4036971: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 8.371 INCHES MINIMUM AND 8.371 INCHES MINIMUM AND 8.441 INCHES MAXIMUM8.441 INCHES MAXIMUM IN, engine_section_location: COMBUSTION CHAMBERCOMBUSTION CHAMBER, criticality_code_justification: AGAVAGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-087-6630, 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 |
| overall_length | 8.371 INCHES MINIMUM AND 8.371 INCHES MINIMUM AND 8.441 INCHES MAXIMUM8.441 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG F100-PW-100; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15ACFT ENG F100-PW-100; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15 A |
| engine_section_location | COMBUSTION CHAMBERCOMBUSTION CHAMBER |
| criticality_code_justification | AGAVAGAV |
| NSN | 2840-01-087-6630 |
| CRITICALITY CODE JUSTIFICATION | AGAVAGAV |
| OVERALL LENGTH | 8.371 INCHES MINIMUM AND 8.371 INCHES MINIMUM AND 8.441 INCHES MAXIMUM8.441 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBERCOMBUSTION CHAMBER |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-100; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15ACFT ENG F100-PW-100; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, EAGLE F-15 A |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.