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National Stock Number:
5325-01-422-9478
Federal Supply Class:
5325
National Item Identification Number:
014229478
Description:
STUD ASSEMBLY,TURNLOCK FASTENER
Detail:
A STUD, TURNLOCK FASTENER over which may be assembled an EYELET, TURNLOCK FASTENER. Stud(s) without cam slots or cam lead threads are provided with a crosspin or eared nut for locking with the mating RECEPTACLE, TURNLOCK FASTENER. May be spring loaded. For like items having a threaded fastener, see SCREW ASSEMBLY, PANEL or SCREW, PANEL FASTENER.
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Manufacturer Information:
| 2700-11 | 71286 | HOWMET GLOBAL FASTENING SYSTEMS INC | | 55131-111 | F0210 | AIRBUS HELICOPTERS (ETS DEMARIGNANE) | | 55131-111 | F5442 | AIRBUS GROUP SAS |
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Techincal Specification:
| MATERIAL | STEEL COMP 4037 OVERALL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS6300 ASSN STD SINGLE MATERIAL RESPONSE OR | | ASTMA331 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | | SURFACE TREATMENT | CADMIUM AND | | CHROMATE OVERALL | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416 TYPE2 CLASS2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL | | TURNLOCK STUD HEAD STYLE | STUD HEAD | | DIAMETER | 0.256 INCHES MAXIMUM | | WIDTH ACROSS FLATS | 0.244 INCHES NOMINAL | | STUD HEAD HEIGHT | 0.076 INCHES NOMINAL | | STUD ASSEMBLY STYLE | STUD ASSEMBLY | | EYELET OUTSIDE DIAMETER | 0.250 INCHES MAXIMUM | | EYELET LENGTH | 0.328 INCHES NOMINAL | | MATERIAL ACCOMMODATED THICKNESS | 0.330 INCHES MINIMUM AND | | 0.359 INCHES MAXIMUM | | SPECIAL FEATURES | OVERALL ASSEMBLY LENGTH 0.910 |
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