68A332192-2001: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 16.500 INCHES NOMINAL IN, overall_length: 17.500 INCHES NOMINAL IN, special_features: DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332201 F-15A,B BLK12&UP, F-15CCUM1-253, F-15D CUM1-41 A, aircraft_location: EMPENAGE SUPPORT BEAM CLOSURE, material_thickness: 0.040 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-467-4191, 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 | 16.500 INCHES NOMINAL IN |
| overall_length | 17.500 INCHES NOMINAL IN |
| special_features | DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332201 F-15A,B BLK12&UP, F-15CCUM1-253, F-15D CUM1-41 A |
| aircraft_location | EMPENAGE SUPPORT BEAM CLOSURE |
| material_thickness | 0.040 INCHES NOMINAL IN |
| aircraft_station_number | FS826 |
| side_for_which_designed | LEFT SIDE |
| aircraft_mission_design_series | F-15A,B,C,D A |
| material_document_and_classification | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-467-4191 |
| AIRCRAFT STATION NUMBER | FS826 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,T62 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 17.500 INCHES NOMINAL IN |
| OVERALL WIDTH | 16.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332201 F-15A,B BLK12&UP, F-15CCUM1-253, F-15D CUM1-41 A |
| AIRCRAFT LOCATION | EMPENAGE SUPPORT BEAM CLOSURE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-15A,B,C,D A |
No substitute or cross-reference records for this part.