35-8226-193: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, overall_length: 7.300 INCHES NOMINAL IN, special_features: USED ON-516,-522 AND -545;TEMPER T3;FINISH F-2.115, aircraft_location: FWD FIREWALL INSTL, material_thickness: 0.025 INCHES NOMINAL IN, aircraft_mission_design_series: B-52 AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-152-2152, 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 |
| overall_length | 7.300 INCHES NOMINAL IN |
| special_features | USED ON-516,-522 AND -545;TEMPER T3;FINISH F-2.115 |
| aircraft_location | FWD FIREWALL INSTL |
| material_thickness | 0.025 INCHES NOMINAL IN |
| aircraft_mission_design_series | B-52 AIRCRAFT |
| material_document_and_classification | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-152-2152 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 7.300 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.025 INCHES NOMINAL IN |
| SPECIAL FEATURES | USED ON-516,-522 AND -545;TEMPER T3;FINISH F-2.115 |
| AIRCRAFT LOCATION | FWD FIREWALL INSTL |
| MATERIAL | ALUMINUM ALLOY |
| AIRCRAFT MISSION DESIGN SERIES | B-52 AIRCRAFT |
No substitute or cross-reference records for this part.