NSN 5340-00-344-2956
Part Details | ANGLE BRACKET
5340-00-344-2956 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: 446169, 446169, 446169, 5340-00-344-2956, 00-344-2956, 5340003442956, 003442956
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-344-2956 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
END RADIUS
CORNER RADIUS
ONE HOLE
TWO HOLES
END RADIUS
CORNER RADIUS
ONE HOLE
TWO HOLES
OFFSET ANGLE
Cross Reference | NSN 5340-00-344-2956
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 446169 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 446169 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 446169 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-344-2956
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL COMP 410 |
| MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | OFFSET ANGLE |
| FIRST LEG THICKNESS | 0.062 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.062 INCHES NOMINAL |
| FIRST LEG ANGLE | 130.0 DEGREES NOMINAL |
| SECOND LEG OFFSET ANGLE | 80.9 DEGREES NOMINAL |
| FIRST LEG STYLE | END RADIUS |
| FIRST LEG WIDTH | 0.510 INCHES NOMINAL |
| FIRST LEG END RADIUS | 0.375 INCHES NOMINAL |
| SECOND LEG WIDTH | 1.509 INCHES NOMINAL |
| SECOND LEG CORNER RADIUS | 0.250 INCHES NOMINAL |
| FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| FIRST LEG HOLE DIAMETER | 0.224 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| SECOND LEG HOLE DIAMETER | 0.286 INCHES NOMINAL |
| SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.009 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | CORNER RADIUS |
| SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| FSC APPLICATION DATA | ENGINE,JET,AIRCRAFT |
| END ITEM IDENTIFICATION | CASE ASSEMBLY,TURBINE; W/S: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, STRATOFORTRESS B-52; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H) |