NSN 5340-00-385-9274
Part Details | ANGLE BRACKET
5340-00-385-9274 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: 4028799, 4028799, 5340-00-385-9274, 00-385-9274, 5340003859274, 003859274
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAR 25, 1974 | 00-385-9274 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
END RADIUS
ONE HOLE
TWO HOLES
END RADIUS
ONE HOLE
TWO HOLES
OFFSET ANGLE
Cross Reference | NSN 5340-00-385-9274
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4028799 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4028799 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-385-9274
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 NATIONAL SPEC SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | OFFSET ANGLE |
| FIRST LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| SECOND LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| FIRST LEG ANGLE | 0.1 RADIANS NOMINAL |
| FIRST LEG STYLE | END RADIUS |
| FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| FIRST LEG HOLE DIAMETER | 0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
| SECOND LEG HOLE DIAMETER | 0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM |
| SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 1.500 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.640 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| END ITEM IDENTIFICATION | W/S: AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ENGINE, AIRCRAFT, F100-PW-220 (F-15C/D/E) |