NSN 5306-00-151-1426, (5306001511426) - Bolt Machine Parts List
Bolt Machine parts under NSN 5306-00-151-1426 manufactured by Aeronautical Standards Group, E C A Etablissement Central, Embraer Aircraft, Embraer Aviation International, Embraer S A. All NSN items provided by NSN Parts Hub are compliant with fit, form, and functionality according to parameters set by the DLA. With over 3 billion new and obsolete parts in our searchable database, you can find your required part number of NSN 5306-00-151-1426 with ease when you use NSN Parts Hub as your purchasing partner. We maintain an unmatched supply-chain network with trusted MFRs and verified PMAs and are the only distributor with a No China Sourcing pledge. Do you require part numbers other than AN4-6A, 5306001511426, 2010255, 145-540-90206, 8812928? Related NSN parts are listed below for your convenience.
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| Alternative NSN: 5306001511426 |
| Item Name: Bolt Machine |
| Federal Supply Class (FSC): 5306 Bolts |
| NIIN: 001511426 |
| NCB Code: USA (00) |
| Manufacturers: Aeronautical Standards Group , E C A Etablissement Central , Embraer Aircraft , Embraer Aviation International , Embraer S A , Honeywell International Inc , National Aerospace Standards , Picatinny Arsenal , Raytheon Technical Services Company , Rockwell Collins Inc , Scandinavian Manufacturing Scama Ab , Sps Technologies Ltd , Surface Combustion Inc |
Characteristics Data of NSN 5306001511426
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | THREAD CLASS | 3A |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASA | THREAD LENGTH | 0.397 INCHES MINIMUM |
| AASB | FASTENER LENGTH | 0.781 INCHES NOMINAL |
| AASK | HEAD STYLE | HEXAGON |
| AASU | HEAD HEIGHT | 0.140 INCHES MINIMUM AND 0.172 INCHES MAXIMUM |
| AATB | WIDTH BETWEEN FLATS | 0.428 INCHES MINIMUM AND 0.440 INCHES MAXIMUM |
| AGAV | III END ITEM IDENTIFICATION | W/S:SUPPORT EQUIPMENT, B-1 AIRCRAFT; TEST CONSOLES, MINI-SACE; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, T56-A-7/15 (C-130B/E/H/N/P); CLOSE IN WEAPON SYSTEM (CIWS-PHALANX); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-1 |
| AHYM | NOMINAL THREAD DIAMETER | 0.250 INCHES |
| ANEE | GRIP LENGTH | 0.383 INCHES NOMINAL |
| CBBL | FEATURES PROVIDED | FINISHED HEAD |
| CMLP | THREAD QUANTITY PER INCH | 28 |
| CQBC | MINIMUM TENSILE STRENGTH | 125000 POUNDS PER SQUARE INCH |
| CQFM | HARDNESS RATING | 26.0 ROCKWELL C MINIMUM OVERALL AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| MATT | MATERIAL | STEEL OVERALL |
| SFTT | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMATE OVERALL |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TYPE 2,CLASS 3 FED SPEC ALL TREATMENT RESPONSES OVERALL |
| THSD | THREAD SERIES DESIGNATOR | UNF |
5306-00-151-1426, 5306001511426 Search Related NSN Catalog
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