Mfg Part Number: CVC10011 79GA
Alternate P/N: CVC1001179GA
NSN : 9540-01-463-0602
NIIN : 014630602
CAGE Code : 80378
Manufacturer: Triumph Aerostructures Llc
Item Name : Beam Structural
Here at Internet For Aviation, we have CVC10011 79GA 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 CVC10011 79GA 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 |
|---|---|---|---|---|---|---|
| 9540-01-463-0602 Item Description: Beam Structural | 9540 | 014630602 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CVC10011 79GA | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.980 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.100 INCHES NOMINAL |
| MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
| CMZY | FIRST TIP STYLE | SQUARE END |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITIION AB-1 AND CONDITION ANNEALED |
| SR-1 | MANUFACTURERS CODE | 81349 |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| AARN | FABRICATION METHOD | EXTRUDED |
| SR-1 | NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | MIL-T-9046 |
| SR-1 | SPEC/STD CONTROLLING DATA | |
| ABKW | OVERALL HEIGHT | 3.360 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.490 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.490 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.440 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.540 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATT | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
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