4920-01-418-7664 ( PWA 71259 )
NSN Information
| NSN | FSC | NIIN | Item Name | INC |
|---|---|---|---|---|
| 4920-01-418-7664 | 4920 | 014187664 | TEST SET,AIRCRAFT ENGINE | 3889 |
NSN Features
| MRC | Parameter | Characteristics |
|---|---|---|
| FEAT | SPECIAL FEATURES | PLATE, TEST- PLASMA SPRAY, KNIFE EDGE SEALS |
| FTLD | FUNCTIONAL DESCRIPTION | CONSISTS OF A SERIES OF TEST PLATES SIMILIAR TO ONE DEPICTED IN SERD NO 7439, USED TO ESTABLISH AND MAINTAIN PLASMA SPRAY PARAMETERS FOR ENGINE PARTS BEING REPAIRED UNDER CIP TASK 311-43Y. SPECIFIC CONFIGURATIONS WILL BE PROVIDED TO ACCOMMODATE ALL PARTS LISTED BELOW |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 ENGINE |
| HGTH | HEIGHT | 3.000 INCHES NOMINAL |
| RDAL | REFERENCE DATA AND LITERATURE | SERD NO 7439 |
Manufacturing Part Numbers (SKUs)
| Part SKU | Cage | Status | RNVC | RNCC | SADC | DAC | RNAAC |
|---|---|---|---|---|---|---|---|
| PWA 71259 | 77445 | A | 2 | 3 | E | ZZ |
Manufacturers
| Part SKU | Cage | Manufacturer | Type | Status |
|---|---|---|---|---|
| PWA 71259 | 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 | 09/06/1 | N | 9803200000 | 3889 |
FLIS Management
| MOE | REC Rep Code | Mgmt Ctl | USC | Phrase Code | Phrase Statement |
|---|---|---|---|---|---|
| DF | N | SF9TG-N | F | ||
| DS | N | I |
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 |
|---|---|---|---|---|---|---|---|---|---|
| DS | SMS | J | 1 | EA | 0 | U | D | ||
| DF | SMS | J | 1 | EA | 0 | U | SF9TG-N | F |
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|