5120-01-502-8126 ( SEV9006P2 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 5120-01-502-8126 | 5120 | 015028126 | STEP PLATE,MECHANICAL PULLER | 2018 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BLOCK |
| AGAV | END ITEM IDENTIFICATION | TOOL, PULLER-GENERATOR ROTOR REMOVAL FOR F-18 AIRCRAFT |
| SFTT | SURFACE TREATMENT | PASSIVATE |
| ABKW | OVERALL HEIGHT | 1.930 INCHES NOMINAL |
| MATT | MATERIAL | STEEL CORROSION RESISTING |
| ADAV | OVERALL DIAMETER | 1.365 INCHES MINIMUM AND 1.367 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 2.260 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| THDS | THREAD SIZE AND SERIES/TYPE DESIGNATOR | 0.190-32 UNF |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| SEV9006P2 | 07639 | A | 2 | 3 | 5 | KE |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| SEV9006P2 | 07639 | GE AVIATION SYSTEMS LLC | 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 | 7 | 11/21/2 | N | 8205700090 | 2018 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DN | M | 1RQE009 | N | ||
| DN | ------- | I |
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 |
|---|---|---|---|---|---|---|---|---|---|
| DN | NRP | D | 1 | EA | 0 | U | 1RQE009 | N | |
| DN | NRP | D | 1 | EA | 0 | U | ------- | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|