The PLATE,MOUNTING,CASE,TURBINE is a the manufacturer industrial component. Key specifications include fsc_application_data: AIRCRAFT JET ENGINE, end_item_identification: ENGINE MODEL TF33, general_characteristics_item_description: CRES,AMS 5504,ROCKWELL C30-38 HARDNESS,2.624 IN. LG,2.212 IN.W,0.120-0.130 IN.
THK IN. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 3030-00-528-6756, 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.
| fsc_application_data | AIRCRAFT JET ENGINE |
| end_item_identification | ENGINE MODEL TF33 |
| general_characteristics_item_description | CRES,AMS 5504,ROCKWELL C30-38 HARDNESS,2.624 IN. LG,2.212 IN.W,0.120-0.130 IN. THK IN |
| NSN | 3030-00-528-6756 |
| END ITEM IDENTIFICATION | RG-33 MRAP |
| NOMINAL EFFECTIVE OUTSIDE LENGTH | 47.000 INCHES IN |
| ANGLE | 38.0 DEGREES |
| PERFORMANCE TYPE | STANDARD CAPACITY |
| STRENGTHENING FEATURE | SYNTHETIC CORD |
| NOMINAL WIDTH | 0.500 INCHES IN |
| STYLE DESIGNATOR | PLAIN |
| MATERIAL | FIBER AND RUBBER BODY |