4730-01-471-9284 ( 110-114-040606 , AE16397-04 , R45122T5-04 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4730-01-471-9284 | 4730 | 014719284 | TEE,TUBE | 0380 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| AGAV | END ITEM IDENTIFICATION | V22 AIRCRAFT |
| FEAT | SPECIAL FEATURES | TITANIUM PER AMS4965 (6AL-4V); OPERATING PRESSURE IS 5000 PSI; PROOF PRESSURE IS 10,000; BURST PRESSURE IS 20,000 |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 110-114-040606 | 97499 | A | 2 | 3 | 1 | KE | |
| AE16397-04 | 00624 | A | 2 | 3 | 5 | KE | |
| R45122T5-04 | 50599 | A | 2 | 3 | 5 | KE |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 110-114-040606 | 97499 | BELL HELICOPTER TEXTRON INC. | A | A |
| AE16397-04 | 00624 | EATON CORPORATION | A | A |
| R45122T5-04 | 50599 | PARKER-HANNIFIN CORPORATION | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | Y | A | 02/17/2 | N | 0380 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DN | 9BV2--9 | N | |||
| DS | N | I | |||
| DF | N | SF9NV-N | F |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | Y |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | SMS | Z | 1 | EA | 0 | U | SF9NV-N | F | |
| DS | SMS | Z | 1 | EA | 0 | U | D | ||
| DN | SMS | Z | 1 | EA | 0 | U | 9BV2--9 | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|