1560-01-502-6884 ( CE01167D511A , ABA24913KT1D120 , ABA24913K1D120A )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 1560-01-502-6884 | 1560 | 015026884 | PLATE,STRUCTURAL,AIRCRAFT | 3149 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | DOUBLER,FRONT |
| MATT | MATERIAL | STEEL CORROSION RESISTING |
| ABPX | MATERIAL THICKNESS | 0.037 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | CH-47 |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| CE01167D511A | 18350 | A | 2 | 3 | 1 | ZZ | |
| ABA24913KT1D120 | 18350 | A | 9 | 5 | 1 | ZZ | |
| ABA24913K1D120A | 18350 | A | 9 | D | 1 | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| CE01167D511A | 18350 | PALL AEROPOWER CORPORATION | A | A |
| ABA24913KT1D120 | 18350 | PALL AEROPOWER CORPORATION | A | A |
| ABA24913K1D120A | 18350 | PALL AEROPOWER CORPORATION | 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 | 11/18/2 | P | 8803909060 | 3149 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DS | N | I | |||
| DA | Z | E2200X- | A |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| B | A | P | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DS | SMS | Z | 1 | EA | 0 | U | D | ||
| DA | SMS | Z | 1 | EA | 0 | U | Z | E2200X- | A |
Management Control Army
| MATCAT 1 | MATCAT 2 | MATCAT 3 | MATCAT 4 5 | ARC |
|---|---|---|---|---|
| E | 2 | 2 | 00 | X |
Freight
| NMFC | NMFC SUB | UFC | HMC | LTL | LCL | WCC | TCC | SHC | ADC | ACC | ASH | NMF DESC |
|---|---|---|---|---|---|---|---|---|---|---|---|---|