Please fill out the form below for Bolt Shear and get a quote for part number NAS6314-42Y manufactured by National Aerospace Standards with NSN 5306015055845 and FSC 5306 Bolts please include required quantity along with expected turn around time. Our knowledgeable account manager will reply you shortly. Also check for the related parts for part number NAS6314-42Y. ASAP Aerospace distributes nose to tail NSN components, sub-assemblies, and assemblies for the aerospace and aviation industry.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5306-01-505-5845 Item Description: Bolt Shear | 5306 | 015055845 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| NAS6314-42Y | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAUR | GRIP DIAMETER | 0.8740 INCHES MINIMUM AND 0.9042 INCHES MAXIMUM |
| AATB | WIDTH BETWEEN FLATS | 1.239 INCHES MINIMUM AND 1.252 INCHES MAXIMUM |
| CRZS | DISTANCE FROM HEAD LARGEST BEARING SURFACE TO SHANK HOLE CENTER | 3.138 INCHES MINIMUM AND 3.148 INCHES MAXIMUM FIRST HOLE |
| CMLP | THREAD QUANTITY PER INCH | 14 |
| AAWB | SHANK UNTHREADED HOLE DIAMETER | 0.141 INCHES MINIMUM AND 0.151 INCHES MAXIMUM FIRST HOLE |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416 TY2 CL2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | CADMIUM OVERALL |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| CQBC | MINIMUM TENSILE STRENGTH | 160000 POUNDS PER SQUARE INCH |
| AHYM | NOMINAL THREAD DIAMETER | 0.8750 INCHES |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5731 ASSN STD SINGLE MATERIAL RESPONSE OR AMS5737 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | BOLT,TENSION,HEX HEAD,CLOSE TOLERANCE,A286 CRES,SHORT THR |
| THSD | THREAD SERIES DESIGNATOR | UNJF |
| ANEE | GRIP LENGTH | 2.615 INCHES MINIMUM AND 2.635 INCHES MAXIMUM |
| AAJD | THREAD CLASS | 3A |
| AGAV | III END ITEM IDENTIFICATION | C-135 AIRCRAFT |
| AASK | HEAD STYLE | DISHED HEXAGON |
| AASB | FASTENER LENGTH | 3.369 INCHES MINIMUM AND 3.399 INCHES MAXIMUM |
| MATT | MATERIAL | IRON ALLOY 660 OVERALL |
| AASA | THREAD LENGTH | 0.759 INCHES NOMINAL |
| AASU | HEAD HEIGHT | 0.438 INCHES MINIMUM AND 0.453 INCHES MAXIMUM |
| NAS-1-5600-1 | NAS-1-R100-1 | NAS-10 | NAS-10-47R0-5 |
| NAS 1006-78A | NAS 1010-26A | NAS 1023D4 | NAS 1057 |
| NAS 1063 | NAS-1075 OHM 5 | NAS 1091A30H | NAS 1099-16 |
| NAS 1099-18 | NAS 1142-4 | NAS 1142-6 | NAS 1143-12 |
| 5-83032-4 | NAS502-6MILG3278 | NAS73-12-007 | NAS77-6-18P |
| NAS6603L3 | NAS6603-68 | NAS1305-72H | NAS6605-72 |
| NAS6605H72 | NAS6604-71 | NAS6604H71 | NAS1054-6-4 |
| NAS77-6-18P | NAS1305-72H | NAS73-12-007 | NAS6605-72 |
| NAS6603L3 | NAS6603-68 | NAS502-6MILG3278 | 5-83032-4 |
| NAS6604H71 | NAS1054-6-4 | NAS6604-71 | NAS6605H72 |
| 5305000000094 | 5305000011366 | 5305000011367 | 5305000011568 |
| 5305000011569 | 5305000011837 | 5305000011918 | 5305000011926 |
| 5305000011948 | 5305000011963 | 5305000012011 | 5305000012012 |
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