NSN 4730-00-717-2246

Part Details | FLUID PASSAGE BOLT

4730-00-717-2246 A boltlike item having a concentric hole along the longitudinal centerline which may extend a part or the full length of the item. It has a hole(s) perpendicular to the axis, joining or passing through the concentric hole along the longitudinal centerline. The item is designed to distribute fluid, air, or lubricant through its body to a mating item, such as a CONNECTOR, MULTIPLE, FLUID PRESSURE LINE, bearing(s), bushing(s), or the like. The item must be capable of attaching to a block fitting and/or a tubing line or be designed to accommodate a FITTING, LUBRICATION. Excludes BOLT, INTERNALLY RELIEVED BODY; BLEEDER VALVE, HYDRAULIC SYSTEM; and BUSHING, MACHINE THREAD. See also PIN, VEHICULAR LEAF SPRING SHACKLE.

Alternate Parts: 7M1304J1, 7M130-4J1, 7M1304C, 7M130-4C, 7M1304J1, 7M130-4J1, 7M1304J1, 7M130-4J1, 7M1304J1, 7M130-4J1, 7M1304J1, 7M130-4J1, 7M1304J1, 7M130-4J1, MILF5509, MIL-F-5509, NAS5514H, NAS551-4H, 7M1304J1, 7M130-4J1, 7M1304J1, 7M130-4J1, AS4875, 7M1304J1, 7M130-4J1, 4730-00-717-2246, 00-717-2246, 4730007172246, 007172246

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
47FEB 09, 196800-717-224618683 ( BOLT, FLUID PASSAGE )
REFERENCE DRAWINGS & PICTURES

RELIEVED

INVERTED FLARE

INVERTED FLARE

HEXAGON

Cross Reference | NSN 4730-00-717-2246
Part Number Cage Code Manufacturer
7M130-4J106581ALLAN AIRCRAFT SUPPLY CO, LLC
7M130-4C76301BOEING COMPANY, THEDBA BOEING
7M130-4J176301BOEING COMPANY, THEDBA BOEING
7M130-4J122995CROWN FITTING CO INC
7M130-4J114798DESIGNED METAL CONNECTIONS, INC.DBA PERMASWAGE USA
7M130-4J100624EATON-AEROQUIP LLC.DBA AEROSPACE GROUP
7M130-4J113899HYDRO FITTING MANUFACTURINGCORPORATION
MIL-F-550981349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
NAS551-4H80205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
7M130-4J152930NELSON AERO SPACE, INC.
7M130-4J1R1120SATAIR A/S
AS487581343SOCIETY OF AUTOMOTIVE ENGINEERS INC
7M130-4J101673SPS TECHNOLOGIES, LLCDBA AIRDROME PRECISION COMPONENTS
Technical Data | NSN 4730-00-717-2246
Characteristic Specifications
MATERIAL STEEL COMP 304
SURFACE TREATMENT PASSIVATE
BODY STYLE7 RELIEVED
CONCENTRIC HOLE DEPTH0.937 INCHES NOMINAL
CONCENTRIC HOLE DIAMETER0.172 INCHES NOMINAL
OVERALL LENGTH1.375 INCHES NOMINAL
FIRST DIAMETER FROM WRENCHING FEATURE0.435 INCHES NOMINAL
LENGTH FROM BEARING SURFACE OF WRENCHING FEATURE TO END OF FIRST DIAMETER0.781 INCHES NOMINAL
FIRST RADIAL FLUID HOLE DIAMETER0.172 INCHES NOMINAL
DISTANCE FROM FIRST RADIAL HOLE CENTER TO END OF BOLT0.796 INCHES NOMINAL
LENGTH FROM BEARING SURFACE OF WRENCHING FEATURE TO BOLT END1.187 INCHES NOMINAL
WRENCHING FEATURE HEIGHT0.188 INCHES NOMINAL
FIRST END CONNECTION TYPE THREADED EXTERNAL TUBE
FIRST END STYLE DESIGNATOR INVERTED FLARE
FIRST END SEAT ANGLE45.0 DEGREES NOMINAL
FIRST END THREAD SERIES DESIGNATOR UNF
FIRST END NOMINAL THREAD SIZE0.437 INCHES
FIRST END THREAD QUANTITY PER INCH20
FIRST END THREAD CLASS3A
FIRST END THREAD DIRECTION RIGHT-HAND
FIRST END THREAD LENGTH0.406 INCHES NOMINAL
WRENCHING FEATURE STYLE HEXAGON
WIDTH ACROSS FLATS0.688 INCHES NOMINAL
SPECIAL FEATURESWEAPONS SYSTEM ESSENTIAL; FITS 1/4 INCH O.D. TUBE; HAS LOCKWIRE HOLE; STANDARD REFERS TO ITEM AS BOLT UNIVERSAL FITTING
SPECIFICATION/STANDARD DATA81343-AS4875 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD
CRITICALITY CODE JUSTIFICATIONFEAT
END ITEM IDENTIFICATIONAIRCRAFT, AH-1W, F-4, F-15, A-6E, C-135, T-38, AH-1J