4920-01-145-9547 ( 856A2534G01 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4920-01-145-9547 | 4920 | 011459547 | SUPPORT,BOOSTER GUIDE | 7777 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | TO SUPPORT LOW PRESSURE TURBINE SHAFT DURING REMOVAL/INSTALLATION OF NO. 1 AND NO. 2 BEARING SUPPORT; O/A DIM: 72.000 IN. LG.,20.000 IN. W.,9.000 IN. H.; WT: 44 LBS |
| ABKW | OVERALL HEIGHT | 9.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | KC-135R AIRCRAFT |
| ABHP | OVERALL LENGTH | 72.000 INCHES NOMINAL |
| FTLD | FUNCTIONAL DESCRIPTION | USED TO SUPPORT LOW PRESSURE TURBINE SHAFT DURING REMOVAL/INSTALLATION OF NUMBER 1 AND NUMBER 2 BEARING SUPPORT |
| ABMK | OVERALL WIDTH | 20.000 INCHES NOMINAL |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| 856A2534G01 | 58828 | A | 2 | 3 | 2 | SB |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| 856A2534G01 | 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 | X | A | 01/21/1 | N | 7777 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | U | --YRN-N | L | F | WHEN EXHAUSTED USE 4920-01-272-4397 |
Demilitarization Codes & Management
| DML | PMI | HMIC | ADP | CC | ESDC |
|---|---|---|---|---|---|
| A | A | N | 0 | X |
Miscellaneous Management
| MOE (S_A) | SOS | AAC | QUP | UI | SLC | CIIC | RC | MCC | SVC |
|---|---|---|---|---|---|---|---|---|---|
| DF | FLZ | V | 1 | EA | 0 | U | --YRN-N | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|