![]() Steven Dzierzynski, Aerospace Engineer, Avionics and Electrical Systems Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590 telephone 51 End Further Info End Preamble Start Supplemental Information SUPPLEMENTARY INFORMATION: Background Start Further Info FOR FURTHER INFORMATION CONTACT: Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. The address for Docket Operations is U.S. The AD docket contains this final rule, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. and 5 p.m., Monday through Friday, except Federal holidays. FAA-2022-0398 or in person at Docket Operations between 9 a.m. You may examine the AD docket on the internet atīy searching for and locating Docket No. It is also available on the internet atīy searching for and locating Docket No. For information on the availability of this material at the FAA, call 20. ADDRESSES:įor service information identified in this final rule, contact Bombardier Business Aircraft Customer Response Center, 400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada telephone 51 You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of October 19, 2022. The FAA is issuing this AD to address the unsafe condition on these products. This AD requires revising the existing airplane flight manual (AFM) to provide the flightcrew with a new limitation and procedure for operation during certainįlight modes. This AD was prompted by reports that during certain operating modes, the flight guidance/autopilot does not account for engine failure while capturing an altitude. The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model CL-600-1A11 (600), CL-600-2A12 (601), and CL-600-2B16 (601-3A and 601-3R Variants) airplanes. Provide legal notice to the public or judicial notice to the courts.įederal Aviation Administration (FAA), Department of Transportation (DOT). Rendition of the daily Federal Register on does not Until the ACFR grants it official status, the XML Legal research should verify their results against an official edition of The official SGML-based PDF version on, those relying on it for The material on is accurately displayed, consistent with While every effort has been made to ensure that Regulatory information on with the objective ofĮstablishing the XML-based Federal Register as an ACFR-sanctioned The OFR/GPO partnership is committed to presenting accurate and reliable Register (ACFR) issues a regulation granting it official legal status.įor complete information about, and access to, our official publications Informational resource until the Administrative Committee of the Federal This prototype edition of theĭaily Federal Register on will remain an unofficial Each document posted on the site includes a link to theĬorresponding official PDF file on. The documents posted on this site are XML renditions of published Federal Register, and does not replace the official print version or the official It is not an official legal edition of the Federal First delivery was in January 1996.This site displays a prototype of a “Web 2.0” version of the dailyįederal Register. First flight with CF-34-3A engines was in September 1994, first flight with the CF-34-3B engines was on March 17 1995, with Transport Canada certification granted that September. Many other minor changes were incorporated based on Bombardier's experience with the Canadair Regional Jet. Improvements include an advanced Collins ProLine IV EFIS avionics system with colour displays, higher weights, CF-34-3B turbofans and increased fuel tankage. Available from 1989, the 601-3R was an extended range model with higher weights (the range increase modifications can also be retrofitted to earlier 601-3As).įurther improvements to the basic design led to the Challenger 604. First flying in 1987, this variant introduced an EFIS glass flightdeck and upgraded engines. Subsequent development of the Challenger led to the 601-3A. The 600 was dropped from the model line in 1983. The 601 first flew on Apand for a time was offered alongside the 600. Another important change was the addition of winglets, which are also offered as a retrofit to earlier aircraft. Troubles with the Avco Lycoming powered Challenger 600 led Canadair (now a division of Bombardier) to develop a vastly improved variant in the form of the General Electric CF-34 powered Challenger 601. The Challenger 601 addressed the original CL-600 Challenger's weight problems and replaced the troubled ALF-502 turbofans, creating a highly successful full size corporate jet.
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