Part Number: 20-131-1 | Manufacturer: Houston Precision Fastener L L C |
NSN: 5306-01-618-6781 | Item Name : Bolt Shear |
CAGE Code: 1VSL7 | FSC: 5306 Bolts |
Alternate P/N : 201311 |
Part number 20-131-1, which is associated with national stock number 5306016186781, is now available in our stock. 20-131-1, which is a Bolt Shear is manufactured by Houston Precision Fastener L L C. This part has an FSC code of 5306 Bolts.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5306-01-618-6781 Item Description: Bolt Shear | 5306 | 016186781 | 0 | N | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
20-131-1 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 3A |
AAJF | THREAD DIRECTION | RIGHT-HAND |
AASA | THREAD LENGTH | 0.960 INCHES NOMINAL |
AASB | FASTENER LENGTH | 1.435 INCHES MINIMUM AND 1.465 INCHES MAXIMUM |
AASK | HEAD STYLE | HEXAGON |
AASU | HEAD HEIGHT | 0.188 INCHES MINIMUM AND 0.203 INCHES MAXIMUM |
AATB | WIDTH BETWEEN FLATS | 0.554 INCHES MINIMUM AND 0.564 INCHES MAXIMUM |
AAUB | HOLE DIAMETER | 0.070 INCHES MINIMUM AND 0.080 INCHES MAXIMUM |
AAUR | GRIP DIAMETER | 0.3735 INCHES MINIMUM AND 0.3745 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | MODEL CODE FOR THE V-22 AIRCRAFT |
AHYM | NOMINAL THREAD DIAMETER | 0.375 INCHES |
ANEE | GRIP LENGTH | 0.365 INCHES MINIMUM AND 0.385 INCHES MAXIMUM |
ASXK | HOLE QUANTITY | 3 |
BQDM | HOLE TYPE | DRILLED |
CBBL | FEATURES PROVIDED | DRY FILM LUBRICANT |
CMLP | THREAD QUANTITY PER INCH | 24 |
CQBC | MINIMUM TENSILE STRENGTH | 260000 POUNDS PER SQUARE INCH |
CRHC | HOLE CONFIGURATION STYLE | HEXAGON CORNERS |
CSYT | CHAMFER ANGLE | 10.0 DEGREES MINIMUM AND 20.0 DEGREES MAXIMUM |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BOLT,HEX HEAD, SPECIAL THREAD LENGTHS, COBALT-NICKEL ALLOY MP35N, 260 KSI FTU, (MAST NUT APPLICATIONS) |
FEAT | SPECIAL FEATURES | THIS BOLT INTENDED TO BE USED FOR PURPOSE OF PROVIDING PRELOAD IN CONJUNCTION WITH A MAST NUT IN ROTOR SYSTEMS SHOULD NOT BE USED IN STANDARD SHEAR/TENSION APPLICATIONS; SEE DRAWING FOR THREAD AND PITCH DETAILS |
MATT | MATERIAL | COBALT COMP MP-35-N OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5844 (UNS R30035) ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
THSD | THREAD SERIES DESIGNATOR | UNJF |
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