Item Name | Stud Continuous Thread |
Federal Supply Group (FSG) | Hardware and Abrasives |
Federal Supply Class (FSC) | 5307 Studs |
National Item Identification Number (NIIN) | 01-003-9459 (010039459) |
NCB Code | USA (01) |
Manufacturer | Harris Corporation, Rockwell Collins Aerospace |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
314319-001 | harris corporation | stud continuous thread | RFQ |
312-3500-000 | rockwell collins aerospace | stud continuous thread | RFQ |
P312-0116-000 | rockwell collins aerospace | stud continuous thread | RFQ |
P312-3500-000 | rockwell collins aerospace | stud continuous thread | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 2A |
AAJF | THREAD DIRECTION | RIGHT-HAND |
ABHP | OVERALL LENGTH | 0.734 INCHES MINIMUM AND 0.766 INCHES MAXIMUM |
CMLP | THREAD QUANTITY PER INCH | 56 |
CQJX | NOMINAL THREAD SIZE | 0.086 INCHES |
MATT | MATERIAL | COPPER ALLOY 360 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-B-626 FED SPEC SINGLE MATERIAL RESPONSE |
SFTT | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMATE OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2 CL 1 FED SPEC SINGLE TREATMENT RESPONSE OVERALL OR QQ-P-416,TY 2 CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL OR QQ-P-416,TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
THSD | THREAD SERIES DESIGNATOR | UNC |
Relevant Components for NSN - 5307-01-003-9459, 5307010039459 | ||||
5305-00-151-0390 (5305001510390) | 5305-00-162-0212 (5305001620212) | 5330-01-021-6193 (5330010216193) | 5306-01-667-2305 (5306016672305) | |
5305-00-702-7578 (5305007027578) | 5306-01-467-0619 (5306014670619) | 5340-14-507-0973 (5340145070973) | 5330-01-545-5049 (5330015455049) | |
5331-01-433-9967 (5331014339967) | 5330-01-176-0563 (5330011760563) | 5330-20-001-0516 (5330200010516) | 5305-00-550-9932 (5305005509932) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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