68A311956-1015: ROD ASSEMBLY,COVER,AIRCRAFT.
The ROD ASSEMBLY,COVER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, aircraft_location: ACCESS DOOR,AVIONICS,RH, aircraft_mission_design_series: F-15I, material_document_and_classification: WW-T-700/3 CONDITION T3,TYPE 1 FED SPEC SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-435-8567, 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 2024 |
| special_features | REQUESTEDNAME:BRACE,ACFT GROUND S;DIMENSION FROM CENTERLINE OF CLEVIS P/N 68A311963-2003 TO THAT OF PIN ASSEMBLY P/N ST9M553-1A IS 15.77 INCHES; LENGTH OF TUBE P/N 68A311956-2005 IS 12.77 INCHES A |
| aircraft_location | ACCESS DOOR,AVIONICS,RH |
| aircraft_mission_design_series | F-15I |
| material_document_and_classification | WW-T-700/3 CONDITION T3,TYPE 1 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-435-8567 |
| MATERIAL DOCUMENT AND CLASSIFICATION | WW-T-700/3 CONDITION T3,TYPE 1 FED SPEC SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | REQUESTEDNAME:BRACE,ACFT GROUND S;DIMENSION FROM CENTERLINE OF CLEVIS P/N 68A311963-2003 TO THAT OF PIN ASSEMBLY P/N ST9M553-1A IS 15.77 INCHES; LENGTH OF TUBE P/N 68A311956-2005 IS 12.77 INCHES A |
| AIRCRAFT LOCATION | ACCESS DOOR,AVIONICS,RH |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | F-15I |
No substitute or cross-reference records for this part.