2-7750-2: RIB,STIFFENER,AIRCRAFT.
The RIB,STIFFENER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, aircraft_location: OUTBOARD FLAP,INBOARD END, end_item_identification: B-52 AIRCRAFT, aircraft_mission_design_series: B-52, part_name_assigned_by_controlling_agency: RIB ASSEMBLY. This part is cataloged in the U.S.
Government catalog under NSN 5315-00-242-4901, 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 |
| aircraft_location | OUTBOARD FLAP,INBOARD END |
| end_item_identification | B-52 AIRCRAFT |
| aircraft_mission_design_series | B-52 |
| part_name_assigned_by_controlling_agency | RIB ASSEMBLY |
| NSN | 5315-00-242-4901 |
| OVERALL HEIGHT | 0.370 INCHES MINIMUM AND 0.375 INCHES MAXIMUM IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY2,CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
| STARTING EDGE SHAPE | STRAIGHT |
| STYLE DESIGNATOR | PLAIN |
| OVERALL LENGTH | 1.875 INCHES MINIMUM AND 1.891 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.370 INCHES MINIMUM AND 0.375 INCHES MAXIMUM IN |
| SURFACE TREATMENT | CADMIUM OVERALL |
| MATERIAL | STEEL COMP 1018 OVERALL |
No substitute or cross-reference records for this part.