5325-01-356-0126 INSERT,PANEL FASTENER Index 5325-01-356-0128 INSERT,PANEL FASTENER

National Stock Number:
5325-01-356-0127

Federal Supply Class:
5325

National Item Identification Number:
013560127

Description:
INSERT,PANEL FASTENER

Detail:
An insert which must have a hole that may be internally threaded with a flange on one end. It may have an undercut on the end opposite the flange to provide a shoulder to allow for mating with another insert. Pre-assembled items will consist of an expansion sleeve and a body which may be flared. Internally threaded items may have a self-locking feature. Excludes INSERT, SCREW THREAD.


Manufacturer Information:
9D0127-3B425F88277THE BOEING COMPANY
SLP5216A3B42597393SPS TECHNOLOGIES LLC


Techincal Specification:
FLANGE DIAMETER0.688 INCHES NOMINAL0.688 INCHES NOMINAL
FLANGE THICKNESS0.017 INCHES MINIMUM AND 0.017 INCHES MINIMUM AND 0.022 INCHES MAXIMUM0.022 INCHES MAXIMUM
HOLE DIAMETER0.195 INCHES MINIMUM AND 0.195 INCHES MINIMUM AND 0.202 INCHES MAXIMUM0.202 INCHES MAXIMUM
HOLE TYPEUNTHREADED-COUNTERSUNKUNTHREADED-COUNTERSUNK
INSERT STYLEPROTRUDING FLANGEPROTRUDING FLANGE
MATERIAL ACCOMMODATED THICKNESS0.375 INCHES MINIMUM AND 0.375 INCHES MINIMUM AND 0.380 INCHES MAXIMUM0.380 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-Q-225/9 FED SPEC SINGLE MATERIAL RESPONSE OVERALL
MATERIALALUMINUM ALLOY 7075 OVERALL
SPECIAL FEATURES0.415 IN. MIN,0.435 IN. MAX,LENGTH; 0.562 IN. WIDTH ACROSS FLAT ON FLANGE0.415 IN. MIN,0.435 IN. MAX,LENGTH; 0.562 IN. WIDTH ACROSS FLAT ON FLANGE
SHOULDER DIAMETER0.374 INCHES MAXIMUM0.374 INCHES MAXIMUM
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-A-8625,TY 1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL
SURFACE TREATMENTANODIZE OVERALL


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