NSN 5340-01-298-6511
Part Details | DOUBLE ANGLE BRACKET
5340-01-298-6511 A rigid item usually fabricated from flat material, forming two alternate or two adjacent interior angles, both which are less than 180 degrees (3.141 radians). It is designed to position, align, and/or support an item. It may be reinforced. See also BRACKET, ANGLE and BRACKET (1), MOUNTING.
Alternate Parts: 68A1130662024, 68A113066-2024, 5340-01-298-6511, 01-298-6511, 5340012986511, 012986511
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | APR 19, 1989 | 01-298-6511 | 20354 ( BRACKET, DOUBLE ANGLE ) |
REFERENCE DRAWINGS & PICTURES
CORNER RADIUS
NO HOLE
TWO HOLES
CORNER RADIUS
NO HOLE
TWO HOLES
DOUBLE ANGLE
Cross Reference | NSN 5340-01-298-6511
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68A113066-2024 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 5340-01-298-6511
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 5 COND 0 FED SPEC SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | DOUBLE ANGLE |
| FIRST LEG THICKNESS | 0.063 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.063 INCHES NOMINAL |
| CENTER SECTION THICKNESS | 0.063 INCHES NOMINAL |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| SECOND LEG ANGLE | 90.0 DEGREES NOMINAL |
| FIRST LEG STYLE | CORNER RADIUS |
| FIRST LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | CORNER RADIUS |
| SECOND LEG HOLE ARRANGEMENT STYLE | NO HOLE |
| MOUNTING HOLE TYPE | PLAIN |
| SPECIAL FEATURES | 1ST LEG HOLES MATE W/68A113026 & 68A113041,THE 2ND LEG MATES W/68A113003; ITEM IS HEAT TREATED TO T72 PER PS15554 WITH OPTIONAL 0.251 IN. CORNER RADIUS @ ALL EXTERNAL CORNERS UNLESS OTHERWISE NOTED; OA LG 2.800 IN.,OA WIDTH 1.850 IN. |
| END ITEM IDENTIFICATION | F-15 AIRCRAFT |