NSN 9540-01-329-2168 of Angle Structural - Parts Details
Alternative NSN: 9540013292168 |
Item Name: Angle Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013292168 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications Promulgat , Boeing Company , Society Of Automotive Engineers Inc , Sae International , Transtar Metals Corp |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers QQ-A-200 3, LS043-0377, AMS-QQ-A-200 3, AMS QQ A 200 3, 60-6600 under NSN 9540-01-329-2168 of Angle Structural manufactured by Federal Specifications Promulgat, Boeing Company, Society Of Automotive Engineers Inc, Sae International, Transtar Metals Corp.
Federal Supply Class of NSN 9540-01-329-2168 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-329-2168, 9540013292168
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Part No Manufacturer Item Name QTY RFQ QQ-A-200 3 Federal Specifications Promulgat angle structural Avl RFQ LS043-0377 Boeing Company angle structural Avl RFQ AMS-QQ-A-200 3 Society Of Automotive Engineers Inc angle structural Avl RFQ AMS QQ A 200 3 Sae International angle structural Avl RFQ 60-6600 Transtar Metals Corp angle structural Avl RFQ
Characteristics Data of NSN 9540013292168MRC Criteria Characteristic ABKW OVERALL HEIGHT 1.800 INCHES NOMINAL ABMK OVERALL WIDTH 4.200 INCHES NOMINAL ABRY LENGTH 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM ADXL LEFT SIDE FLANGE THICKNESS 0.071 INCHES NOMINAL AGAV III END ITEM IDENTIFICATION B-1B AIRCRAFT AJGL FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE 0.125 INCHES NOMINAL AJGP BASE FLANGE THICKNESS 0.071 INCHES NOMINAL BRFD WEIGHT PER UNIT MEASURE 0.509 POUNDS PER LINEAR FOOT CMZY FIRST TIP STYLE SQUARE END CQHP LEFT INSIDE ANGLE 90.0 DEGREES NOMINAL HEAT HEAT TREATMENT T-3511 SOLUTION HEAT TREATED MATT MATERIAL ALUMINUM ALLOY 2024 AARN FABRICATION METHOD EXTRUDED MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE AGTA BASIC SHAPE STYLE ANGLE CNQJ SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL ZZZT NONDEFINITIVE SPEC/STD DATA T3511 TEMPER
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 1.800 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 4.200 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXL | LEFT SIDE FLANGE THICKNESS | 0.071 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | B-1B AIRCRAFT |
AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
AJGP | BASE FLANGE THICKNESS | 0.071 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.509 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
AARN | FABRICATION METHOD | EXTRUDED |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
AGTA | BASIC SHAPE STYLE | ANGLE |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER |