1560-01-553-0449 ( 204-70045-55 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-553-0449 | 1560 | 015530449 | PLATE,STRUCTURAL,AIRCRAFT | 3149 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| ABPX | MATERIAL THICKNESS | 0.050 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 2.200 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER |
| ABHP | OVERALL LENGTH | 2.500 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | E-3A |
| FEAT | SPECIAL FEATURES | DIM. ARE STOCK MATERIAL |
| CZDJ | AIRCRAFT LOCATION | SIDE COWL PANEL, ENGINE NACELLE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 TYPE I COMP B ANNEALED MIL SPEC SINGLE MATERIAL RESPONSE |
| MATT | MATERIAL | TITANIUM ALLOY |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 204-70045-55 | 81205 | A | 2 | 3 | C | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 204-70045-55 | 81205 | THE BOEING COMPANY | F | 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 | 07/03/2 | A | P | 8803909060 | 3149 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DS | N | I | |||
| DF | N | SF9---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 |
|---|---|---|---|---|---|---|---|---|---|
| DS | SMS | Z | 1 | EA | 0 | U | D | ||
| DF | SMS | Z | 1 | EA | 0 | U | SF9---N | F |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|