2840PL1776183: CASE,COMPRESSOR,AIRCRAFT GAS TUR.
CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 28.700 INCHES NOMINAL IN, material: NICKEL ALLOY OUTER CASE, design_type: COMPRESSOR, overall_length: 17.390 INCHES MINIMUM AND 17.414 INCHES MAXIMUM IN, special_features: INCLUDES 4-9 STAGES; USE ONLY ON 4079598-05; T.O. 2J-F100-54, end_item_identification: F100PW0229 AIRCRAFT ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-377-3510, 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.
| diameter | 28.700 INCHES NOMINAL IN |
| material | NICKEL ALLOY OUTER CASE |
| design_type | COMPRESSOR |
| overall_length | 17.390 INCHES MINIMUM AND 17.414 INCHES MAXIMUM IN |
| special_features | INCLUDES 4-9 STAGES; USE ONLY ON 4079598-05; T.O. 2J-F100-54 |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-377-3510 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 28.700 INCHES NOMINAL IN |
| OVERALL LENGTH | 17.390 INCHES MINIMUM AND 17.414 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | INCLUDES 4-9 STAGES; USE ONLY ON 4079598-05; T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OUTER CASE |
No substitute or cross-reference records for this part.