Editing Gulfstream V (section)

==Design==
Compared to the [[Gulfstream IV]], the engines are changed from [[Rolls-Royce RB.183 Tay|Rolls-Royce Tay]] to [[Rolls-Royce BR700]]-710A1-10 with increased thrust, higher bypass ratio, and [[Full Authority Digital Engine Control]]s (FADEC).<!--ref name= typeCert--> Operating ceiling is increased from {{cvt|45,000|to|51,000|ft|m}}.<!--ref name= typeCert--> It has thrust reversers and composite flight control surfaces.<!--ref name= typeCert--> The horizontal tail area is 30% larger, wingspan is increased from {{convert|74.6|to|93.5|ft|m|abbr=on}}, the fuselage is lengthened by {{convert|5|ft|m|abbr=on}} forward of the main entry door, and by {{cvt|2|ft|m|1}} aft of the wing.<!--ref name= typeCert--> Maximum takeoff and landing weights are increased by 15%.<ref name= typeCert/>

It has a new semi [[supercritical airfoil|supercritical]] wing for a fuel capacity of {{cvt|41,000|-|12,000|lb|t}} more than the G-IV.<!--ref name=BCA24dec2018-->
The three zone cabin is similar to the G-IV, smaller than the Global Express, while its dispatch reliability, cabin noise and [[fuel efficiency]] compare favourably against its competitors of the same era.<!--ref name=BCA24dec2018-->
Compared to the comparably priced Global Express, the GV offers more range and is more [[fuel economy in aircraft|fuel efficient]] while the Bombardier offers better runway performance, a larger cabin and a softer ride.<!--ref name=BCA24dec2018-->
BR710 overhaul comes at 8,000 hour or 10 years if it comes earlier and costs $1.25 million per engine.<ref name=BCA24dec2018>{{cite news |url= https://aviationweek.com/business-aviation/gulfstream-v-tokyo-new-york-range-10-million |title= Gulfstream V: Tokyo To New York Range For $10 Million |date= Dec 24, 2018 |author= Fred George |work= Business & Commercial Aviation}}</ref>