At NSN Unlimited, we maintain a large database of parts 1E-712, 60 1778 2024 T3511, 60-1778 2024-T3511, AMS QQ A 200 3, AMS-QQ-A-200 3 with NSN 9540-01-353-5552 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Transtar Metals Corp, Federal Specifications, Boeing Company The, Society Of Automotive Engineers Inc, Sae International. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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Alternative NSN: 9540-01-353-5552 |
Item Name: Angle Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013535552 |
NCB Code: USA (01) |
Manufacturers: Transtar Metals Corp , Federal Specifications , Boeing Company The , Society Of Automotive Engineers Inc , Sae International |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1E-712 | 9540-01-353-5552 | angle structural | transtar metals corp | Avl | RFQ |
1E-712 | 9540-01-353-5552 | angle structural | federal specifications | Avl | RFQ |
1E-712 | 9540-01-353-5552 | angle structural | boeing company the | Avl | RFQ |
60 1778 2024 T3511 | 9540-01-353-5552 | angle structural | transtar metals corp | Avl | RFQ |
60-1778 2024-T3511 | 9540-01-353-5552 | angle structural | federal specifications | Avl | RFQ |
60-1778 2024-T3511 | 9540-01-353-5552 | angle structural | boeing company the | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-353-5552 | angle structural | society of automotive engineers inc | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-353-5552 | angle structural | sae international | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-353-5552 | angle structural | boeing company the | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-353-5552 | angle structural | transtar metals corp | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-353-5552 | angle structural | federal specifications | Avl | RFQ |
QQ-A-200 3 | 9540-01-353-5552 | angle structural | transtar metals corp | Avl | RFQ |
QQ-A-200 3 | 9540-01-353-5552 | angle structural | federal specifications | Avl | RFQ |
QQ-A-200 3 | 9540-01-353-5552 | angle structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.750 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 1.750 INCHES NOMINAL |
ADXL | LEFT SIDE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | ANGLE |
AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
AJGM | OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.031 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.385 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBD | FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
CNBF | SECOND TIP INNER RADIUS | 0.062 INCHES NOMINAL |
CNQK | SECOND TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER |
AJGP | BASE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
CNBJ | FIRST TIP OUTER RADIUS | 0.062 INCHES NOMINAL |
CNBK | SECOND TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
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