68A332068-2006: SKIN,AIRCRAFT.
The SKIN,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: TITANIUM ALLOY, thickness: 0.112 INCHES NOMINAL IN, overall_width: 22.000 INCHES NOMINAL IN, overall_length: 22.000 INCHES NOMINAL IN, special_features: TYPE 3,COMP E,COND ANNEALED,6AL-6V-2SN; PART OF -1002 SKIN,SPINDLE BAY; OPPOSITE P/N -2005 V, aircraft_location: UPPER OUTBOARD. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-235-9352, 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 | TITANIUM ALLOY |
| thickness | 0.112 INCHES NOMINAL IN |
| overall_width | 22.000 INCHES NOMINAL IN |
| overall_length | 22.000 INCHES NOMINAL IN |
| special_features | TYPE 3,COMP E,COND ANNEALED,6AL-6V-2SN; PART OF -1002 SKIN,SPINDLE BAY; OPPOSITE P/N -2005 V |
| aircraft_location | UPPER OUTBOARD |
| end_item_identification | F-15 |
| material_document_and_classification | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-235-9352 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 22.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 22.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | TYPE 3,COMP E,COND ANNEALED,6AL-6V-2SN; PART OF -1002 SKIN,SPINDLE BAY; OPPOSITE P/N -2005 V |
| AIRCRAFT LOCATION | UPPER OUTBOARD |
| END ITEM IDENTIFICATION | F-15 |
| MATERIAL | TITANIUM ALLOY |
| THICKNESS | 0.112 INCHES NOMINAL IN |
No substitute or cross-reference records for this part.