4920-01-375-5529 ( 856A1453G02 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4920-01-375-5529 | 4920 | 013755529 | FIXTURE,ENGINE MAINTENANCE,AIRCR | 4892 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| RDAL | REFERENCE DATA AND LITERATURE | SERD CFC3711 |
| FTLD | FUNCTIONAL DESCRIPTION | SUPPORTS P/N 856A1452G02,SHAFT WHEN CENTERING THE HIGH PRESSURE TURBINE (HPT) ROTOR AT MODULE 12 INSTALLATION OR REMOVAL IN THE HORIZIONAL POSITION |
| AGAV | END ITEM IDENTIFICATION | F-108 ENGINE |
| FCLS | FUNCTIONAL CLASSIFICATION | GG-7.4 |
| FEAT | SPECIAL FEATURES | CONSIST OF A A-FRAME WELDMENT; ADJUSTABLE JACKSCREW THRU THE TOP CENTER PLATE; A V-GROOVE BLOCK ON TOP TO INTERFACE WITH THE HPT SHAFT EXTENSION,P/N 856A1454; CONSTRUCTED OF ALUMINUM AND IS ANODIZED FOR CORROSION PROTECTION |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 856A1453G02 | 58828 | A | 2 | 3 | 4 | MB |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 856A1453G02 | 58828 | CFM INTERNATIONAL INC. | A | A |
FLIS Identification
| PMIC | ADPE Code | CRITL Code | DEMIL Code | DEMIL INTG | NIIN Asgt | ESD | HMIC | ENAC | Schedule-B | INC |
|---|---|---|---|---|---|---|---|---|---|---|
| A | 0 | N | A | 05/14/1 | N | 8466208040 | 4892 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | U | --YRN-E | L |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | N |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | FLZ | Y | 1 | EA | 0 | U | --YRN-E | L |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|