NSN 5340-01-105-6679
Part Details | ANGLE BRACKET
5340-01-105-6679 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: ST9M580C15, ST9M580C1R, ST9M580C1LW, ST9M580AC1R, ST9M580103, ST9M580-103, ST9M580102, ST9M580-102, ST9M580C1R, ST9M580103, ST9M580-103, 10117638, ST9M580C1R, 5340-01-105-6679, 01-105-6679, 5340011056679, 011056679
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1981 | 01-105-6679 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
CORNER RADIUS
TWO HOLES
CORNER RADIUS
TWO HOLES
ANGLE
Cross Reference | NSN 5340-01-105-6679
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ST9M580C15 | 76301 | BOEING COMPANY, THEDBA BOEING |
| ST9M580C1R | 76301 | BOEING COMPANY, THEDBA BOEING |
| ST9M580C1LW | 76301 | BOEING COMPANY, THEDBA BOEING |
| ST9M580AC1R | 76301 | BOEING COMPANY, THEDBA BOEING |
| ST9M580-103 | 76301 | BOEING COMPANY, THEDBA BOEING |
| ST9M580-102 | 76301 | BOEING COMPANY, THEDBA BOEING |
| ST9M580C1R | 04967 | FASTENER SPECIALTY, INC. |
| ST9M580-103 | 04967 | FASTENER SPECIALTY, INC. |
| 10117638 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| ST9M580C1R | 59570 | TRICO MANUFACTURING INC. |
Technical Data | NSN 5340-01-105-6679
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 5,T81 FED SPEC SINGLE MATERIAL RESPONSE |
| SURFACE TREATMENT | PAINT |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE |
| STYLE DESIGNATOR | ANGLE |
| FIRST LEG LENGTH | 0.750 INCHES NOMINAL |
| SECOND LEG LENGTH | 0.750 INCHES NOMINAL |
| FIRST LEG THICKNESS | 0.050 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.050 INCHES NOMINAL |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| FIRST LEG STYLE | CORNER RADIUS |
| FIRST LEG WIDTH | 0.980 INCHES MINIMUM AND 1.020 INCHES MAXIMUM |
| FIRST LEG CORNER RADIUS | 0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM |
| SECOND LEG WIDTH | 0.980 INCHES MINIMUM AND 1.020 INCHES MAXIMUM |
| SECOND LEG CORNER RADIUS | 0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM |
| FIRST LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| FIRST LEG HOLE DIAMETER | 0.129 INCHES MINIMUM AND 0.134 INCHES MAXIMUM |
| FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 0.490 INCHES MINIMUM AND 0.510 INCHES MAXIMUM |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM |
| SECOND LEG HOLE DIAMETER | 0.220 INCHES MINIMUM AND 0.230 INCHES MAXIMUM |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.230 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | CORNER RADIUS |
| SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| END ITEM IDENTIFICATION | W/S: AIRCRAFT, HARRIER AV-8B; AIRCRAFT, EAGLE F-15; AIRCRAFT, HORNET F/A-18; F/A-18E/F HORNET AIRCRAFT; AVIATION ORDANCE; GUN SYSTEM, 25MM |