35-10720-84: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.200 INCHES NOMINAL IN, overall_length: 4.300 INCHES NOMINAL IN, special_features: OPPOSITE 35-10720-83, aircraft_location: SUPPORT ANGLE ON AFT COWL, material_thickness: 0.070 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-151-8501, 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 7075 |
| overall_width | 2.200 INCHES NOMINAL IN |
| overall_length | 4.300 INCHES NOMINAL IN |
| special_features | OPPOSITE 35-10720-83 |
| aircraft_location | SUPPORT ANGLE ON AFT COWL |
| material_thickness | 0.070 INCHES NOMINAL IN |
| aircraft_mission_design_series | B-52 ACFT |
| material_document_and_classification | QQ-A-287 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-151-8501 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-287 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 4.300 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.200 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.070 INCHES NOMINAL IN |
| SPECIAL FEATURES | OPPOSITE 35-10720-83 |
| AIRCRAFT LOCATION | SUPPORT ANGLE ON AFT COWL |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B-52 ACFT |
No substitute or cross-reference records for this part.