NSN 5340-00-939-3521
Part Details | ANGLE BRACKET
5340-00-939-3521 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.
Alternate Parts: 524464, 524464, 524464, 524464, 524464, 524464, 524464, 524464, 5340-00-939-3521, 00-939-3521, 5340009393521, 009393521
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | NOV 16, 1965 | 00-939-3521 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
SQUARE
NO HOLE
ONE HOLE
SQUARE
NO HOLE
ONE HOLE
ANGLE
Cross Reference | NSN 5340-00-939-3521
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 524464 | 05457 | BRITISH AEROSPACE NORTH AMERICA INC |
| 524464 | 26389 | DYNAMIC METAL PRODUCTS CO INC |
| 524464 | 1J4P3 | PARADIGM MANCHESTER INC.DBA PARADIGM PRECISION |
| 524464 | 26065 | PARMAC INC |
| 524464 | 79043 | THE UNITED TOOL AND DIE COMPANY |
| 524464 | S0554 | TOKYO JUDOGI KOGYO CO. |
| 524464 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 524464 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-939-3521
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4901 ASSN STD SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | ANGLE |
| FIRST LEG LENGTH | 0.710 INCHES NOMINAL |
| SECOND LEG LENGTH | 0.780 INCHES NOMINAL |
| FIRST LEG THICKNESS | 0.062 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.062 INCHES NOMINAL |
| FIRST LEG ANGLE | 84.0 DEGREES NOMINAL |
| FIRST LEG STYLE | SQUARE |
| FIRST LEG WIDTH | 1.100 INCHES NOMINAL |
| SECOND LEG WIDTH | 1.100 INCHES NOMINAL |
| FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| FIRST LEG HOLE DIAMETER | 0.221 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.550 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.220 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | SQUARE |
| SECOND LEG HOLE ARRANGEMENT STYLE | NO HOLE |
| FSC APPLICATION DATA | AFTERBURNER,ENGINE AIRCRAFT |