5998-01-453-8478 CIRCUIT CARD ASSEMBLY Index 1560-01-453-8480 WING ASSEMBLY,AIRCRAFT

National Stock Number:
5320-01-453-8479

Federal Supply Class:
5320

National Item Identification Number:
014538479

Description:
RIVET,BLIND

Detail:
An item consisting of two or more of the following components: stem, rivet body, sleeve, expander, bolt, and collar. It is a headed fastening device with the shank designed to be expanded by means of a separate or integral stem or mandrel, or bolt and expander. It is designed to be installed or expanded from one side only. Excludes NUT, BLIND ASSEMBLY.


Manufacturer Information:
3M1235D-4-276301THE BOEING COMPANY
CR2172-4-211815SPS TECHNOLOGIES, LLC
RV1301-4-253551ALLFAST FASTENING SYSTEMS, LLC


Techincal Specification:
COUNTERSINK ANGLE99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM
CRITICALITY CODE JUSTIFICATIONAGAV
EXPANSION DEVICESERRATED STEM-TYPE W
FASTENER LENGTH0.260 INCHES NOMINAL
GRIP LENGTH0.063 INCHES MINIMUM AND 0.125 INCHES MAXIMUM
HEAD STYLEFLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER)
HEAD MAJOR DIAMETER0.221 INCHES MINIMUM AND 0.229 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONQ-A-430 FED SPEC 13TH MATERIAL RESPONSE LOCKING RING
MATERIAL DOCUMENT AND CLASSIFICATIONQ-A-430 FED SPEC 13TH MATERIAL RESPONSE SLEEVE
MATERIALALUMINUM ALLOY 2017 SLEEVE
MATERIALALUMINUM ALLOY 5056 LOCKING RING
MATERIALALUMINUM ALLOY 7075 STEM
SHANK DIAMETER0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM
SHANK STYLESELF-PLUGGING MECHANICALLY LOCKED STEM
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OR MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE SLEEVE
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OR MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE STEM
SURFACE TREATMENTANODIZE OR CHROMATE SLEEVE
SURFACE TREATMENTANODIZE OR CHROMATE STEM


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