5365-01-502-8075 ( SEV9006P11 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 5365-01-502-8075 | 5365 | 015028075 | SPACER,SLEEVE | 1320 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| ADAR | BODY OUTSIDE DIAMETER | 0.6250 INCHES NOMINAL |
| BZLX | CORNER SHAPE | CHAMFERED SECOND OUTSIDE CORNER |
| AGAV | END ITEM IDENTIFICATION | TOOL, PULLER-GENERATOR ROTOR REMOVAL FOR F-18 AIRCRAFT |
| MATT | MATERIAL | STEEL COMP 304 OVERALL |
| BZLX | CORNER SHAPE | CHAMFERED FIRST OUTSIDE CORNER |
| STYL | STYLE DESIGNATOR | SOLID |
| ABHP | OVERALL LENGTH | 2.2500 INCHES MINIMUM AND 2.5250 INCHES MAXIMUM |
| ADAS | BODY INSIDE DIAMETER | 0.2810 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| SFTT | SURFACE TREATMENT | PASSIVATE OVERALL |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| SEV9006P11 | 07639 | A | 2 | 3 | 5 | KE |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| SEV9006P11 | 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 | 7326908595 | 1320 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DS | I | ||||
| DN | 9BQE--9 | N |
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 |
|---|---|---|---|---|---|---|---|---|---|
| DS | SMS | Z | 1 | EA | 0 | U | D | ||
| DN | SMS | Z | 1 | EA | 0 | U | 9BQE--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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|