5340-00-999-3992 CLIP,SPRING TENSION Index 5340-00-999-3994 CLIP,SPRING TENSION

National Stock Number:
5340-00-999-3993

Federal Supply Class:
5340

National Item Identification Number:
009993993

Description:
CLIP,SPRING TENSION

Detail:
A preformed item of semirigid material designed to retain, position, fasten, or support other items, such as cable(s), access cover(s), by its own inherent spring action. It may be fastened to a structure by bolt(s), clip(s), screw(s), and the like. For items conducting electric current, see CLIP, ELECTRICAL or CLAMP, ELECTRICAL. For items which partially surround an item, see STRAP, RETAINING. For items which entirely surround an item and do not have inherent spring tension, see CLAMP, LOOP. See also CLIP, RETAINING. Do not use if a more specific item name is available.


Manufacturer Information:
100-300-6-999378ATLEE OF DELAWARE, INCORPORATED
457-5720A486GNIMIKKEISTOKESKUS NCB FINLAND
6010-4-1CC91506AUGAT INC
M24066/2-22180205NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE
M24066/2-22181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MIL-C-24066/281349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MS17160-12196906MILITARY STANDARDS PROMULGATED BY MILITARY DEPARTMENTS UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MS24066-2-02181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
NASM24066/280205NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE


Techincal Specification:
DISTANCE FROM LOOP CENTER TO END0.223 INCHES NOMINAL
LENGTH0.410 INCHES NOMINAL
LOOP/HOLDING DIMENSION0.375 INCHES NOMINAL
OVERALL HEIGHT0.460 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-C-533 FED SPEC ALL MATERIAL RESPONSES OVERALL
MATERIAL THICKNESS0.018 INCHES NOMINAL
MATERIALCOPPER ALLOY 170 OR COPPER ALLOY 172 OVERALL
MOUNTING METHODUNTHREADED HOLE
WIDTH0.750 INCHES NOMINAL
SURFACE TREATMENTCADMIUM AND CHROMATE OVERALL


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