4730-01-524-8645 ( 7D0479A24-1 , EFFB24A0-1A )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4730-01-524-8645 | 4730 | 015248645 | UNION,TUBE | 0378 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CQGM | MAXIMUM OPERATING PRESSURE | 125.0 POUNDS PER SQUARE INCH SINGLE RESPONSE |
| AGAV | END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| MATT | MATERIAL | ALUMINUM ALLOY OVERALL |
| CWCK | NOMINAL THICKNESS | 0.283 INCHES ALL ENDS BULKHEAD |
| CWFD | NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 1.500 INCHES ALL ENDS |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | UNION,TUBE - FUEL CPLY FERRULE ENDS,FORCED EXPANSION SPECIAL |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 7D0479A24-1 | 88277 | A | 2 | 5 | C | ZZ | |
| EFFB24A0-1A | 51439 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 7D0479A24-1 | 88277 | BOEING COMPANY THE | F | A |
| EFFB24A0-1A | 51439 | FATIGUE TECHNOLOGY INTERNATIONAL | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | X | A | 1 | 10/19/2 | N | 7609000000 | 0378 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | --SBA-E | F | ||
| DF | ------- | I |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | F77 | D | 1 | EA | 0 | U | --SBA-E | D | |
| DF | F77 | D | 1 | EA | 0 | U | ------- | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|