|
|
|
National Stock Number:
9540-00-145-8429
Federal Supply Class:
9540
National Item Identification Number:
001458429
Description:
ANGLE,STRUCTURAL
Detail:
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.
|
Manufacturer Information:
| 1114111 | 18355 | THE BOEING COMPANY | | 1114111 | 88277 | THE BOEING COMPANY | | AND10134-0701 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP RADIUS | 0.063 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED | | LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL HEIGHT | 0.625 INCHES NOMINAL | | OVERALL WIDTH | 0.875 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | NONDEFINITIVE SPEC/STD DATA | T4 TEMPER | | SECOND TIP RADIUS | 0.063 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 0.110 POUNDS PER LINEAR FOOT |
|