NSN 5340-00-344-2951
Part Details | ANGLE BRACKET
5340-00-344-2951 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: 6511659867, 65-11659-867, 444538, 444538, 444538, 5340-00-344-2951, 00-344-2951, 5340003442951, 003442951
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-344-2951 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
END RADIUS
ONE HOLE
END RADIUS
ONE HOLE
ANGLE
Cross Reference | NSN 5340-00-344-2951
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 65-11659-867 | 82918 | BOEING COMPANY, THEDBA BOEING |
| 444538 | 82918 | BOEING COMPANY, THEDBA BOEING |
| 444538 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 444538 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-344-2951
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP 410 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5504 ASSN STD SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | ANGLE |
| FIRST LEG LENGTH | 0.690 INCHES MINIMUM AND 0.710 INCHES MAXIMUM |
| SECOND LEG LENGTH | 1.360 INCHES MINIMUM AND 1.380 INCHES MAXIMUM |
| FIRST LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM |
| SECOND LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| FIRST LEG STYLE | END RADIUS |
| FIRST LEG WIDTH | 0.625 INCHES MINIMUM AND 0.635 INCHES MAXIMUM |
| FIRST LEG END RADIUS | 0.469 INCHES MINIMUM AND 0.531 INCHES MAXIMUM |
| SECOND LEG WIDTH | 0.625 INCHES MINIMUM AND 0.635 INCHES MAXIMUM |
| SECOND LEG END RADIUS | 0.469 INCHES MINIMUM AND 0.531 INCHES MAXIMUM |
| FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| FIRST LEG HOLE DIAMETER | 0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.312 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.290 INCHES MINIMUM AND 0.310 INCHES MAXIMUM |
| SECOND LEG HOLE DIAMETER | 0.214 INCHES MINIMUM AND 0.224 INCHES MAXIMUM |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.312 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.290 INCHES MINIMUM AND 0.310 INCHES MAXIMUM |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | END RADIUS |
| SECOND LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT TF33-PW-102 (C0135E, EC-135H/K/P); ENGINE, AIRCRAFT, C-18A, EC-18B; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, AWACS, E-3A; AIRCRAFT, STRATOLIFTER C-135 |