9488118-17: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 1.100 INCHES NOMINAL IN, overall_length: 2.400 INCHES NOMINAL IN, aircraft_location: FAIRING BRACKET F-15 AILERON RETROFIT DESIGN, surface_treatment: CHROMATE AND DICHROMATE, material_thickness: 0.063 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-561-6929, 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 | 1.100 INCHES NOMINAL IN |
| overall_length | 2.400 INCHES NOMINAL IN |
| aircraft_location | FAIRING BRACKET F-15 AILERON RETROFIT DESIGN |
| surface_treatment | CHROMATE AND DICHROMATE |
| material_thickness | 0.063 INCHES NOMINAL IN |
| special_test_features | PENETRANT INSP PER AMS 2647 |
| end_item_identification | F-15 ACFT AILERON |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | F-15 EAGLE |
| relationship_to_similar_equipment | 9488118-18 OPPOSITE |
| material_document_and_classification | AMS-QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE OR AMS-QQ-A-250/5 FED SPEC 2ND MATERIAL RESPONSE |
| NSN | 1560-01-561-6929 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 TYPE II CLASS I MIL SPEC SINGLE TREATMENT RESPONSE |
| RELATIONSHIP TO SIMILAR EQUIPMENT | 9488118-18 OPPOSITE |
| SPECIAL TEST FEATURES | PENETRANT INSP PER AMS 2647 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE OR AMS-QQ-A-250/5 FED SPEC 2ND MATERIAL RESPONSE |
| OVERALL LENGTH | 2.400 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.100 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL IN |
| SPECIAL FEATURES | MATL 2024-0 BARE AL SHEET OR 2024-0 CLAD AL SHEET, AMS-QQ-A-250/4 OR AMS-QQ-A-250/5;IDENTIFY PER MIL-STD-130, PENETRANT INSPECT PER AMS2647;HEAT TREAT COND 0, AL ALLOY TO T62 PER AMS 2770 AFTER FORMING;ANODIZE AND DICRHROMATE PER MIL-A-8625 TYPE II CLASS I |
| SURFACE TREATMENT | CHROMATE AND DICHROMATE |
| AIRCRAFT LOCATION | FAIRING BRACKET F-15 AILERON RETROFIT DESIGN |
No substitute or cross-reference records for this part.