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MRC | Criteria | Characteristic |
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FTLD | III FUNCTIONAL DESCRIPTION | USED FOR TESTING OF MODEL TPC-23/24 PUMPS USED ON THE F100-PW-220/229 ENGINE |
AGAV | END ITEM IDENTIFICATION | F100-PW-100/200/220/220E/229 AIRCRAFT ENGINE |
RDAL | III REFERENCE DATA AND LITERATURE | SERD NO. 5942 |
SR-5 | THE MANUFACTURERS DATA | |
SR-5 | DESIGN CONTROL REFERENCE | PWA56214-3 |
SR-5 | MANUFACTURERS CODE | 77445 |
FEAT | SPECIAL FEATURES | C/O FUEL FLOW-PUMP; FUEL FLOW-BEARING; AIR FLOW; FUEL OUTLET PRESSURE AIR INLET PRESSURE; AIR INLET TEMPERATURE T/C; FUEL INLET TEMPERATURE T/C; THERMOCOUPLE INDICATOR; FUEL LEAKAGE; FUEL INLET PRESSURE; SHAFT SPEED; AIR OUTLET PRESSURE; FUEL WETTED TURBINE AIR MODULE; POWER CABINET; CONSOLE; SINK; CABLES; DEDICATED REMOTE PUMP MODULE;POWER: 277/480 VOLT,3 PHASE,60 HZ OR 380 VOLT,3 PHASE,50 HZ; CONTROL CIRCUIT; 120 VOLTS,SINGLE PHASE,60 HZ; OR 220 VOLTS,SINGLE PHASE,50 HZ; COMPRESSED AIR; LOW PRESSEUR; 100 SCFM,90 PSIG; 30 DEGREE F DEW POINT; FACILITY TURBINE AIR: 120 PPM,400 PSIG,600 F; CHILLED WATER: 150 GPM,75 PSIG,45DEGREE F |
SUPP | III SUPPLEMENTARY FEATURES | COMPANY ITEM NAME-TEST STATION |
Guaranteed on-time |
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Customized and |
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Over 5100 |
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Complete Purchasing |