4940-01-384-9447 ( PWA95207 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4940-01-384-9447 | 4940 | 013849447 | ADAPTER,MECHANICAL TEST | 3993 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F117-PW-100 AIRCRAFT ENGINE |
| RDAL | REFERENCE DATA AND LITERATURE | SERD 1775 |
| FTLD | FUNCTIONAL DESCRIPTION | USED TO DEAD LOAD TEST THE ADAPTER USED TO SUPPORT THE HIGH PRESSURE ROTOR AND STATOR MODULE |
| FEAT | SPECIAL FEATURES | CONSISTS OF A WELDED STEEL ASSEMBLY; CIRCULAR BASE SUPPORTING A RING ON SIX CYLINDRICAL PEDESTALS, AND A LONG CYLINDER; FOUR TRIANGULAR SHAPED PLATES WELDED TO THE BASE AND THE CYLINDER OUTER SURFACE, TO PROVIDE STIFFENING TO THE ASSEMBLY; MOUNTING HOLES ARE INCORPORATED IN THE BASE AND RING; APPROX. 28.3000 IN. DIA.; 37.000 IN. HT. |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| PWA95207 | 77445 | A | 2 | 3 | 4 | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| PWA95207 | 77445 | UNITED TECHNOLOGIES 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 | A | 12/28/1 | N | 3993 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | U | --SBE-P | L |
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 | F77 | J | 1 | EA | 0 | U | --SBE-P | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|