Mfg Part Number: NAS342 18 2024T8511 | Alternate P/N: NAS342182024T8511 | NSN : 9540-01-495-6444 |
NIIN : 014956444 | CAGE Code : 80205 | Manufacturer: Nat Aerospace Std |
Item Name : Angle Structural | FSC : 9540 Structural Shapes Nonferrous Metal |
Aviation Gamut, owned and operated by ASAP Semiconductor, is an all-inclusive purchasing platform for hard-to-find and in-demand parts NAS342 18 2024T8511 and components pertaining to the civil aviation, defense, aerospace, industrial, and electronic markets. An NSN is a 13-digit numeric code that serves to identify 'standardized material items of supply' as they have been recognized by all NATO countries and the United States Department of Defense. As such, we have an inventory of more than two billion new and obsolete parts, among which is an unparalleled selection of NSN parts and much more. This includes items such as Angle Structural NAS342 18 2024T8511 from manufacturer Nat Aerospace Std and many more, all of which are available with short lead times and competitive prices. For NSN parts, Aviation Gamut is the ultimate source.
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MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 0.750 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 1.500 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXL | LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | ANGLE |
AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL |
AJGM | OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.010 INCHES NOMINAL |
AJGP | BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FEAT | SPECIAL FEATURES | END VARIATIONS OBTAINABLE BY SPECIFING CORNER RADII |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
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