NSN 5340-00-075-4899
Part Details | ANGLE BRACKET
5340-00-075-4899 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: 487990, 487990, 3P50004131, 3P50004-131, 487990, 487990, 5340-00-075-4899, 00-075-4899, 5340000754899, 000754899
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-075-4899 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
END RADIUS
CORNER RADIUS
ONE HOLE
THREE HOLES
END RADIUS
CORNER RADIUS
ONE HOLE
THREE HOLES
ANGLE
Cross Reference | NSN 5340-00-075-4899
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 487990 | 59420 | DYNAMIC GUNVER TECHNOLOGIES LLC |
| 487990 | 03730 | GOULD E A AND CO |
| 3P50004-131 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 487990 | 1J4P3 | PARADIGM MANCHESTER INC.DBA PARADIGM PRECISION |
| 487990 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-075-4899
| Characteristic | Specifications |
|---|---|
| MATERIAL | 0$DST8630 |
| MATERIAL DOCUMENT AND CLASSIFICATION | BAMS 6350$CAMS 6355 AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ALL MATERIAL RESPONSES |
| SURFACE TREATMENT | CADMIUM |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | AMS 2400 ASSN STD SINGLE TREATMENT RESPONSE |
| STYLE DESIGNATOR | ANGLE |
| FIRST LEG LENGTH | 0.900 INCHES NOMINAL |
| SECOND LEG LENGTH | 1.631 INCHES NOMINAL |
| FIRST LEG THICKNESS | 0.160 INCHES NOMINAL |
| SECOND LEG THICKNESS | 0.160 INCHES NOMINAL |
| FIRST LEG ANGLE | 159.0 DEGREES NOMINAL |
| FIRST LEG STYLE | END RADIUS |
| FIRST LEG WIDTH | 0.750 INCHES NOMINAL |
| FIRST LEG END RADIUS | 0.375 INCHES NOMINAL |
| SECOND LEG WIDTH | 1.300 INCHES NOMINAL |
| SECOND LEG CORNER RADIUS | 0.281 INCHES NOMINAL |
| SECOND LEG END RADIUS | 0.380 INCHES NOMINAL |
| 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 | 0.375 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.375 INCHES NOMINAL |
| SECOND LEG HOLE DIAMETER | 0.339 INCHES MINIMUM AND 0.349 INCHES MAXIMUM |
| SECOND LEG DISTANCE BETWEEN FIRST AND SECOND HOLE CENTERS ALONG WIDTH | 0.857 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.884 INCHES NOMINAL |
| SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.374 INCHES NOMINAL |
| SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| SECOND LEG STYLE | CORNER RADIUS |
| SECOND LEG HOLE ARRANGEMENT STYLE | THREE HOLES |
| SPECIAL FEATURES | LEFT HAND |
| END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B) |
