NSN 5340-00-808-1002
Part Details | ANGLE BRACKET
5340-00-808-1002 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: 39107944, 39-10794-4, 39107944, 39-10794-4, 421117, 421117, 5340-00-808-1002, 00-808-1002, 5340008081002, 008081002
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1962 | 00-808-1002 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
CORNER RADIUS
THREE HOLES
CORNER RADIUS
THREE HOLES
ANGLE
Cross Reference | NSN 5340-00-808-1002
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 39-10794-4 | 82918 | BOEING COMPANY, THEDBA BOEING |
| 39-10794-4 | 81205 | THE BOEING COMPANYDBA BOEING |
| 421117 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 421117 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-808-1002
| 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 | 0.730 INCHES NOMINAL |
| SECOND LEG LENGTH | 0.970 INCHES NOMINAL |
| FIRST LEG THICKNESS | 0.028 INCHES MINIMUM AND 0.034 INCHES MAXIMUM |
| SECOND LEG THICKNESS | 0.028 INCHES MINIMUM AND 0.034 INCHES MAXIMUM |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| SECOND LEG WIDTH | 4.220 INCHES NOMINAL |
| SECOND LEG CORNER RADIUS | 0.219 INCHES NOMINAL |
| FIRST LEG HOLE ARRANGEMENT STYLE | THREE HOLES |
| FIRST LEG HOLE DIAMETER | 0.339 INCHES MINIMUM AND 0.349 INCHES MAXIMUM |
| FIRST LEG DISTANCE BETWEEN LOWER HOLE CENTERS ALONG WIDTH | 1.919 INCHES NOMINAL |
| FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 0.031 INCHES NOMINAL |
| FIRST LEG DISTANCE BETWEEN FIRST AND SECOND HOLE CENTERS ALONG WIDTH | 0.959 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
| SECOND LEG STYLE | CORNER RADIUS |
| END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); AIRCRAFT, STRATOFORTRESS B-52; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H) |