200945042-35: STIFFENER,AIRCRAFT.
The STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 2.600 INCHES NOMINAL IN, overall_length: 7.200 INCHES NOMINAL IN, special_features: U/O -70; DIM. ARE STOCKSIZE MATL.; SIMILAR, M/F,FAB.
AND TRIM FROM 35-6157-2, aircraft_location: DOOR ASSY, WHEEL WELL, material_thickness: 0.040 INCHES NOMINAL IN. This part is cataloged in the U.S. Government catalog under NSN 1560-01-587-4181, 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_width | 2.600 INCHES NOMINAL IN |
| overall_length | 7.200 INCHES NOMINAL IN |
| special_features | U/O -70; DIM. ARE STOCKSIZE MATL.; SIMILAR, M/F,FAB. AND TRIM FROM 35-6157-2 |
| aircraft_location | DOOR ASSY, WHEEL WELL |
| material_thickness | 0.040 INCHES NOMINAL IN |
| end_item_identification | B-52 ACFT |
| aircraft_mission_design_series | B-52 |
| material_document_and_classification | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | CHANNEL STIFFENER |
| NSN | 1560-01-587-4181 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 7.200 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.600 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | U/O -70; DIM. ARE STOCKSIZE MATL.; SIMILAR, M/F,FAB. AND TRIM FROM 35-6157-2 |
| AIRCRAFT LOCATION | DOOR ASSY, WHEEL WELL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CHANNEL STIFFENER |
| END ITEM IDENTIFICATION | B-52 ACFT |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | B-52 |
No substitute or cross-reference records for this part.