160D612212-15: DOOR,ACCESS,AIRCRAFT.
The DOOR,ACCESS,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, body_thickness: 0.100 INCHES NOMINAL IN, special_features: ACCESS LOWER,OUTBOARD WING PANEL WS187.14 TO 230, surface_treatment: ALODIZE AND PAINT EPOXY, peripheral_shape_style: OVAL, MULTI HOLES, end_item_identification: A-10 ACFT. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-514-9255, 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 |
| body_thickness | 0.100 INCHES NOMINAL IN |
| special_features | ACCESS LOWER,OUTBOARD WING PANEL WS187.14 TO 230 |
| surface_treatment | ALODIZE AND PAINT EPOXY |
| peripheral_shape_style | OVAL, MULTI HOLES |
| end_item_identification | A-10 ACFT |
| hole_quantity_along_width | 12 |
| hole_quantity_along_length | 8 |
| cross-sectional_shape_style | FLAT |
| material_document_and_classification | QQ-A-250/5,T3 FED SPEC SINGLE MATERIAL RESPONSE |
| surface_treatment_document_and_classification | MIL-C-5541, CLASS 1A MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-23377 MIL SPEC 2ND TREATMENT RESPONSE A |
| NSN | 1560-01-514-9255 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-5541, CLASS 1A MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-23377 MIL SPEC 2ND TREATMENT RESPONSE A |
| HOLE QUANTITY ALONG LENGTH | 8 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,T3 FED SPEC SINGLE MATERIAL RESPONSE |
| CROSS-SECTIONAL SHAPE STYLE | FLAT |
| HOLE QUANTITY ALONG WIDTH | 12 |
| SPECIAL FEATURES | ACCESS LOWER,OUTBOARD WING PANEL WS187.14 TO 230 |
| SURFACE TREATMENT | ALODIZE AND PAINT EPOXY |
| PERIPHERAL SHAPE STYLE | OVAL, MULTI HOLES |
| END ITEM IDENTIFICATION | A-10 ACFT |
| MATERIAL | ALUMINUM ALLOY 2024 |
No substitute or cross-reference records for this part.