L3002126: PANEL,STRUCTURAL,AIRCRAFT.
The PANEL,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 47.000 INCHES NOMINAL IN, special_features: HEAT TREAT PER ST0111LA0009 TO CONDITION -T76;NHA L3022047 USED ON FATIGUE FRAME;ITEM KNOWN AS LOWER FRAME CAP;, aircraft_location: CAP,UPPER FRAME,FUSELAGE, aircraft_station_number: YF 747 TO YF 909.5, end_item_identification: B1-B AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-696-4530, 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_length | 47.000 INCHES NOMINAL IN |
| special_features | HEAT TREAT PER ST0111LA0009 TO CONDITION -T76;NHA L3022047 USED ON FATIGUE FRAME;ITEM KNOWN AS LOWER FRAME CAP; |
| aircraft_location | CAP,UPPER FRAME,FUSELAGE |
| aircraft_station_number | YF 747 TO YF 909.5 |
| end_item_identification | B1-B AIRCRAFT |
| aircraft_mission_design_series | B1-B AIRCRAFT |
| part_name_assigned_by_controlling_agency | CAP |
| NSN | 1560-01-696-4530 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CAP, UPPER FRAME, FUSELAGE |
| END ITEM IDENTIFICATION | B1-BACFT |
No substitute or cross-reference records for this part.