650857CL3: RING,LOCKING,FUEL MANIFOLD.
The RING,LOCKING,FUEL MANIFOLD is a the manufacturer industrial component. Key specifications include special_features: FORM,FIT,FUNICITON, functional_description: USED ON NOZZLE CLUSTER, end_item_identification: TF33-PW-102 AIRCRAFT ENGINE, criticality_code_justification: FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2915-01-162-3175, 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.
| special_features | FORM,FIT,FUNICITON |
| functional_description | USED ON NOZZLE CLUSTER |
| end_item_identification | TF33-PW-102 AIRCRAFT ENGINE |
| criticality_code_justification | FEAT |
| general_characteristics_item_description | NICKLE ALLOY PER AMS5663; 0.374 -0.397 IN. W O/A; FLANGE 0.080 IN. NOM THK,0.825 - 0.850 IN. DIA W/CUTOUT 0.130 X 0.230 IN. NOM; 0.462 IN. NOM OD,0.294 IN. NOM ID IN |
| NSN | 2915-01-162-3175 |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | NICKLE ALLOY PER AMS5663; 0.374 -0.397 IN. W O/A; FLANGE 0.080 IN. NOM THK,0.825 - 0.850 IN. DIA W/CUTOUT 0.130 X 0.230 IN. NOM; 0.462 IN. NOM OD,0.294 IN. NOM ID IN |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SPECIAL FEATURES | FORM,FIT,FUNICITON |
| FUNCTIONAL DESCRIPTION | USED ON NOZZLE CLUSTER |
| END ITEM IDENTIFICATION | TF33-PW-102 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.