|
|
|
National Stock Number:
9540-01-419-2017
Federal Supply Class:
9540
National Item Identification Number:
014192017
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:
| 10135-1201 | 29321 | TRANSTAR METALS CORP | | AMS-QQ-A-200/3 | 0U583 | SAE INTERNATIONAL | | NF9540-ASTM B221 | 14153 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA | | AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | | AND10135-1201 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD |
|
Techincal Specification:
| BASE FLANGE THICKNESS | 0.078 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.117 INCHES NOMINAL | | FIRST TIP RADIUS | 0.078 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.078 INCHES NOMINAL | | LENGTH | 12.000 FEET NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 2024 | | NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER | | OVERALL HEIGHT | 0.875 INCHES NOMINAL | | OVERALL WIDTH | 1.250 INCHES NOMINAL | | SECOND TIP DIAMETER | 0.234 INCHES NOMINAL | | SECOND TIP RADIUS | 0.117 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP STYLE | UPPER BULBOUS | | WEIGHT PER UNIT MEASURE | 2.760 POUNDS PER PIECE |
|