NSN 4730-00-663-1393

Part Details | FLUID PASSAGE BOLT

4730-00-663-1393 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: NAS5515H, NAS551-5H, NAS5515H, NAS551-5H, NAS5515H, NAS551-5H, NAS5515H, NAS551-5H, NAS5515H, NAS551-5H, NAS5515H, NAS551-5H, NAS5515H, NAS551-5H, MILF5509, MIL-F-5509, NAS5515H, NAS551-5H, NAS5515, NAS551-5, NAS5515H, NAS551-5H, NAS5515H, NAS551-5H, AS4875, 4730-00-663-1393, 00-663-1393, 4730006631393, 006631393

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
47JAN 01, 196300-663-139318683 ( BOLT, FLUID PASSAGE )
REFERENCE DRAWINGS & PICTURES

RELIEVED

PLAIN

PLAIN

HEXAGON

Cross Reference | NSN 4730-00-663-1393
Part Number Cage Code Manufacturer
NAS551-5H34724ACRA AEROSPACE INC
NAS551-5H06581ALLAN AIRCRAFT SUPPLY CO, LLC
NAS551-5H71563COLLINS ENGINEERING CORP
NAS551-5H22995CROWN FITTING CO INC
NAS551-5H14798DESIGNED METAL CONNECTIONS, INC.DBA PERMASWAGE USA
NAS551-5H00624EATON-AEROQUIP LLC.DBA AEROSPACE GROUP
NAS551-5H14397FABER ENTERPRISES, INC.DIV FABER ENTERPRISE INC
MIL-F-550981349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
NAS551-5H80205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
NAS551-580205NATIONAL AEROSPACE STANDARDSCOMMITTEE AEROSPACE INDUSTRIES
NAS551-5H50948PARKER HANNIFIN CORPSTRATOFLEX DIV AIRCRAFT FITTINGS OPN
NAS551-5HR1120SATAIR A/S
AS487581343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 4730-00-663-1393
Characteristic Specifications
MATERIAL STEEL
BODY STYLE7 RELIEVED
CONCENTRIC HOLE DEPTH0.968 INCHES NOMINAL
CONCENTRIC HOLE DIAMETER0.295 INCHES NOMINAL
OVERALL LENGTH1.437 INCHES NOMINAL
FIRST DIAMETER FROM WRENCHING FEATURE0.498 INCHES NOMINAL
LENGTH FROM BEARING SURFACE OF WRENCHING FEATURE TO END OF FIRST DIAMETER0.875 INCHES NOMINAL
FIRST RADIAL FLUID HOLE DIAMETER0.339 INCHES NOMINAL
DISTANCE FROM FIRST RADIAL HOLE CENTER TO END OF BOLT0.812 INCHES NOMINAL
LENGTH FROM BEARING SURFACE OF WRENCHING FEATURE TO BOLT END1.250 INCHES NOMINAL
WRENCHING FEATURE HEIGHT0.172 INCHES NOMINAL
FIRST END CONNECTION TYPE THREADED EXTERNAL TUBE
FIRST END STYLE DESIGNATOR PLAIN
FIRST END THREAD SERIES DESIGNATOR UNF
FIRST END NOMINAL THREAD SIZE0.500 INCHES
FIRST END THREAD QUANTITY PER INCH20
FIRST END THREAD CLASS3A
FIRST END THREAD DIRECTION RIGHT-HAND
FIRST END THREAD LENGTH0.300 INCHES NOMINAL
WRENCHING FEATURE STYLE HEXAGON
WIDTH ACROSS FLATS0.750 INCHES NOMINAL
MINIMUM TENSILE STRENGTH125000 POUNDS PER SQUARE INCH
SPECIAL FEATURESGRUMMAN AEROSPACE CORP A10 AIRCRAFT
SPECIFICATION/STANDARD DATA80205-NAS551 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD AND 81343-AS4875 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD
END ITEM IDENTIFICATIONAIRCRAFT, HERCULES C-130