NSN 9540-00-720-4242 Angle Structural, Beam Structural manufactured by Sae International, Society Of Automotive Engineers Inc, Sikorsky Aircraft Corporation, Federal Specifications Promulgat is available within ASAP Part Service’s ready-to-ship inventory. Owned and operated by ASAP Semiconductor, ASAP Part Services has over 6 billion parts within its inventory including AMS QQ A 200 11, AMS-QQ-A-200 11, QQ-A-200 11. ASAP is committed to streamlining the parts procurement process for our customers. We make it easy for our customers to search through billions of parts to find the exact part they are looking for.
A dedicated ASAP account manager is ready to help solve any procurement issues or needs that a customer may have. As a company we are quick and responsive meaning we can deliver a part within an AOG timeframe. Quality control is at the center of all that we do. Each and every NSN 9540-00-720-4242 part is subject to numerous quality checks that are designed to screen out any part imperfections or validity issues. Subject a request for quote for NSN 9540-00-720-4242 part today and allow us to simplify your procurement process.
Alternative NSN: 9540-00-720-4242 |
Item Name:Angle Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NCB Code: USA (00) |
Manufacturers: Sae International , Society Of Automotive Engineers Inc , Sikorsky Aircraft Corporation , Federal Specifications Promulgat |
Sae International | Society Of Automotive Engineers Inc | Sikorsky Aircraft Corporation |
Federal Specifications Promulgat |
Part No Part No
|
Manufacturer NSN Parts
|
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
AMS QQ A 200 11 | Sae International | angle structural | Avl | RFQ |
AMS-QQ-A-200 11 | Society Of Automotive Engineers Inc | angle structural | Avl | RFQ |
AMS-QQ-A-200 11 | Sikorsky Aircraft Corporation | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | Federal Specifications Promulgat | angle structural | Avl | RFQ |
QQ-A-200 11 | Federal Specifications Promulgat | angle structural | Avl | RFQ |
QQ-A-200 11 | Sikorsky Aircraft Corporation | angle structural | Avl | RFQ |
QQ-A-200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
S6105-2111 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
S6105-2111 | Sikorsky Aircraft Corporation | beam structural | Avl | RFQ |
S6105-2111 | Federal Specifications Promulgat | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 2.250 INCHES NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.062 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 1.750 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.029 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 7075 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
SFTT | SURFACE TREATMENT | ANODIZE |
AARN | FABRICATION METHOD | EXTRUDED |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
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