PWA81908: HEATER,AIRCRAFT ENGINE MAINTENAN.
HEATER,AIRCRAFT ENGINE MAINTENAN. Key specifications include fsc_application_data: F117-PW-100 ENGINE GROUND SUPPORTEQUIPMENT, functional_description: USED TO EXPAND THE FRONT FLANGE INNER DIAMETER OF THE HIGH PRESSURE COMPRESSOR AND SIXTH STAGE HUB DURING ASSEMBLY, functional_classification: GG-7.4, reference_data_and_literature: SERD NO. 1367.
This part is cataloged in the U.S. Government catalog under NSN 4920-01-382-4598, indicating validated use in U.S. government and defense logistics supply chains.
Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.
| special_features | C/O AN ALUMINUM BASE PLATE, A WELDED STEEL REFLECTOR, A TUBULAR ELECTRIC RESISTANCE ELEMENT, AN ELECTRICAL CONNECTOR, AND A THERMOCOUPLE PROBE; 16.00 IN. L, 14.5 IN. W, 13.00 IN. H; 25 LBS LBS |
| fsc_application_data | F117-PW-100 ENGINE GROUND SUPPORTEQUIPMENT |
| functional_description | USED TO EXPAND THE FRONT FLANGE INNER DIAMETER OF THE HIGH PRESSURE COMPRESSOR AND SIXTH STAGE HUB DURING ASSEMBLY |
| functional_classification | GG-7.4 |
| reference_data_and_literature | SERD NO. 1367 |
| NSN | 4920-01-382-4598 |
| FSC APPLICATION DATA | F117-PW-100 ENGINE GROUND SUPPORTEQUIPMENT |
| REFERENCE DATA AND LITERATURE | SERD NO. 1367 |
| FUNCTIONAL CLASSIFICATION | GG-7.4 |
| SPECIAL FEATURES | C/O AN ALUMINUM BASE PLATE, A WELDED STEEL REFLECTOR, A TUBULAR ELECTRIC RESISTANCE ELEMENT, AN ELECTRICAL CONNECTOR, AND A THERMOCOUPLE PROBE; 16.00 IN. L, 14.5 IN. W, 13.00 IN. H; 25 LBS LBS |
| FUNCTIONAL DESCRIPTION | USED TO EXPAND THE FRONT FLANGE INNER DIAMETER OF THE HIGH PRESSURE COMPRESSOR AND SIXTH STAGE HUB DURING ASSEMBLY |
No substitute or cross-reference records for this part.