35-8233-508: FORMER,AIRCRAFT.
The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL COMP 4130, overall_width: 2.800 INCHES NOMINAL IN, overall_length: 26.000 INCHES NOMINAL IN, special_features: ANNEALED;DECARB LIMIT,AMS 6350; HEAT TREATED 180,000 TO 200,000;OPPOSITE P/N -507, aircraft_location: CAP ANGLE,INBOARD AND OUTBOARD STRUT FAIRING, material_thickness: 0.040 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-150-5201, 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 | STEEL COMP 4130 |
| overall_width | 2.800 INCHES NOMINAL IN |
| overall_length | 26.000 INCHES NOMINAL IN |
| special_features | ANNEALED;DECARB LIMIT,AMS 6350; HEAT TREATED 180,000 TO 200,000;OPPOSITE P/N -507 |
| aircraft_location | CAP ANGLE,INBOARD AND OUTBOARD STRUT FAIRING |
| material_thickness | 0.040 INCHES NOMINAL IN |
| side_for_which_designed | RIGHT SIDE |
| aircraft_mission_design_series | B-52 |
| material_document_and_classification | AN-QQ-S-685 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-150-5201 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AN-QQ-S-685 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 26.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.800 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL IN |
| SPECIAL FEATURES | ANNEALED;DECARB LIMIT,AMS 6350; HEAT TREATED 180,000 TO 200,000;OPPOSITE P/N -507 |
| AIRCRAFT LOCATION | CAP ANGLE,INBOARD AND OUTBOARD STRUT FAIRING |
| MATERIAL | STEEL COMP 4130 |
| SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | B-52 |
No substitute or cross-reference records for this part.