Part Details | FUEL CONTROL SYSTEM COMPONENTS TEST STATION
4920-00-908-9341 A group of items containing a console and/or perpheral equipment specifically designed to provide appropriate instrumentation and data acquisition/control logic for testing of components of an aircraft fuel system.
Alternate Parts: PWA15710, PWA15500, 4920-00-908-9341, 00-908-9341, 4920009089341, 009089341
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 49 | JAN 01, 1960 | 00-908-9341 | 41317 ( TEST STATION, FUEL CONTROL SYSTEM COMPONENTS ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4920-00-908-9341
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| PWA15710 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| PWA15500 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 4920-00-908-9341
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | PW-TF30 ENGINES, FUEL MANIFOLD SYSTEM AND AFTERBURNER NOZZLE ACTUATOR |
| SPECIAL FEATURES | THE TEST STAND IS A MOBILE STEEL STRUCTURE HOUSING FUEL CIRCUIT AND REFRIGERATION SYSTEM COMPONENTS AND THE NECESSARY WIRING, PLUMBING, CONTROLS AND INSTRUMENTATION NECESSARY FOR OPERATION; THE COMPLETE TEST STAND MEETS THE REQUIREMENTS FOR CLASS 1, GROUP D, HAZARDOUS LOCATION EQUIPMENT; CONNECTION TO THE TEST COMPONENT IS BY QUICK DISCONNECT FLEXIBLE HOSE LINES ON THE RIGHT SIDE OF THE TEST STAND ALONG WITH THE POWER INPUT CABLE |
| UNPACKAGED UNIT LENGTH | 53.500 INCHES NOMINAL |
| UNPACKAGED UNIT WIDTH | 43.500 INCHES NOMINAL |
| UNPACKAGED UNIT HEIGHT | 42.000 INCHES NOMINAL |
| PORTABILITY METHOD | BRAKE TYPE CASTERS |
| CUBIC MEASURE | 97744.500 CUBIC INCHES |
| SUPPLEMENTARY FEATURES | THE QUICK CONNECT FLEXIBLE HOSE LINES ARE NOT SUPPLIED WITH THE PWA15500A AND PWA15710 TEST STANDS HOWEVER THEY ARE AVAILABLE AS KIT ASSY PWA-15747; ELECTRICAL POWER REQUIREMENTS-220VAC, 3PHASE, 60 CYCLE, 7KVA; FUEL TANK CAPACITY- 20 GALLONS OF MIL-F-7024A TYPE 2 FUEL; STAND MAINTAINS FUEL BETWEEN 85 TO 90 DEG F UP TO AMBIENTS OF 100 DEG F |
| FUNCTIONAL DESCRIPTION | TEST STAND IS USED TO LEAK TEST THE FUEL MANIFOLD SYSTEM AND AFTERBURNER NOZZLE ON THE PW-TF30 ENGINE |
| REFERENCE DATA AND LITERATURE | T.O. 33D4-6-310-11; NAVAIR17-15BD-25 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | STAND ASSEMBLY,FUEL PRESSURE TEST |