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National Stock Number:
9540-00-147-7721
Federal Supply Class:
9540
National Item Identification Number:
001477721
Description:
CHANNEL,STRUCTURAL
Detail:
A STRUCTURAL SHAPE FABRICATED FROM A FERROUS OR NONFERROUS MATERIAL AND HAS A FLANGE EXTENDING USUALLY AT RIGHT ANGLES IN THE SAME DIRECTION FROM EACH EDGE OF A WEB AND/OR RESEMBLING THE LETTER U IN CROSS-SECTIONAL FORM.
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Manufacturer Information:
| 1019047 | 18355 | THE BOEING COMPANY | | 1019047 | 88277 | THE BOEING COMPANY | | 12845 | 01634 | ALUMINUM CO OF AMERICA | | 19150 | 77783 | ALCOA/REYNOLDS METALS COMPANY | | 60-1482 | 29321 | TRANSTAR METALS CORP | | AMS-QQ-A-200/3 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | PA7915 | 06012 | TRANSTAR METALS CORP | | QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | | S221 | 71379 | CESSNA AIRCRAFT COMPANY | | S221 | 7EK50 | TEXTRON AVIATION INC |
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Techincal Specification:
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL | | BASIC SHAPE STYLE | CHANNEL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE RIGHT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE HEIGHT | 1.000 INCHES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.156 INCHES NOMINAL | | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | | OVERALL WIDTH | 1.000 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 2024 | | NONDEFINITIVE SPEC/STD DATA | T-3511 TEMPER | | RIGHT SIDE FLANGE HEIGHT | 1.000 INCHES NOMINAL | | RIGHT SIDE FLANGE THICKNESS | 0.156 INCHES NOMINAL | | RIGHT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | | WEIGHT PER UNIT MEASURE | 0.490 POUNDS PER LINEAR FOOT |
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