Abstract
This article deals with the characteristics of attitude information display facilities integrated into the electrical flight instrument system Garmin and the electrical flight instrument system of Boeing and Airbus aircraft. Article contains recommendations for improving flight safety by mitigating the influence of the negative skill transfer.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.