NSN 5320-01-478-7254

Part Details | PIN-RIVET COLLAR

5320-01-478-7254 A soft metal or nonmetal sleeve, designed to mate with a PIN-RIVET. It may include an external wrenching facility which breaks off at a perdetermined torque to form a head.

Alternate Parts: HL1828AW, HL182-8AW, HS56138, HS5613-8, HL1828AW, HL182-8AW, HL1828AW, HL182-8AW, HS56138, HS5613-8, HL1828AW, HL182-8AW, 5320-01-478-7254, 01-478-7254, 5320014787254, 014787254

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53SEP 25, 200001-478-725467166 ( COLLAR, PIN-RIVET )
REFERENCE DRAWINGS & PICTURES

THREADED (BREAK OFF) TYPE

Cross Reference | NSN 5320-01-478-7254
Part Number Cage Code Manufacturer
HL182-8AW92215ARCONIC GLOBAL FASTENERS & RINGS,INC.
HS5613-88V613BOEING COMPANY, THEDBA BOEING
HL182-8AW73197HI-SHEAR CORPORATION
HL182-8AWL4528LISI AEROSPACE CANADA CORPDIV HI SHEAR HOLDINGS INC
HS5613-802731MCDONNELL DOUGLAS HELICOPTER CO INC
HL182-8AW56878SPS TECHNOLOGIES, LLCDBA AEROSPACE DIVISION
Technical Data | NSN 5320-01-478-7254
Characteristic Specifications
COLLAR STYLE THREADED (BREAK OFF) TYPE
COLLAR OUTSIDE DIAMETER0.465 INCHES MINIMUM AND 0.475 INCHES MAXIMUM
COLLAR OVERALL HEIGHT0.570 INCHES NOMINAL
COLLAR INSIDE DIAMETER0.270 INCHES NOMINAL
THREAD SERIES DESIGNATOR UNJF
NOMINAL THREAD SIZE0.250 INCHES
THREAD CLASS3B
THREAD QUANTITY PER INCH28
THREAD DIRECTION RIGHT-HAND
LUBRICATION CETYL ALCOHOL
SPECIAL FEATURESHEAT TREAT COLLAR AGE TO T6 CONDITION PER MIL-H-6088 AND WASHER TO AGE H1025 FOR 17-4PH, AGE TO TH1050 CONDITION FOR 17-7PH AND 15-7MO PER MIL-H-6875;NO LUBRICANT ON WASHER;COLOR FINISH ANODIZE COLOR BROWN;GO THREAD GAGE PENETRATION SHALL BE 3/4 ON ONE REVOLUTION MINIMUM AFTER THREAD LOCK;SURFACE TEXTURE 125 MICROINCHES PER ANSI B46.1-1978;DIMENTIONS APPLY AFTER FINISH;DISIGNED FOR USE WITH PROTRUDING SHEAR HEAD AND 100 DEG FLUSH SHEAR HEAD PINS;COLLAR SHALL BE USED WITH ALLUMINUM STRUCTURAL MATERIAL ONLY AT TEMP NO EXCEEDING 350 DEG F;FOR USE ON SLOPED SURFACES UP TO 7 DEG MAX ON STANDARD AND 1/64 OVERSIZE PINS
END ITEM IDENTIFICATIONHELICOPTER,ATTACK