4065342: PLATE,COMPONENT MOUNTING,AIRCRAF.
PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include material: TITANIUM ALLOY OVERALL, overall_length: 5.400 INCHES NOMINAL IN, special_features: T.O. 2J-F100-14, FIG 122, IND 42;3 HOLES W/DIA OF 1.771-1.791, end_item_identification: F100-PW-200/-220 AIRCRAFT ENGINES, engine_section_location: TURBINE, criticality_code_justification: CZBJ AND ABHP AND FEAT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-242-4616, 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.
| material | TITANIUM ALLOY OVERALL |
| overall_length | 5.400 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-14, FIG 122, IND 42;3 HOLES W/DIA OF 1.771-1.791 |
| end_item_identification | F100-PW-200/-220 AIRCRAFT ENGINES |
| engine_section_location | TURBINE |
| criticality_code_justification | CZBJ AND ABHP AND FEAT |
| material_document_and_classification | PWA1262-1 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BOSS BYPASS DUCT |
| NSN | 2840-01-242-4616 |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1262-1 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 5.400 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 122, IND 42;3 HOLES W/DIA OF 1.771-1.791 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BOSS BYPASS DUCT |
| END ITEM IDENTIFICATION | F100-PW-200/-220 AIRCRAFT ENGINES |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.