9488118-7: FAIRING,AIRCRAFT.
The FAIRING,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.500 INCHES NOMINAL IN, overall_length: 26.000 INCHES NOMINAL IN, special_features: 2024-0 BARE AL SH OR 2024-0 CLAD AL SH; OR AMS QQ-A-250/5; DIM. ARE STOCKSIZE MATL; -8 OPPOSITE, aircraft_location: AILERON RETROFIT, material_thickness: 0.050 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-561-7965, 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 |
| overall_width | 2.500 INCHES NOMINAL IN |
| overall_length | 26.000 INCHES NOMINAL IN |
| special_features | 2024-0 BARE AL SH OR 2024-0 CLAD AL SH; OR AMS QQ-A-250/5; DIM. ARE STOCKSIZE MATL; -8 OPPOSITE |
| aircraft_location | AILERON RETROFIT |
| material_thickness | 0.050 INCHES NOMINAL IN |
| end_item_identification | F-15 A-E ACFT A |
| aircraft_mission_design_series | FAIRING LH |
| relationship_to_similar_equipment | OPPOSITE -8 |
| material_document_and_classification | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | FAIRING LH |
| NSN | 1560-01-561-7965 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | OPPOSITE -8 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 26.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | 2024-0 BARE AL SH OR 2024-0 CLAD AL SH; OR AMS QQ-A-250/5; DIM. ARE STOCKSIZE MATL; -8 OPPOSITE |
| AIRCRAFT LOCATION | AILERON RETROFIT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FAIRING LH |
| END ITEM IDENTIFICATION | F-15 A-E ACFT A |
| MATERIAL | ALUMINUM ALLOY 2024 |
No substitute or cross-reference records for this part.