1560-01-574-5980 ( 205-061-503-1 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-574-5980 | 1560 | 015745980 | SUPPORT,STRUCTURAL COMPONENT,AIR | 3224 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 T4 FED SPEC SINGLE MATERIAL RESPONSE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT |
| CZDJ | AIRCRAFT LOCATION | OIL COOLER ASSY |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | TH-1H-MOD. |
| AGAV | END ITEM IDENTIFICATION | TH-1H HELICOPTER |
| ABHP | OVERALL LENGTH | 17.540 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | AL ALY; DIM ARE STOCKSIZE MATL; C/O 1 SUPPORT, 4 NUTPLATE, RIVETS AR |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 205-061-503-1 | 97499 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 205-061-503-1 | 97499 | BELL HELICOPTER TEXTRON INC. | 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 | 06/03/2 | A | P | 8803909060 | 3224 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DS | N | I | |||
| DF | N | SF9HL-N | F |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| B | A | P | 0 | X | A |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | SMS | Z | 1 | EA | 0 | U | SF9HL-N | F | |
| DS | SMS | Z | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|