1602M28P02: SLIDER,DIVERGENT FLAP,TURBINE EN.
SLIDER,DIVERGENT FLAP,TURBINE EN. Key specifications include material: NICKEL ALLOY, overall_width: 0.443 INCHES MINIMUM AND 0.447 INCHES MAXIMUM IN, overall_length: 0.510 INCHES MINIMUM AND 0.514 INCHES MAXIMUM IN, end_item_identification: F110-GE-100 AIRCRAFT ENGINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-357-4327, 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 | NICKEL ALLOY |
| overall_width | 0.443 INCHES MINIMUM AND 0.447 INCHES MAXIMUM IN |
| overall_length | 0.510 INCHES MINIMUM AND 0.514 INCHES MAXIMUM IN |
| end_item_identification | F110-GE-100 AIRCRAFT ENGINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-357-4327 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 0.510 INCHES MINIMUM AND 0.514 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.443 INCHES MINIMUM AND 0.447 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY |
No substitute or cross-reference records for this part.