Mfg Part Number: CVC10012-220GA
Alternate P/N: CVC10012220GA
NSN : 9540-01-441-0089
NIIN : 014410089
CAGE Code : 80378
Manufacturer: Triumph Aerostructures Llc
Item Name : Beam Structural
Here at Internet For Aviation, we have CVC10012-220GA Beam Structural from Triumph Aerostructures Llc, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific CVC10012-220GA to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-441-0089 Item Description: Beam Structural | 9540 | 014410089 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
CVC10012-220GA | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 3.630 INCHES NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.150 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.250 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CRZC | RIGHT TOP INSIDE ANGLE | 125.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | ANNEALED |
MATT | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.250 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AARN | FABRICATION METHOD | EXTRUDED |
ABRY | LENGTH | 12.000 FEET NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.150 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.150 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.390 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.250 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.640 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CSMZ | LEFT TOP INSIDE ANGLE | 55.0 DEGREES NOMINAL |
MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 AND CONDITION ANNEALED |
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