428988CL3: GASKET.
The GASKET is a the manufacturer industrial component. Key specifications include material: STEEL COMP 410 OVERALL, outside_diameter: 1.625 INCHES MINIMUM AND 1.635 INCHES MAXIMUM IN, special_features: CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIAL PROPERTIES AND MANUFACTURING PROCESS, style_designator: CIRCULAR, aperture_diameter: 1.035 INCHES MINIMUM AND 1.045 INCHES MAXIMUM IN, gage_ring_thickness: 0.123 INCHES MINIMUM AND 0.138 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 5330-00-944-1565, 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 410 OVERALL |
| outside_diameter | 1.625 INCHES MINIMUM AND 1.635 INCHES MAXIMUM IN |
| special_features | CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIAL PROPERTIES AND MANUFACTURING PROCESS |
| style_designator | CIRCULAR |
| aperture_diameter | 1.035 INCHES MINIMUM AND 1.045 INCHES MAXIMUM IN |
| gage_ring_thickness | 0.123 INCHES MINIMUM AND 0.138 INCHES MAXIMUM IN |
| end_item_identification | W/S: AIRCRAFT, STRATOLIFTER C-135; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT TF33-PW-102 (C-135, EC-135H/K/P); AIRCRAFT, C-18A, EC-18B A |
| criticality_code_justification | FEAT |
| material_document_and_classification | AMS 5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 5330-00-944-1565 |
| GAGE RING THICKNESS | 0.123 INCHES MINIMUM AND 0.138 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| STYLE DESIGNATOR | CIRCULAR |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OUTSIDE DIAMETER | 1.625 INCHES MINIMUM AND 1.635 INCHES MAXIMUM IN |
| APERTURE DIAMETER | 1.035 INCHES MINIMUM AND 1.045 INCHES MAXIMUM IN |
| SPECIAL FEATURES | CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIAL PROPERTIES AND MANUFACTURING PROCESS |
| END ITEM IDENTIFICATION | W/S: AIRCRAFT, STRATOLIFTER C-135; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT TF33-PW-102 (C-135, EC-135H/K/P); AIRCRAFT, C-18A, EC-18B A |
| MATERIAL | STEEL COMP 410 OVERALL |
No substitute or cross-reference records for this part.