identification Number:
008567295
Description:
RING,EXTERNALLY THREADED
Detail:
A cylindrically shaped item with a concentric bore and a peripheral thread over its entire length or over a portion thereof. One face is drilled, slotted, knurled, or has projecting lugs for installation and/or removal purposes. Excludes RETAINER, OPTICAL ELEMENT.
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Manufacturer Information:
| 114H4034-1 | 77272 | THE BOEING COMPANY | | 114H4034-1 | 81205 | THE BOEING COMPANY | | 114H4043-1 | 27541 | TRANSAERO, INC. | | 114H4043-1 | 33068 | TRIUMPH ACTUATION SYSTEMS - CONNECTICUT, LLC |
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Techincal Specification:
| MATERIAL | ALUMINUM ALLOY 2024 | | SURFACE TREATMENT | ANODIZE | | OVERALL LENGTH | 0.560 INCHES NOMINAL | | CASEHARDENING INDICATOR | NOT CASEHARDENED | | DRIVE TYPE | DRILLED FACE | | ACCOMMODATION TYPE AND QUANTITY | 4 HOLES | | DIAMETER | 0.188 INCHES NOMINAL | | DEPTH | 0.370 INCHES NOMINAL | | ANGLE BETWEEN ACCOMMODATIONS IN DEG | 90.0 | | RADIUS FROM GEOMETRIC AXIS TO ACCOMMODATION | 0.756 INCHES NOMINAL | | THREAD SIZE | 2 IN.-16 | | SCREW THREAD SERIES DESIGNATOR | UNEF | | THREAD CLASS | 3A | | THREAD DIRECTION | RIGHT-HAND | | BEVELED THREAD | INCLUDED | | THREAD LOCATION | BOTH ENDS | | BORE SHAPE | STRAIGHT | | BORE DIAMETER | 1.093 INCHES NOMINAL | | BORE ANNULAR INTERNAL SERRATION | NOT INCLUDED | | BORE EDGE PROCESS | CHAMFERED | | PROCESS END LOCATION | END OPPOSITE DRIVE END | | CHAMFER ANGLE IN DEG | 45.0 | | CHAMFER LENGTH | 0.030 INCHES NOMINAL | | SETSCREW LOCKING NOTCH | NOT INCLUDED | | FSC APPLICATION DATA | DRIVE MECHANISM,HELICOPTER | | THE MANUFACTURERS DATA | | | MANUFACTURERS CODE | 77272 | | DESIGN CONTROL REFERENCE | 114H4034-1 |
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