4710-01-460-7263 ( DAA3122U454-001 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4710-01-460-7263 | 4710 | 014607263 | TUBE ASSEMBLY,METAL | 2198 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| AHSA | TUBING MATERIAL | TITANIUM ALLOY, TI-3AL-2.5V |
| ARJD | DESIGN FORM | PREBENT |
| AAGT | WALL THICKNESS | 0.024 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | ASSEMBLY IS PARTIALLY COILED; HAS INTERNAL SWAGE DYNATUBE TUBE FITTINGS ON EACH END; NOMINAL OPERATING PRESSURE IS 4000 PSI;LENGTH IS 61.8 INCHES |
| BBYQ | TUBE OUTSIDE DIAMETER | 0.250 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | B2 AIRCRAFT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | TUBE ASSEMBLY-COILED, RETURN, APU ACTUATOR |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| DAA3122U454-001 | 80378 | A | 2 | 3 | A | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| DAA3122U454-001 | 80378 | TRIUMPH AEROSTRUCTURES, LLC | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | X | B | 3 | 11/16/1 | A | N | 8108908000 | 2198 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | --SBQ-N | F | ||
| DF | ------- | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| B | A | N | 0 | X | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | F59 | J | 0 | EA | 0 | U | ------- | D | |
| DF | F59 | J | 0 | EA | 0 | U | --SBQ-N | D |
Management Control Army
| MATCAT 1 | MATCAT 2 | MATCAT 3 | MATCAT 4 5 | ARC |
|---|
Freight
| NMFC | NMFC SUB | UFC | HMC | LTL | LCL | WCC | TCC | SHC | ADC | ACC | ASH | NMF DESC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|