1364M44G04: SHIELD,HEAT,AIRCRAFT GAS TURBINE.
SHIELD,HEAT,AIRCRAFT GAS TURBINE. Key specifications include material: NICKEL ALLOY SHIELD, overall_width: 0.920 INCHES MINIMUM AND 0.960 INCHES MAXIMUM IN, overall_length: 7.300 INCHES MINIMUM AND 7.340 INCHES MAXIMUM IN, special_features: T.O. 2J-F110-14; ITEM FITS OVER TURBINE FRAME STRUT EDGE; IS FOLDED IN V-SHAPED, end_item_identification: F110-GE-129 AIRCRAFT ENGINE, engine_section_location: TURBINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-368-5693, 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 | 0.920 INCHES MINIMUM AND 0.960 INCHES MAXIMUM IN |
| overall_length | 7.300 INCHES MINIMUM AND 7.340 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F110-14; ITEM FITS OVER TURBINE FRAME STRUT EDGE; IS FOLDED IN V-SHAPED |
| end_item_identification | F110-GE-129 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE SHIELD |
| NSN | 2840-01-368-5693 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE SHIELD |
| OVERALL LENGTH | 7.300 INCHES MINIMUM AND 7.340 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.920 INCHES MINIMUM AND 0.960 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F110-14; ITEM FITS OVER TURBINE FRAME STRUT EDGE; IS FOLDED IN V-SHAPED |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY SHIELD |
No substitute or cross-reference records for this part.