Part Details | SOLID RIVET
5320-00-754-0822 A headed fastening device having a smooth solid shank designed to have the shank end upset after insertion.
Alternate Parts: AS125740, AN470AD45, AN470AD4-5, AN470AD45, AN470AD4-5, AS125740, 3M269AD45, 3M269AD4-5, 413719077, 413719-077, 110050D45, 110-050D4-5, 3M269AD45, 3M269AD4-5, 5320007540822, AS125740, 2780024051, 278-002-4051, 252AD45, 25-2AD4-5, GHN1000321, GHN10003-21, MS20470AD45, MS20470AD4-5, MS20470AD45, MS20470AD4-5, AS125740, 10123831, 2780024051, 278-002-4051, 9461312305, 946131-2305, 1761500505, 17-615-00-505, 939.17.81.236, AS125740, 58322, 126832, 2161034P30, 216-1034P30, AS125740, AS125740, 413719077, 413719-077, AS125740, 790373824, 7903738-24, 7330019025, 733-00190-25, 5320-00-754-0822, 00-754-0822, 5320007540822, 007540822
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1962 | 00-754-0822 | 00861 ( RIVET, SOLID ) |
REFERENCE DRAWINGS & PICTURES
BRAZIER
STRAIGHT
Cross Reference | NSN 5320-00-754-0822
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AS125740 | 33823 | ADAMS INDUSTRIES INCA SUB OF BANNER INDUSTRIES INC |
| AN470AD4-5 | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| AN470AD4-5 | 81352 | AIR FORCE-NAVY AERONAUTICALSPECIFICATIONS |
| AS125740 | 53551 | ALLFAST FASTENING SYSTEMS, LLC |
| 3M269AD4-5 | 53551 | ALLFAST FASTENING SYSTEMS, LLC |
| 413719-077 | 02964 | AMERICAN STERILIZER COMPANYDBA AMSCO STERILITY ASSURANCE |
| 110-050D4-5 | 97499 | BELL HELICOPTER TEXTRON INC.DBA BELL HELICOPTER |
| 3M269AD4-5 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 5320007540822 | SCY13 | E.C.A ETABLISSEMENTCENTRALD'APPROVISIONNEMENT DES |
| AS125740 | 82224 | JOHN HASSALL, INC.DIV JOHN HASSALL INC. |
| 278-002-4051 | C1834 | KONTRON AG |
| 25-2AD4-5 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| GHN10003-21 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| MS20470AD4-5 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS20470AD4-5 | 80205 | NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES |
| AS125740 | 03827 | NATIONAL BIRD CONTROL LABORATORIES |
| 10123831 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| 278-002-4051 | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 946131-2305 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| 17-615-00-505 | 78022 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
| 939.17.81.236 | S4080 | PILATUS AIRCRAFT LTD |
| AS125740 | 00198 | PRATT & WHITNEY CANADA CIE DIVPRATT& WHITNEY CANADA CORP. |
| 58322 | 00198 | PRATT & WHITNEY CANADA CIE DIVPRATT& WHITNEY CANADA CORP. |
| 126832 | 00198 | PRATT & WHITNEY CANADA CIE DIVPRATT& WHITNEY CANADA CORP. |
| 216-1034P30 | 49956 | RAYTHEON COMPANYDBA RAYTHEON |
| AS125740 | R1120 | SATAIR A/S |
| AS125740 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 413719-077 | 0NWN1 | STERIS CORPORATION |
| AS125740 | 30040 | TELECTRO SYSTEMS CORP |
| 7903738-24 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
| 733-00190-25 | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5320-00-754-0822
| Characteristic | Specifications |
|---|---|
| SHEAR STRENGTH | 26000 SINGLE POUNDS PER SQUARE INCH |
| HEAD STYLE | 8 BRAZIER |
| HEAD HEIGHT | 0.054 INCHES MINIMUM AND 0.064 INCHES MAXIMUM |
| HEAD MAJOR DIAMETER | 0.238 INCHES MINIMUM AND 0.262 INCHES MAXIMUM |
| SHANK STYLE | STRAIGHT |
| FASTENER LENGTH | 0.302 INCHES MINIMUM AND 0.322 INCHES MAXIMUM |
| SHANK DIAMETER | 0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM |
| GRIP LENGTH | 0.114 INCHES MINIMUM AND 0.134 INCHES MAXIMUM |
