4062398: PLATE,COMPONENT MOUNTING,AIRCRAF.
PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include diameter: 28.610 INCHES MINIMUM AND 28.630 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 1.346 INCHES MINIMUM AND 1.366 INCHES MAXIMUM IN, special_features: MATERIAL SPEC AMS 5662, end_item_identification: F100-PW-220 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: DIFFUSER. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-396-0550, 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 | 28.610 INCHES MINIMUM AND 28.630 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 1.346 INCHES MINIMUM AND 1.366 INCHES MAXIMUM IN |
| special_features | MATERIAL SPEC AMS 5662 |
| end_item_identification | F100-PW-220 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | DIFFUSER |
| criticality_code_justification | AGAV |
| NSN | 2840-01-396-0550 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 28.610 INCHES MINIMUM AND 28.630 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.346 INCHES MINIMUM AND 1.366 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | DIFFUSER |
| SPECIAL FEATURES | MATERIAL SPEC AMS 5662 |
| END ITEM IDENTIFICATION | F100-PW-220 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.