NSN 9540-01-479-0438
Part Details | STRUCTURAL ANGLE
9540-01-479-0438 A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet.
Alternate Parts: HS1004AA04B0100, 9540-01-479-0438, 01-479-0438, 9540014790438, 014790438
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | OCT 06, 2000 | 01-479-0438 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-479-0438
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| HS1004AA04B0100 | 8V613 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9540-01-479-0438
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 11 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | K$DRL |
| LENGTH | 1.000 INCHES NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 0.750 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.062 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| END ITEM IDENTIFICATION | APACHE HELICOPTER |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | EXTRUDED ANGLE - UNEQUAL LEG, ALUMINUM ALLOY |