PWA57151: HEATER,AIRCRAFT ENGINE MAINTENAN.
HEATER,AIRCRAFT ENGINE MAINTENAN. Key specifications include overall_length: 15.000 INCHES NOMINAL IN, overall_diameter: 11.000 INCHES NOMINAL IN, supplementary_features: WEIGHT 20 LBS LBS, end_item_identification: F100-PW-100/200/220 ENGINE, functional_classification: JJ-1.1, reference_data_and_literature: T.O.2J-F100-94. This part is cataloged in the U.S.
Government catalog under NSN 4920-01-200-2276, 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.
| overall_length | 15.000 INCHES NOMINAL IN |
| overall_diameter | 11.000 INCHES NOMINAL IN |
| functional_description | USED TO OVERCOME INTERFERENCE FIT BETWEEN REAR COMPRESSOR DRIVE TURBINE SHAFT AND REAR COMPRESSOR DRIVE ROTOR AND STATOR FRONT HUB DURING ASSEMBLY |
| supplementary_features | WEIGHT 20 LBS LBS |
| end_item_identification | F100-PW-100/200/220 ENGINE |
| functional_classification | JJ-1.1 |
| reference_data_and_literature | T.O.2J-F100-94 |
| NSN | 4920-01-200-2276 |
| OVERALL DIAMETER | 11.000 INCHES NOMINAL IN |
| SUPPLEMENTARY FEATURES | WEIGHT 20 LBS LBS |
| REFERENCE DATA AND LITERATURE | T.O.2J-F100-94 |
| OVERALL LENGTH | 15.000 INCHES NOMINAL IN |
| FUNCTIONAL CLASSIFICATION | JJ-1.1 |
| FUNCTIONAL DESCRIPTION | USED TO OVERCOME INTERFERENCE FIT BETWEEN REAR COMPRESSOR DRIVE TURBINE SHAFT AND REAR COMPRESSOR DRIVE ROTOR AND STATOR FRONT HUB DURING ASSEMBLY |
| END ITEM IDENTIFICATION | F100-PW-100/200/220 ENGINE |
No substitute or cross-reference records for this part.