9340M95G05: SHIELD,HEAT,AIRCRAFT GAS TURBINE.
SHIELD,HEAT,AIRCRAFT GAS TURBINE. Key specifications include material: NICKEL ALLOY SHIELD, overall_width: 1.400 INCHES NOMINAL IN, overall_length: 13.360 INCHES MINIMUM AND 13.400 INCHES MAXIMUM IN, material_thickness: 0.030 INCHES MINIMUM AND 0.034 INCHES MAXIMUM IN, end_item_identification: ACFT ENG F110, engine_section_location: EXHAUST. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-200-0123, 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 SHIELD |
| overall_width | 1.400 INCHES NOMINAL IN |
| overall_length | 13.360 INCHES MINIMUM AND 13.400 INCHES MAXIMUM IN |
| material_thickness | 0.030 INCHES MINIMUM AND 0.034 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG F110 |
| engine_section_location | EXHAUST |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5540 ASSN STD SINGLE MATERIAL RESPONSE SHIELD |
| NSN | 2840-01-200-0123 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5540 ASSN STD SINGLE MATERIAL RESPONSE SHIELD |
| OVERALL LENGTH | 13.360 INCHES MINIMUM AND 13.400 INCHES MAXIMUM IN |
| OVERALL WIDTH | 1.400 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | EXHAUST |
| MATERIAL THICKNESS | 0.030 INCHES MINIMUM AND 0.034 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | ACFT ENG F110 |
| MATERIAL | NICKEL ALLOY SHIELD |