Item Name | Screw Close Tolerance |
Federal Supply Group (FSG) | Hardware and Abrasives |
Federal Supply Class (FSC) | 5305 Screws |
National Item Identification Number (NIIN) | 00-211-9039 (002119039) |
NCB Code | USA (00) |
Manufacturer | National Aerospace Standards Com, Apcom Inc, Air Industries Corp, Collins Engineering Corp, Nor Cal Supply Coinc, Sps Technologies Inc, Durham Aircraft Service Inc, Hi Shear Corporation, Lawrence Engineering And Supply Inc, F And C Sales Inc, Eriks Southwest Inc, Lisi Aerospace Canada Corp |
Part Number | Manufacturer | Item Name | Cage Code | RFQ |
---|---|---|---|---|
NAS1206-23D | national aerospace standards com | screw close tolerance | 80205 | RFQ |
NAS1206-23D | apcom inc | screw close tolerance | 50568 | RFQ |
NAS1206-23D | air industries corp | screw close tolerance | 08938 | RFQ |
NAS1206-23D | collins engineering corp | screw close tolerance | 71563 | RFQ |
NAS1206-23D | nor cal supply coinc | screw close tolerance | 07851 | RFQ |
NAS1206-23D | sps technologies inc | screw close tolerance | 80539 | RFQ |
NAS1206-23D | durham aircraft service inc | screw close tolerance | 82172 | RFQ |
NAS1206-23D | hi shear corporation | screw close tolerance | 73197 | RFQ |
NAS1206-23D | lawrence engineering and supply inc | screw close tolerance | 04348 | RFQ |
NAS1206-23D | f and c sales inc | screw close tolerance | 30902 | RFQ |
NAS1206-23D | eriks southwest inc | screw close tolerance | 30889 | RFQ |
NAS1206-23D | lisi aerospace canada corp | screw close tolerance | l4528 | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 3A |
AAJF | THREAD DIRECTION | RIGHT-HAND |
AASA | THREAD LENGTH | 0.366 INCHES MINIMUM AND 0.416 INCHES MAXIMUM |
AASB | FASTENER LENGTH | 1.814 INCHES MINIMUM AND 1.844 INCHES MAXIMUM |
AASK | HEAD STYLE | FLAT COUNTERSUNK |
AASL | HEAD DIAMETER | 0.704 INCHES MINIMUM AND 0.762 INCHES MAXIMUM |
AAUR | GRIP DIAMETER | 0.3735 INCHES MINIMUM AND 0.3745 INCHES MAXIMUM |
AAWB | SHANK UNTHREADED HOLE DIAMETER | 0.106 INCHES MINIMUM FIRST HOLE AND 0.116 INCHES MAXIMUM FIRST HOLE |
ABQZ | INTERNAL DRIVE STYLE | CROSS RECESS TYPE 1 |
AHYM | NOMINAL THREAD DIAMETER | 0.375 INCHES |
ANEE | GRIP LENGTH | 1.428 INCHES MINIMUM AND 1.448 INCHES MAXIMUM |
CMLP | THREAD QUANTITY PER INCH | 24 |
CQBC | MINIMUM TENSILE STRENGTH | 160000 POUNDS PER SQUARE INCH |
CQFM | HARDNESS RATING | 36.0 ROCKWELL C MINIMUM OVERALL AND 40.0 ROCKWELL C MAXIMUM OVERALL |
CRSQ | COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
CRZS | DISTANCE FROM HEAD LARGEST BEARING SURFACE TO SHANK HOLE CENTER | 1.684 INCHES MINIMUM FIRST HOLE AND 1.734 INCHES MAXIMUM FIRST HOLE |
MATT | MATERIAL | STEEL COMP 4140 OVERALL OR STEEL COMP E4340 OVERALL OR STEEL COMP 6150 OVERALL OR STEEL COMP 8735 OVERALL OR STEEL COMP 8740 OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5626 MIL SPEC 1ST MATERIAL RESPONSE OVERALL OR MIL-S-5000 MIL SPEC 2ND MATERIAL RESPONSE OVERALL OR MIL-S-8503 MIL SPEC 3RD MATERIAL RESPONSE OVERALL OR MIL-S-6098 MIL SPEC 4TH MATERIAL RESPONSE OVERALL OR MIL-S-6049 MIL SPEC 5TH MATE |
SFTT | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMATE OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416 TY 2 CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
THSD | THREAD SERIES DESIGNATOR | UNF |
ZZZK | SPECIFICATION/STANDARD DATA | 80205-NAS1206 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
Relevant Components for NSN - 5305-00-211-9039, 5305002119039 | ||||
5330-00-037-6893 (5330000376893) | 5307-00-803-5029 (5307008035029) | 5306-00-638-8373 (5306006388373) | 5330-01-185-7225 (5330011857225) | |
5365-00-089-1699 (5365000891699) | 5331-01-025-7783 (5331010257783) | 5330-01-362-7880 (5330013627880) | 5307-01-286-8388 (5307012868388) | |
5340-01-407-7865 (5340014077865) | 5340-01-609-2404 (5340016092404) | 5330-01-167-2303 (5330011672303) | 5340-01-145-4055 (5340011454055) | |
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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