5340-01-370-9834 CLAMP,LOOP Index 5340-01-370-9836 CLAMP,LOOP

National Stock Number:
5340-01-370-9835

Federal Supply Class:
5340

National Item Identification Number:
013709835

Description:
CLAMP,LOOP

Detail:
A clamp designed to surround other item(s) such as cable(s), conduit(s), pipe(s), hose(s), or tube(s), and to fasten together or to another object or structure. Includes straight flexible items. For items specifically designed to clamp a hose to a connection to prevent leakage, see CLAMP, HOSE. See also HANGER, PIPE and CLIP, SPRING TENSION. For retaining straps with a bridge, see STRAP, RETAINING. Excludes CLAMP, ELECTRICAL; BAND, RETAINING; CLAMP (1), C; BRACKET PIPE.


Manufacturer Information:
5340PL08039749009HINSPEKTORAT WSPARCIA SIL ZBROJNYCH
5340PL17712399009HINSPEKTORAT WSPARCIA SIL ZBROJNYCH
ST2817-2052661RTX CORPORATION
ST2817-2077445RTX CORPORATION
TA10300016-2084971TA AEROSPACE CO


Techincal Specification:
STYLE DESIGNATORCLAMP & BRACKET
MATERIALSTEEL CORROSION RESISTING BAND
STEEL COMP 316 NUT
STEEL SCREW
RUBBER FLUOROSILICONE CLASS FQ OR
RUBBER SILICONE CLASS Q CUSHION
STEEL PIN/STUD
MATERIAL DOCUMENT AND CLASSIFICATIONAMS 5510 ASSN STD SINGLE MATERIAL RESPONSE BAND
ASTM B-525 ASSN STD SINGLE MATERIAL RESPONSE NUT
AMS 5525 ASSN STD SINGLE MATERIAL RESPONSE SCREW
PWA 36081,CAGEC 77445 MFR REF SINGLE MATERIAL RESPONSE OR
MIL-C-85052/3 MIL SPEC SINGLE MATERIAL RESPONSE CUSHION
AMS 5513 ASSN STD SINGLE MATERIAL RESPONSE PIN/STUD
OVERALL WIDTH0.500 INCHES NOMINAL
MATERIAL THICKNESS0.040 INCHES NOMINAL
CENTER TO CENTER DISTANCE BETWEEN FIRST AND SECOND HOLES1.250 INCHES NOMINAL
CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE1.133 INCHES MINIMUM AND
1.163 INCHES MAXIMUM
DISTANCE FROM LOOP CENTER TO TONGUE END1.528 INCHES NOMINAL
LOOP INSIDE DIAMETER1.250 INCHES NOMINAL
LUG HOLE DIAMETER0.204 INCHES NOMINAL
FASTENING DEVICE TYPESPRING TENSION
CRITICALITY CODE JUSTIFICATIONFEAT
SPECIAL FEATURESTORQUE SET HEAD SCREW;ONE LUG HOLE SLOTTED;INCLUDES WASHER. PART PERFORMS A CRITICAL APPLICATION IN THE ENGINE. IF THE PART WERE TO FAIL IT WOULD CONTRIBUTE TO TEH FAILURE OF OTHER SYSTEMS IN THE ENGINE


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