NSN 9540-00-540-5941
Part Details | STRUCTURAL ANGLE
9540-00-540-5941 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: AND101330701, AND10133-0701, ASTM B221, 40304, S97, S101, AND101330701ASTM B2210, AND10133-0701/ASTM B221-0, QQA277, QQ-A-277, QQA20011, QQ-A-200/11, J219P108, 17157, HA359, 21326, 2-1326, 50669, 5773, AMSQQA20011 ALLOY 7075 TMPR, AMS-QQ-A-200/11 ALLOY 7075 TMPR, AMSQQA20011, AMS-QQ-A-200/11, AND101330701, AND10133-0701, AMS101330701, AMS10133-0701, AMSSTD184, AMS-STD-184, 101330701, 10133-0701, 9540-00-540-5941, 00-540-5941, 9540005405941, 005405941
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-540-5941 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-540-5941
Part Number | Cage Code | Manufacturer |
---|---|---|
AND10133-0701 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
40304 | 99267 | BOHN ALUMINUM AND BRASS CODIV OF GULF AND WESTERN MFG CO |
S97 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
S101 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
AND10133-0701/ASTM B221-0 | 14153 | DEFENSE LOGISTICS AGENCYDBA DEFENSE SUPPLY CENTER |
QQ-A-277 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
J219P108 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
17157 | 27610 | INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP |
HA359 | 10383 | KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT |
2-1326 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
50669 | 08588 | NATIONAL DISTILLERS AND CHEMICALCORP BRIDGEPORT BRASS CO DIV |
5773 | 01484 | REYNOLDS METALS CO |
AMS-QQ-A-200/11 ALLOY 7075 TMPR | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
AND10133-0701 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
AMS10133-0701 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
AMS-STD-184 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
10133-0701 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-00-540-5941
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | O-ANNEALED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.875 INCHES NOMINAL |
OVERALL WIDTH | 0.875 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.063 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.130 POUNDS PER LINEAR FOOT |