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MRC | Criteria | Characteristic |
---|---|---|
SUPP | III 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 |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | STAND ASSEMBLY,FUEL PRESSURE TEST |
AFJS | III PORTABILITY METHOD | BRAKE TYPE CASTERS |
AJAG | III UNPACKAGED UNIT WIDTH | 43.500 INCHES NOMINAL |
AJAH | III UNPACKAGED UNIT HEIGHT | 42.000 INCHES NOMINAL |
FEAT | 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 |
RDAL | III REFERENCE DATA AND LITERATURE | T.O. 33D4-6-310-11; NAVAIR17-15BD-25 |
AGAV | END ITEM IDENTIFICATION | PW-TF30 ENGINES, FUEL MANIFOLD SYSTEM AND AFTERBURNER NOZZLE ACTUATOR |
CBME | III CUBIC MEASURE | 97744.500 CUBIC INCHES |
FTLD | III FUNCTIONAL DESCRIPTION | TEST STAND IS USED TO LEAK TEST THE FUEL MANIFOLD SYSTEM AND AFTERBURNER NOZZLE ON THE PW-TF30 ENGINE |
ALQG | III CONTAINER TYPE | ROLL CABINET |
AJAF | III UNPACKAGED UNIT LENGTH | 53.500 INCHES NOMINAL |
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