NSN 5340-00-415-5313
Part Details | ANGLE BRACKET
5340-00-415-5313 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: 4033331, 4033331, 5340-00-415-5313, 00-415-5313, 5340004155313, 004155313
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAY 01, 1974 | 00-415-5313 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
END RADIUS
ONE HOLE
END RADIUS
ONE HOLE
ANGLE
Cross Reference | NSN 5340-00-415-5313
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4033331 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4033331 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-415-5313
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | ANGLE |
| FIRST LEG LENGTH | 0.800 INCHES NOMINAL |
| SECOND LEG LENGTH | 2.050 INCHES NOMINAL |
| FIRST LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.068 INCHES MAXIMUM |
| SECOND LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.068 INCHES MAXIMUM |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| SECOND LEG WIDTH | 0.600 INCHES NOMINAL |
| SECOND LEG END RADIUS | 0.300 INCHES NOMINAL |
| SECOND LEG HOLE DIAMETER | 0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.300 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.300 INCHES NOMINAL |
| SECOND LEG STYLE | END RADIUS |
| SECOND LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); SUPPORT EQUIPMENT, C-5 AIRCRAFT |