6625-01-147-7679 LEAD,ELECTRICAL Index 5935-01-147-7681 BACKSHELL,ELECTRICAL CONNECTOR

National Stock Number:
4730-01-147-7680

Federal Supply Class:
4730

National Item Identification Number:
011477680

Description:
ELBOW,TUBE

Detail:
A fitting that forms an angle of less than 180 degrees (3.141 radians) from a straight flow. Both connecting ends have machine threads (straight threads other than pipe or hose series) designed to accommodate a tube or is unthreaded and designed to accommodate a tube. It may have side or heel inlet(s). See also ELBOW, PIPE and CONNECTOR, MULTIPLE, FLUID PRESSURE LINE.


Manufacturer Information:
10108772A486GNIMIKKEISTOKESKUS NCB FINLAND
7M14876301THE BOEING COMPANY
7M148V1001673SPS TECHNOLOGIES, LLC
7M148V1006581ALLAN AIRCRAFT SUPPLY CO., LLC
7M148V1014397FABER ENTERPRISES, INC.
7M148V1014798DESIGNED METAL CONNECTIONS INC
7M148V101V757WESCO AIRCRAFT HARDWARE CORP.
7M148V102N935BOEING DISTRIBUTION SERVICES X, INC.
7M148V1052930NELSON AERO SPACE, INC.
7M148V1061KM5JIT INDUSTRIES, INC. DBA JIT MILITARY SALES DIV JIT MILITARY SALES
7M148V1076301THE BOEING COMPANY


Techincal Specification:
CONNECTION STYLESWIVEL NUT, FLARE (TUBE) STYLE 3 OPTIONAL END 1ST END
CONNECTION TYPETHREADED EXTERNAL TUBE 2ND END
CONNECTION TYPETHREADED INTERNAL TUBE 1ST END
CONNECTION STYLEFLARED (TUBE) 2ND END
FLOW ANGLE90.0 DEGREES
LEG LENGTH1.000 INCHES NOMINAL 1ST END
LEG LENGTH1.453 INCHES NOMINAL 2ND END
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-225/6 T6 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-225/6 T851 FED SPEC SINGLE MATERIAL RESPONSE NUT
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-367,T6 FED SPEC SINGLE MATERIAL RESPONSE ELBOW
MATERIALALUMINUM ALLOY 2014 ELBOW
MATERIALALUMINUM ALLOY 2024 NUT
MAXIMUM OPERATING PRESSURE3000.0 POUNDS PER SQUARE INCH SINGLE RESPONSE
MEDIA FOR WHICH DESIGNEDHYDRAULIC FLUID SINGLE RESPONSE
NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED0.625 INCHES ALL ENDS
NOMINAL THREAD SIZE0.875 INCHES ALL ENDS
SPECIAL FEATURES37 DEG SEALING SURFACE SHALL BE FREE OF ANODIZE AND ALODINED PER MIL-C-5541,CLASS 1A
SEAT ANGLE37.0 DEGREES ALL ENDS
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-C-83488,CLASS 3,TYPE 2 MIL SPEC 1ST TREATMENT RESPONSE OVERALL
SURFACE TREATMENTALUMINUM OR CHROMATE OVERALL
THREAD CLASS3A 2ND END
THREAD CLASS3B 1ST END
THREAD SERIES DESIGNATORUNJF ALL ENDS


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