Gulfstream G550 Warning: You are not logged in. Your IP address will be publicly visible if you make any edits. If you log in or create an account, your edits will be attributed to your username, along with other benefits.Anti-spam check. Do not fill this in! == Specifications == [[File:Gulfstream G500 3-view line drawing.svg|thumb|370px|Gulfstream G500]] {{Aircraft specs |ref=G550 Brochure<ref>{{Cite web |url= http://www.gulfstream.com/images/uploads/brochures/aircraft/Gulfstream_G550_BrochureV2.pdf |title= G550 Brochure |publisher= Gulfstream |date= July 2016}}</ref> |prime units?=kts <!-- General characteristics --> |crew=2 pilots, 0β2 attendants |capacity=14β19 passengers / {{cvt|6200|lb|0}} payload :* '''Cabin dimensions: height Γ width Γ length''' {{cvt|1.88|x|2.24|x|13.39|m|ftin|order=flip}}; total length including baggage hold: {{cvt|50|ft|1|in|m|2}} :* '''Cabin volume:''' {{cvt|1669|cuft|2}}; usable baggage compartment volume: {{cvt|170|cuft|2}} :* '''[[Cabin altitude]]:''' {{cvt|6000|ft|0}}<ref>{{cite press release |url= http://gulfstreamnews.com/news/gulfstream-v-in-service-for-10-years |title= Gulfstream V in Service For 10 years |publisher= Gulfstream |date= June 18, 2007 }}</ref> |length ft=96 |length in=5 |length note= |span ft=93 |span in=6 |span note= |height ft=25 |height in=10 |height note= |wing area sqft= |wing area note= |aspect ratio=<!-- sailplanes --> |airfoil=<!--'''root:''' [[NACA airfoil|NACA ]]; '''tip:''' [[NACA airfoil|NACA ]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019}}</ref>--> |empty weight lb=48300 |empty weight note= |gross weight lb=54500 |gross weight note= |max takeoff weight lb=91000 |max takeoff weight note=<br> *'''Maximum landing weight:''' {{cvt|75300|lb|0}} |fuel capacity= {{cvt|41300|lb|0}} |more general= <!-- Powerplant --> |eng1 number=2 |eng1 name=[[Rolls-Royce BR700#BR710|Rolls-Royce BR710]] C4-11 |eng1 type=[[turbofan]] engines |eng1 lbf=15385 |eng1 note= <!-- Performance --> |max speed note= |max speed mach= |cruise speed kts= |cruise speed note= |stall speed kts= |stall speed note= |never exceed speed kts= |never exceed speed note= |minimum control speed kts= |minimum control speed note= |range nmi=6750 |range note=<br> * '''High Speed Cruise:''' M0.85 at {{cvt|41000|ft|0}} *'''Long Range Cruise:''' M0.80 at {{cvt|41000|ft|0}} *'''Maximum Mach Operating (MMO):''' M0.885 at {{cvt|41000|ft|0}} |ferry range nmi= |ferry range note= |endurance=<!-- if range unknown --> |ceiling ft=51000 |ceiling note= |climb rate ftmin= |climb rate note= |time to altitude= |wing loading lb/sqft= |wing loading note= |fuel consumption lb/mi= |thrust/weight= |more performance=<br/> *'''Take-off run:''' {{cvt|5910|ft|0}} *'''Landing run:''' {{cvt|2770|ft|0}} |avionics= }} Summary: Please note that all contributions to Christianpedia may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here. You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see Christianpedia:Copyrights for details). Do not submit copyrighted work without permission! Cancel Editing help (opens in new window) Discuss this page