5054M43P02: SEAL,METALLIC,AIRCRAFT GAS TURBI.
SEAL,METALLIC,AIRCRAFT GAS TURBI. Key specifications include material: NICKEL ALLOY OVERALL, overall_height: 0.300 INCHES MINIMUM AND 0.320 INCHES MAXIMUM IN, overall_length: 0.840 INCHES MINIMUM AND 0.860 INCHES MAXIMUM IN, material_thickness: 0.024 INCHES MINIMUM AND 0.032 INCHES MAXIMUM IN, end_item_identification: F110-100 F16C/D AIRCRAFT ENGINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-362-3771, 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 | NICKEL ALLOY OVERALL |
| overall_height | 0.300 INCHES MINIMUM AND 0.320 INCHES MAXIMUM IN |
| overall_length | 0.840 INCHES MINIMUM AND 0.860 INCHES MAXIMUM IN |
| material_thickness | 0.024 INCHES MINIMUM AND 0.032 INCHES MAXIMUM IN |
| end_item_identification | F110-100 F16C/D AIRCRAFT ENGINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-362-3771 |
| OVERALL HEIGHT | 0.300 INCHES MINIMUM AND 0.320 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 0.840 INCHES MINIMUM AND 0.860 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.024 INCHES MINIMUM AND 0.032 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | F110-100 F16C/D AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.