The cookie is set by the GDPR Cookie Consent plugin and is used to store whether or not user has consented to the use of cookies. The cookie is used to store the user consent for the cookies in the category "Performance". This cookie is set by GDPR Cookie Consent plugin. The Bombardier Challenger 300 is one of the premier private jets on the market. The cookie is used to store the user consent for the cookies in the category "Other. Aircraft depicted are a sample from our fleet and is for reference only. Test of a plugin made for Challenger 300 jet for. The Aircraft carries a crew of two and up. This cookie is set by GDPR Cookie Consent plugin. Bombardier Challenger 300 for X-plane 10, reflections plugin test. The Challenger 300 is a business jet with a range of 3,100 mi (5,700 km) and manufactured by Bombardier Aerospace. The cookies is used to store the user consent for the cookies in the category "Necessary". Up to 10 Passengers Medium to Long Ranges 5-9 passengers. This cookie is set by GDPR Cookie Consent plugin. Bombardiers Challenger 300 aircraft was the first in the super-midsize business jet category. The cookie is set by GDPR cookie consent to record the user consent for the cookies in the category "Functional". The cookie is used to store the user consent for the cookies in the category "Analytics". These cookies ensure basic functionalities and security features of the website, anonymously. The maximum take-off weight is 38,850 lbs, while the maximum landing weight is 33,750 lbs.Necessary cookies are absolutely essential for the website to function properly. Landing distance (amount of runway required to land the aircraft at an average weight). The high cruise speed is Mach 0.82 or 469knot and the maximum operating altitude is 45,000ft. The main performance parameters are the aircraft’s non-stop range of 3,099 nautical miles combined with its ability to take-off from airstrips of 1.5km (0.8 nautical miles). Fuel consumption is approximately 266 gallons per hour. The aircraft is equipped with an Inter technique fuel system. The two integral wing tanks hold 6,124kg (13,501 lbs) of fuel. The AS907 is configured with four axial compressor stages, including two variable-geometry stators, a single centrifugal compressor, an effusion-cooled combustor, a two-stage high-pressure turbine, and a three-stage low-pressure turbine driving a high-efficiency fan. The engines are fitted with dual-channel FADEC (full authority digital engine control) and Hurel-Dubois thrust reversers. The aircraft has two Honeywell AS907 turbofan engines each providing 35.81kN (8,050lbs) thrust. The FMS-5000 synchronizes the operation of all lateral and vertical flight plans through coupled or advisory VNAV capability, supports time/fuel planning, and automatically flies en route, terminal, and approach procedures, as well as providing missed-approach guidance. The flight systems include a dual VHF omnidirectional radio ranger with a linked instrument landing system (VOR/ILS), a flight management system, an automatic heading and reference system (AHRS), automatic direction finding, distance measuring equipment, a global positioning system, electronic ground proximity warning receiver, TCAS II, a radar altimeter and an air data system.įully integrated with the Pro Line 21 avionics system, the Rockwell Collins FMS-5000 combines workload-reducing automation on the flight deck with true multi-sensor navigation capability. The avionics suite is based on a Rockwell Collins Pro Line 21 with four 10in x 12in liquid crystal displays, an integrated four-tube electronic flight instrumentation system (EFIS), and a two-tube engine in-flight condition monitoring system (EIFCMS). The ergonomically designed flight deck accommodates two crew. What is Fractional Ownership of a Private Jet?.
0 Comments
Leave a Reply. |
Details
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |