NSN 5340-00-425-9299
Part Details | ANGLE BRACKET
5340-00-425-9299 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: 4042430, 4042430, 5340-00-425-9299, 00-425-9299, 5340004259299, 004259299
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAY 04, 1974 | 00-425-9299 | 16900 ( BRACKET, ANGLE ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
ONE SLOT
ANGLE
ONE SLOT
ANGLE
Cross Reference | NSN 5340-00-425-9299
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4042430 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4042430 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5340-00-425-9299
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE |
| STYLE DESIGNATOR | ANGLE |
| FIRST LEG LENGTH | 2.495 INCHES NOMINAL |
| SECOND LEG LENGTH | 2.595 INCHES NOMINAL |
| FIRST LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| SECOND LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
| FIRST LEG STYLE | ANGLE |
| FIRST LEG HOLE ARRANGEMENT STYLE | ONE SLOT |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.300 INCHES NOMINAL |
| FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.300 INCHES NOMINAL |
| FIRST LEG SLOT LENGTH | 0.290 INCHES MINIMUM AND 0.310 INCHES MAXIMUM |
| FIRST LEG SLOT WIDTH | 0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | W/S:AIRCRAFT, EAGLE F-15; SUPPORT EQUIPMENT, C-5 AIRCRAFT; ENGINE, AIRCRAFT, F1000-PW-200 (F-16A/B/C/D); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); AIRCRAFT, F-16 |