DAA3150D362-030: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: STEEL COMP 631, overall_width: 6.000 INCHES NOMINAL IN, overall_length: 14.000 INCHES NOMINAL IN, aircraft_location: ELEVON RUB STRIP, material_thickness: 0.160 INCHES NOMINAL IN, end_item_identification: PACER SPECIAL. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-458-0372, 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 631 |
| overall_width | 6.000 INCHES NOMINAL IN |
| overall_length | 14.000 INCHES NOMINAL IN |
| special_features | NUCLEAR HARDNESS CRITICAL ITEM; MANUFACTURER SUGGESTED NAME: RUB STRIP; MATL: CRES SHT, 17-7PH COND A; HT TO TH 1050 PER H-110; OPPOSITE -029.ACTION ID 45410853 |
| aircraft_location | ELEVON RUB STRIP |
| material_thickness | 0.160 INCHES NOMINAL IN |
| end_item_identification | PACER SPECIAL |
| aircraft_mission_design_series | B-2 |
| nuclear_hardness_critical_feature | HARDENED |
| material_document_and_classification | MIL-S-25043 MIL SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1560-01-458-0372 |
| MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-25043 MIL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 14.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.000 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.160 INCHES NOMINAL IN |
| SPECIAL FEATURES | NUCLEAR HARDNESS CRITICAL ITEM; MANUFACTURER SUGGESTED NAME: RUB STRIP; MATL: CRES SHT, 17-7PH COND A; HT TO TH 1050 PER H-110; OPPOSITE -029.ACTION ID 45410853 |
| AIRCRAFT LOCATION | ELEVON RUB STRIP |
| END ITEM IDENTIFICATION | PACER SPECIAL |
| MATERIAL | STEEL COMP 631 |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| AIRCRAFT MISSION DESIGN SERIES | B-2 |
No substitute or cross-reference records for this part.