Mfg Part Number: CVC10010 121GA
Alternate P/N: CVC10010121GA
NSN : 9540-01-463-0446
NIIN : 014630446
CAGE Code : 80378
Manufacturer: Triumph Aerostructures Llc
Item Name : Beam Structural
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-463-0446 Item Description: Beam Structural | 9540 | 014630446 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
CVC10010 121GA | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
AJJP | LEG THICKNESS | 0.080 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 AND CONDITION ANNEALED |
SR-1 | MANUFACTURERS CODE | 81349 |
ABKW | OVERALL HEIGHT | 1.060 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
SR-1 | NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | MIL-T-81556 |
SR-1 | SPEC/STD CONTROLLING DATA | |
AARN | FABRICATION METHOD | EXTRUDED |
ABRY | LENGTH | 12.000 FEET NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.000 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
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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