Richter, A. B., Ridenour-Bender, M., & Tsao, M. (1992). Turbine Aircraft Engine Operational Trending and JT8D Static Component Reliability Study (Report No. DOT/FAA/CT-91/10). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/93249
Richter, A. Bruce, Margaret Ridenour-Bender, and Mike Tsao. Turbine Aircraft Engine Operational Trending and JT8D Static Component Reliability Study. Report no. DOT/FAA/CT-91/10. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1992. https://rosap.ntl.bts.gov/view/dot/93249.
Richter, A. Bruce, et al. Turbine Aircraft Engine Operational Trending and JT8D Static Component Reliability Study. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1992, Report no. DOT/FAA/CT-91/10, ROSA P. https://rosap.ntl.bts.gov/view/dot/93249.
The engine subpanel of the June 1988 International Conference on Aging Airplanes identified the need to study aircraft turbine engine static components for reliability problems resulting from aging effects. This study trended in-flight shutdowns and unscheduled removal rates of JT8D, CF6, and JT3D turbine aircraft engines for the two year period of February 1988 through January 1990. Specific engine components on the JT8D engines of air carriers frequently exceeding the industry norm during the trending period were identified. This review resulted in the following types of component failures occurring: hard failures, wear and tear/inspection failures, structural failures, diagnostic troubleshooting, and maintenance errors. In addition to specific JT8D engine components being identified, an ultrasonic inspection procedure was developed for the JT8D engine outer combustor case boss.
Richter, A. B., Ridenour-Bender, M., & Tsao, M. (1992). Turbine Aircraft Engine Operational Trending and JT8D Static Component Reliability Study (Report No. DOT/FAA/CT-91/10). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/93249
Richter, A. Bruce, Margaret Ridenour-Bender, and Mike Tsao. Turbine Aircraft Engine Operational Trending and JT8D Static Component Reliability Study. Report no. DOT/FAA/CT-91/10. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1992. https://rosap.ntl.bts.gov/view/dot/93249.
Richter, A. Bruce, et al. Turbine Aircraft Engine Operational Trending and JT8D Static Component Reliability Study. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1992, Report no. DOT/FAA/CT-91/10, ROSA P. https://rosap.ntl.bts.gov/view/dot/93249.
ROSA P serves as an archival repository of USDOT-published products including scientific
findings, journal articles, guidelines, recommendations, or other information authored or co-authored by
USDOT or funded partners. As a repository, ROSA P retains documents in their original published format to
ensure public access to scientific information.
Links with this icon indicate that you are leaving a Bureau of Transportation
Statistics (BTS)/National Transportation Library (NTL)
Web-based service.
Thank you for visiting.
You are about to access a non-government link outside of
the U.S. Department of Transportation's National
Transportation Library.
Please note: While links to Web sites outside of DOT are
offered for your convenience, when you exit DOT Web sites,
Federal privacy policy and Section 508 of the Rehabilitation
Act (accessibility requirements) no longer apply. In
addition, DOT does not attest to the accuracy, relevance,
timeliness or completeness of information provided by linked
sites. Linking to a Web site does not constitute an
endorsement by DOT of the sponsors of the site or the
products presented on the site. For more information, please
view DOT's Web site linking policy.
To get back to the page you were previously viewing, click
your Cancel button.