160J611335-13: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_length: 15.000 INCHES NOMINAL IN, aircraft_location: WING CTR. PANEL FRONT-SPAR WEB, material_thickness: 0.094 INCHES NOMINAL IN, aircraft_station_number: WS44.5 TO WS54.0, side_for_which_designed: BOTH SIDES.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-489-5350, 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 | 15.000 INCHES NOMINAL IN |
| special_features | AND WS79.0 LH;AL SHP/T6511;DIMENSIONS ARE STOCKSIZE,AND 10136-1702; NHA-2; MANF. SUGGEST NAME(TEE-SPCL,A/OA-10A WING CTR. PANEL REPAIR-FRT. SPAR WEB) A |
| aircraft_location | WING CTR. PANEL FRONT-SPAR WEB |
| material_thickness | 0.094 INCHES NOMINAL IN |
| aircraft_station_number | WS44.5 TO WS54.0 |
| side_for_which_designed | BOTH SIDES |
| aircraft_mission_design_series | 10A A |
| material_document_and_classification | QQ-A/200-11 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-489-5350 |
| AIRCRAFT STATION NUMBER | WS44.5 TO WS54.0 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A/200-11 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 15.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.094 INCHES NOMINAL IN |
| SPECIAL FEATURES | AND WS79.0 LH;AL SHP/T6511;DIMENSIONS ARE STOCKSIZE,AND 10136-1702; NHA-2; MANF. SUGGEST NAME(TEE-SPCL,A/OA-10A WING CTR. PANEL REPAIR-FRT. SPAR WEB) A |
| AIRCRAFT LOCATION | WING CTR. PANEL FRONT-SPAR WEB |
| MATERIAL | ALUMINUM ALLOY 7075 |
| SIDE FOR WHICH DESIGNED | BOTH SIDES |
| AIRCRAFT MISSION DESIGN SERIES | 10A A |
No substitute or cross-reference records for this part.