29-7470-1038: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 2.4 INCHES NOMINAL IN, overall_length: 42.9 INCHES NOMINAL IN, special_features: REINFORCEING ANGLE-INBOARD FLAP;REINF. ANGLE CTR & UPR;OPPOSIT PART DASH1037, aircraft_location: INBOARD FLAP, material_thickness: 0.040 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 1560-01-649-1024, 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 | 2.4 INCHES NOMINAL IN |
| overall_length | 42.9 INCHES NOMINAL IN |
| special_features | REINFORCEING ANGLE-INBOARD FLAP;REINF. ANGLE CTR & UPR;OPPOSIT PART DASH1037 |
| aircraft_location | INBOARD FLAP |
| material_thickness | 0.040 INCHES NOMINAL IN |
| end_item_identification | B-52 AIRCRAFT |
| aircraft_mission_design_series | B52 |
| material_document_and_classification | QQ0A0355 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT |
| NSN | 1560-01-649-1024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ0A0355 ASSN STD SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 42.9 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.4 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | REINFORCEING ANGLE-INBOARD FLAP;REINF. ANGLE CTR & UPR;OPPOSIT PART DASH1037 |
| AIRCRAFT LOCATION | INBOARD FLAP |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SUPPORT,STRUCTURAL COMPONENT,AIRCRAFT |
| END ITEM IDENTIFICATION | B-52 AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | B52 |
No substitute or cross-reference records for this part.