The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL COMP 347, overall_length: 21.540 INCHES NOMINAL IN, aircraft_location: RETAINER-ENGINE DUCT SEAL, aircraft_mission_design_series: C-130B,E,H, material_document_and_classification: MIL-S-6721 MIL SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 3110-00-155-6174, 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 | STEEL COMP 347 |
| overall_length | 21.540 INCHES NOMINAL IN |
| aircraft_location | RETAINER-ENGINE DUCT SEAL |
| aircraft_mission_design_series | C-130B,E,H |
| material_document_and_classification | MIL-S-6721 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 3110-00-155-6174 |
| STANDARD TOLERANCE DESIGNATION | ABEC NO.1 |
| INTERNAL FIT-UP DESIGNATION | STANDARD |
| INTERNAL FIT-UP DESIGNATION | STANDARD |
| SHIELD QUANTITY | 1 |
| STYLE DESIGNATOR | NON-LOADING GROOVE, NON-SEPARABLE |
| BORE SHAPE | STRAIGHT |
| NONDEFINITIVE SPEC/STD DATA | 111CL5GR00 TYPE |
| MATERIAL | STEEL OVERALL |
| STYLE DESIGNATOR | NON-LOADING GROOVE, NON-SEPARABLE |
| MATERIAL | STEEL OVERALL |