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" |
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" |