- Design & development
- Variants
- Specifications (SG-VI-E)
- See also
- References
- Further reading
{{Multiple issues|{{more footnotes|date=July 2017}}{{one source|date=July 2017}} }} name=SG-VI | image= | caption= }}{{Infobox Aircraft Type | type=Helicopter | national origin=Canada | manufacturer=Engineering Products of Canada Ltd. (SG-VI-C), Intercity Airlines (SG-VI-D) | designer=Bernard W Sznycer | first flight= 9 July 1947 (SG-VI-C), 2 July 1948 (SG-VI-D) | introduced= | retired= | status= | primary user= | more users= | produced= | number built= 2 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Sznycer SG-VI (aka Sznycer-Gottlieb SG-VI) was a single-engined three-seat utility helicopter designed and built in the United States and Canada in the late 1940s to the design of Bernard Sznycer, assisted by Selma Gottlieb and Engineering Products of Canada Ltd. (CanAmerican) Design & developmentInitial design work on the SG-VI began at Philadelphia in 1943 by a team led by Bernard Sznycer, including Selma Gottlieb, Harold Pitcairn and Agnew Larsen. Pitcairn and Larsen left the partnership by August 1945 when Sznycer and Intercity Airlines of Montreal, Quebec, Canada, signed a contract for the detailed design, testing and certification of a prototype helicopter to be marketed and built by the Canadian helicopter Company. The contract did not develop as planned and the first prototpye, the SG-VI-C, was built by Engineering Products of Canada Ltd., (a BF. Goodrich subsidiary at Montreal). Construction of the first prototype commenced, but with inadequate management of resources and poor supervision of workers resulting in a lack of confidence in the safety of the aircraft. A second prototpye, (SG-VI-D), was built with the sanction of Intercity Airlines and satisfactory supervision. The SG-VI-D had a crude enclosed cabin and open tubular tailboom and was powered by an {{convert|178|hp|kW|abbr=on|2}} Franklin 6GA4-165-BGF engine positioned horizontally above the tailboom driving a four-bladed main rotor with a complex control system. Given the registration CF-FGG-X and named Grey Gull, the SG-VI-D gained its type certificate in February 1951, becoming the first Canadian and British Commonwealth helicopter to do so. After certification the SG-VI-D was re-engined with a {{convert|200|hp|kW|abbr=on|2}} Franklin 6A4-200-C6 engine and offered to investors for development and production as the SG-VI-E. Sznycer eventually sold the helicopter and production rights to an investor from Brooklyn who failed to capitalise on his investment, ending the development of the SG-VI. Presently the sole remaining prototype is preserved at the Reynolds Alberta Museum, Wetaskiwin, Alberta, Canada. Variants- SG-VI-C
- Initial prototype powered by a {{convert|178|hp|kW|abbr=on|2}} Franklin 6GA4-165-BGF engine. Apparently little flown due to lack of confidence in the structural integrity of the airframe.
- SG-VI-D
- Second prototype used for flight testing and type certification.
- SG-VI-E
- the second prototype re-engined with a {{convert|200|hp|kW|abbr=on|2}} Franklin 6A4-200-C6.
Specifications (SG-VI-E){{Aircraft specs |ref=http://www.flightglobal.com/pdfarchive/view/1954/1954%20-%200674.html[1] |prime units?=imp |genhide= |crew=one |capacity=two passengers |length m= |length ft= |length in= |length note= |span m= |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=1,750 |empty weight note= |gross weight kg= |gross weight lb=2,380 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=1 |eng1 name=Franklin 6A4-200-C6 |eng1 type=6-cyl. air-cooled horizontally opposed piston engine |eng1 kw= |eng1 hp=200 |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop note= |rot number=1 |rot dia m= |rot dia ft=35 |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh= |max speed mph=88 |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph=78 |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin=760 |climb rate note=at sea level |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |power/mass= |thrust/weight= |more performance= |avionics= }}
See also{{aircontent |see also= |related= |similar aircraft= |lists= }}References1. ^{{cite journal|title=Helicopters 1954|journal=Flight|date=12 March 1954|pages=293–308|url=http://www.flightglobal.com/pdfarchive/view/1954/1954%20-%200674.html|accessdate=28 March 2013}}
{{refbegin}}{{refend}}Further reading- Milberry, Larry. Aviation in Canada: The Pioneer Decades, Vol. 1. Toronto: CANAV Books, 2008. {{ISBN|978-0-921022-19-0}}, Enter the Helicopter, Bernard Sznycer and the Grey Gull, pages 339-44
2 : Canadian helicopters|Aircraft manufactured in Canada |