| DOCUMENT IDENTIFICATION | 351042 |
| DOCUMENT SOURCE | 06848 |
| DOCUMENT TYPE | PARTS LIST |
| COMPONENT DOCUMENT ORIGIN | INDUSTRIAL |
| COMPONENT DOCUMENT PAGE NUMBER | 2 |
| COMPONENT QUANTITY | 16 |
| END ITEM NAME | ENGINE, GAS TURBINE, AIRCRAFT |
| END ITEM SOURCE | 77445 |
| FSC APPLICATION DATA | AIRCRAFT ENGINE FUEL SYSTEM COMPONENT |
| MODEL NUMBER | PW-229 |
| SPECIAL FEATURES | C/O: 2 CAPS - 2651578; 4 SCREWS -2653065; 1 CAP - 2654828; 1 COVER - 2670068; 2 COVERS - 2672509; 1 DRIVE AY - 2678089; 1 SCREW - 953528-481; 1 EA LOCK WIRE OF - 78660-08;-010;-012;-014;-016;-018;-020;-022;-024 |
| USAGE DESIGN | DRIVE AY OF NOZZLE CONTROL |
| SUPPLEMENTARY FEATURES | NHA:CONVERGENT EXHAUST NOZZLE CONTROL ASSEMBLY |