BACS40X011B028: SHIM STOCK,LAMINATED.
The SHIM STOCK,LAMINATED is a the manufacturer industrial component. Key specifications include width: 1.100 INCHES NOMINAL IN, length: 2.800 INCHES NOMINAL IN, material: GLASS CLOTH, special_features: THESE SHIMS ARE INTENDED FOR USE IN GRAPHITE COMPOSITE STRUCTURE, lamination_quantity: 10, lamination_thickness: 0.004 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 9535-01-501-1706, 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.
| width | 1.100 INCHES NOMINAL IN |
| length | 2.800 INCHES NOMINAL IN |
| material | GLASS CLOTH |
| special_features | THESE SHIMS ARE INTENDED FOR USE IN GRAPHITE COMPOSITE STRUCTURE |
| lamination_quantity | 10 |
| lamination_thickness | 0.004 INCHES NOMINAL IN |
| end_item_identification | MV-22 AIRCRAFT (V-22 LRIP 1 E-NSN ISIL) |
| cross-sectional_thickness | 0.045 INCHES NOMINAL IN |
| criticality_code_justification | AGAV |
| material_document_and_classification | BMS8-139, CLASS 1, STYLE 120 OR 220 MFR REF SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | SHIM, PEELABLE, LAMINATED, FIBERGLASS, SQUARE AND RECTANGULAR; INAVY: SHIM |
| NSN | 9535-01-501-1706 |
| LENGTH | 2.800 INCHES NOMINAL IN |
| CROSS-SECTIONAL THICKNESS | 0.045 INCHES NOMINAL IN |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | BMS8-139, CLASS 1, STYLE 120 OR 220 MFR REF SINGLE MATERIAL RESPONSE |
| LAMINATION QUANTITY | 10 |
| SPECIAL FEATURES | THESE SHIMS ARE INTENDED FOR USE IN GRAPHITE COMPOSITE STRUCTURE |
| LAMINATION THICKNESS | 0.004 INCHES NOMINAL IN |
| WIDTH | 1.100 INCHES NOMINAL IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHIM, PEELABLE, LAMINATED, FIBERGLASS, SQUARE AND RECTANGULAR; INAVY: SHIM |
| END ITEM IDENTIFICATION | MV-22 AIRCRAFT (V-22 LRIP 1 E-NSN ISIL) |
No substitute or cross-reference records for this part.