NSN 9540-01-444-4375 of Beam Structural - Parts Details
Alternative NSN: 9540014444375 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014444375 |
NCB Code: USA (01) |
Manufacturers: Triumph Actuation Systems |
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 CVC10012-187GA under NSN 9540-01-444-4375 of Beam Structural manufactured by Triumph Actuation Systems.
Federal Supply Class of NSN 9540-01-444-4375 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-444-4375, 9540014444375
-
Part No Manufacturer Item Name QTY RFQ CVC10012-187GA Triumph Actuation Systems beam structural Avl RFQ
Characteristics Data of NSN 9540014444375MRC Criteria Characteristic AARN FABRICATION METHOD EXTRUDED ABKW OVERALL HEIGHT 3.250 INCHES NOMINAL ABRY LENGTH 12.000 FEET NOMINAL ADXR LEFT SIDE TOP FLANGE THICKNESS 0.410 INCHES NOMINAL ADXS RIGHT SIDE TOP FLANGE THICKNESS 0.410 INCHES NOMINAL AGTA BASIC SHAPE STYLE T SHAPE AJJP LEG THICKNESS 0.200 INCHES NOMINAL BPXD LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.420 INCHES NOMINAL BPXG RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.740 INCHES NOMINAL BPXJ FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG 0.188 INCHES NOMINAL BPXL FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG 0.188 INCHES NOMINAL BQJG TOP FLANGE WIDTH 3.160 INCHES NOMINAL CMZY FIRST TIP STYLE SQUARE END CNQJ SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL CNQL THIRD TIP RELATIONSHIP TO PRECEDING TIPS IDENTICAL W/FIRST TIP CRZC RIGHT TOP INSIDE ANGLE 96.0 DEGREES NOMINAL CSMZ LEFT TOP INSIDE ANGLE 84.0 DEGREES NOMINAL HEAT HEAT TREATMENT ANNEALED MATL MATERIAL TITANIUM ALLOY, MIL-T-81556, COMPOSITION AB-1 (6AL-4V) ZZZT NONDEFINITIVE SPEC/STD DATA COMPOSITION AB-1 (6AL-4V) AND CONDITION ANNEALED
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 3.250 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.410 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.410 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.200 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.420 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.740 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.160 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 96.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 84.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | ANNEALED |
MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMPOSITION AB-1 (6AL-4V) |
ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 (6AL-4V) AND CONDITION ANNEALED |