4064107: GUIDE,COMBUSTION CHAMBER,AIRCRAF.
GUIDE,COMBUSTION CHAMBER,AIRCRAF. Key specifications include overall_width: 0.370 INCHES MINIMUM AND 0.400 INCHES MAXIMUM IN, overall_length: 0.580 INCHES MINIMUM AND 0.600 INCHES MAXIMUM IN, overall_diameter: 16.780 INCHES MINIMUM AND 16.810 INCHES MAXIMUM IN, end_item_identification: F100-PW-200 AIRCRAFT ENGINE, reference_data_and_literature: 2J-F100-24, FIG 136 IND 11, criticality_code_justification: ABHP AND ABMK AND ADAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-395-8181, 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.
| overall_width | 0.370 INCHES MINIMUM AND 0.400 INCHES MAXIMUM IN |
| overall_length | 0.580 INCHES MINIMUM AND 0.600 INCHES MAXIMUM IN |
| overall_diameter | 16.780 INCHES MINIMUM AND 16.810 INCHES MAXIMUM IN |
| end_item_identification | F100-PW-200 AIRCRAFT ENGINE |
| reference_data_and_literature | 2J-F100-24, FIG 136 IND 11 |
| criticality_code_justification | ABHP AND ABMK AND ADAV |
| NSN | 2840-01-395-8181 |
| OVERALL DIAMETER | 16.780 INCHES MINIMUM AND 16.810 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMK AND ADAV |
| REFERENCE DATA AND LITERATURE | 2J-F100-24, FIG 136 IND 11 |
| OVERALL LENGTH | 0.580 INCHES MINIMUM AND 0.600 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.370 INCHES MINIMUM AND 0.400 INCHES MAXIMUM IN |
| END ITEM IDENTIFICATION | F100-PW-200 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.