Product Description
The General Electric CF6 high-bypass turbofan powered a generation of widebody commercial transports from the 1970s onward, including the McDonnell Douglas DC-10, Boeing 747-200, and Airbus A300. Plaintiffs allege in publicly filed U.S. asbestos personal-injury and wrongful-death litigation that the CF6 engine build package was assembled with asbestos-composite combustor and exhaust-flange gaskets and asbestos-fabric fan-case wrap insulation. Plaintiffs allege these materials were selected for their high-temperature sealing performance in the combustor and turbine sections and for thermal management around the fan case and core.
Workers Exposed
Plaintiffs alleged in publicly filed U.S. asbestos personal-injury and wrongful-death litigation that occupational exposure to alleged CF6 asbestos components occurred among:
- Airline engine-shop mechanics performing heavy overhaul and module split
- Aircraft engine test-cell operators running post-overhaul acceptance runs
- Airline line-maintenance engine mechanics performing on-wing gasket and duct service
- U.S. Air Force propulsion technicians on CF6-derived F103/F138 engines
- Engine-shop combustor and turbine hot-section teardown technicians
Alleged exposure pathways included dust generated during gasket scraping at combustor and exhaust flanges and disturbance of fan-case wrap insulation during engine module split, re-wrap, and re-assembly.