68A321029-2057: STRINGER,AIRCRAFT.
The STRINGER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, special_features: NHA 68A321029-1017,-1009; U/O F-15E CUM3&UP, F-15I,S CUM1&UP, aircraft_location: FUSELAGE NO.2, side_for_which_designed: LEFT SIDE, aircraft_mission_design_series: F-15E,I,S, material_document_and_classification: 1MA160B04-10407 MFR REF SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-480-6366, 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 | ALUMINUM ALLOY |
| special_features | NHA 68A321029-1017,-1009; U/O F-15E CUM3&UP, F-15I,S CUM1&UP |
| aircraft_location | FUSELAGE NO.2 |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | F-15E,I,S |
| material_document_and_classification | 1MA160B04-10407 MFR REF SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-480-6366 |
| MATERIAL DOCUMENT AND CLASSIFICATION | 1MA160B04-10407 MFR REF SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | NHA 68A321029-1017,-1009; U/O F-15E CUM3&UP, F-15I,S CUM1&UP |
| AIRCRAFT LOCATION | FUSELAGE NO.2 |
| MATERIAL | ALUMINUM ALLOY |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-15E,I,S |
No substitute or cross-reference records for this part.