BRACKET ASSEMBLY,MANIFOLD,TURBIN. Key specifications include material: RUBBER SEALING ELEMENT, seal_width: 0.531 INCHES NOMINAL IN, construction: SOLID, housing_bore_diameter: 5.502 INCHES MINIMUM IN, accommodated_shaft_diameter: 4.435 INCHES MINIMUM AND 4.441 INCHES MAXIMUM IN, cross-sectional_shape_style: SINGLE LIP. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-980-2656, 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 | RUBBER SEALING ELEMENT |
| seal_width | 0.531 INCHES NOMINAL IN |
| construction | SOLID |
| housing_bore_diameter | 5.502 INCHES MINIMUM IN |
| accommodated_shaft_diameter | 4.435 INCHES MINIMUM AND 4.441 INCHES MAXIMUM IN |
| cross-sectional_shape_style | SINGLE LIP |
| NSN | 2840-00-980-2656 |
| FSC APPLICATION DATA | AIRCRAFT JET ENGINE |
| END ITEM IDENTIFICATION | ENGINE MODEL TF33 |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | CRES,AMS 5504 BRACKET MATERIAL,ROCKWELL C30-38 HARDNESS,3.955 IN. LONG LEG LG,1.195 IN. SHORT LEG LG,90 DEG ANGLE,1.516 IN.O/A W,0.058-0.068 IN. BRACKET MATERIAL THK IN |