5340-00-828-1413 BRACKET,ANGLE Index 2915-00-828-1416 FUEL CONTROL,MAIN,TURBINE ENGINE

National Stock Number:
5340-00-828-1414

Federal Supply Class:
5340

National Item Identification Number:
008281414

Description:
BRACKET,ANGLE

Detail:
A ridge item, usually of flat material, formed into a dihedral angle (generally a right angle) which may be reinforced; it is designed to position, align, or support an item(s) in relation to another. Excludes BRACE (as modified); BRACKET (1), MOUNTING; and BRACKET, SHELF.


Manufacturer Information:
42871111449TURBO POWER & MARINE SYSTEM INC SUB OF UNITED TECHNOLOGIES CORP
42871177445RTX CORPORATION
65-11659-1182918THE BOEING COMPANY


Techincal Specification:
FIRST LEG ANGLE90.0 DEGREES NOMINAL
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.250 INCHES NOMINAL
FIRST LEG END RADIUS0.375 INCHES NOMINAL
FIRST LEG HOLE ARRANGEMENT STYLEONE HOLE
FIRST LEG HOLE DIAMETER0.219 INCHES NOMINAL
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.250 INCHES NOMINAL
FIRST LEG STYLEEND RADIUS
FIRST LEG THICKNESS0.059 INCHES NOMINAL
FIRST LEG WIDTH0.500 INCHES NOMINAL
FIRST LEG LENGTH0.750 INCHES NOMINAL
FSC APPLICATION DATAENGINE,ACFT,TURBO-FAN
MATERIAL DOCUMENT AND CLASSIFICATION66 FED STD SINGLE MATERIAL RESPONSE
MATERIALSTEEL COMP 410
SECOND LEG END RADIUS0.375 INCHES NOMINAL
SECOND LEG HOLE ARRANGEMENT STYLEONE HOLE
SECOND LEG HOLE DIAMETER0.281 INCHES NOMINAL
SECOND LEG LENGTH1.000 INCHES NOMINAL
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.250 INCHES NOMINAL
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.250 INCHES NOMINAL
SECOND LEG THICKNESS0.059 INCHES NOMINAL
SECOND LEG WIDTH0.500 INCHES NOMINAL
SECOND LEG RELATIONSHIP TO FIRST LEGNOT IDENTICAL
SECOND LEG STYLEEND RADIUS
STYLE DESIGNATORANGLE
SURFACE TREATMENTPASSIVATE


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