2915-00-651-7392 ( 319100 , CV21-505500-1 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 2915-00-651-7392 | 2915 | 006517392 | VALVE,ELBOW TYPE,CHECK | 7777 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | BODY,SEAT AND FLAPPER,ALUMINUM ALLOY,HINGE,ARM AND SPRING,STAINLESS STEEL,ANODIZE AND PASSIVATED METAL FINISH,FIRST END CONNECTION PER MS33660-32,1.490 IN. MIN,1.495 IN. MAX OD ON SECOND END CONNECTION,225 PSI BURST PRESSURE,75 PSI WORKING PRESSURE,150 PSI PROOF PRESSURE,M65 DEG F TO 135 DEG F FUEL TEMPERATURE RANGE |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT,F8U-2N |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 319100 | 96124 | A | 2 | 3 | X | XX | |
| CV21-505500-1 | 80378 | A | 2 | 5 | X | XX |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 319100 | 96124 | TRANSDIGM INC | F | A |
| CV21-505500-1 | 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 | 01/01/1 | N | 8481809050 | 7777 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DS | I | ||||
| DN | 9B----- | N | V | DISCONTINUED W/O REPLACEMENT |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| B | A | N | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DS | SMS | Y | 1 | EA | 0 | U | D | ||
| DN | SMS | V | 1 | EA | 0 | U | 9B----- | N |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|