NSN 5340-01-255-6823
Part Details | DOUBLE ANGLE BRACKET
5340-01-255-6823 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: 68A1131192001, 68A113119-2001, 5340-01-255-6823, 01-255-6823, 5340012556823, 012556823
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAY 23, 1987 | 01-255-6823 | 20354 ( BRACKET, DOUBLE ANGLE ) |
REFERENCE DRAWINGS & PICTURES
ADJACENT ANGLES
Cross Reference | NSN 5340-01-255-6823
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 68A113119-2001 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 5340-01-255-6823
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 13 COND 0 FED SPEC SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | ADJACENT ANGLES |
| FIRST LEG THICKNESS | 0.100 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.100 INCHES NOMINAL |
| CENTER SECTION THICKNESS | 0.100 INCHES NOMINAL |
| FIRST LEG ANGLE | 33.5 DEGREES NOMINAL |
| SECOND LEG ANGLE | 88.0 DEGREES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SPECIAL FEATURES | 1ST LEG HAS 3 HOLES DIA 0.2495 TO 0.2517 IN. THAT MATES W/68A113091 OR 68A113132,68A113070,68A113004 OR 68A113135 AND 2 HOLES FOR 0.250 IN. TAPER LOK PINS MATING W/68A113004 OR 68A113135 AND 68A112107; CNTR SECTION HAS 3 HOLES DIA 0.2495 TO 0.2517 IN. MATING W/68A113091 OR 68A113132,IS BUP 91 DEG ON 1 END AND 87 DEG ON OPPOSITE END; 2ND LEG HAS 1O HOLES DIA 0.2495 TO 0.2517,5 HOLES MATING W/68A113091 OR 68A113132 AND 5 HOLES MATING W/68A113091 OR 68A113132,68A112107 AND 68A113070 AND HAS 0.750 IN. FLG BUP 90 DEG |