- Design
- Specifications
- See also
- Notes
- References
name=Falcon | image= | caption= }}{{Infobox Aircraft Type | type= | national origin= | manufacturer=ACE Air-Craft (Air-Craft Corporation of America) | designer=Orin Moore Welch | first flight= | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost=$995 in 1931 | developed from= | variants with their own articles=Welch OW-5M }} |
The ACE Aircraft Falcon Cabin Coupe was a light, low cost aircraft built during the Great Depression. DesignThe Falcon is a two-place, strut-braced high-wing conventional geared aircraft. The fuselage is constructed of welded steel tubing and fabric covering. The engine was a 42 hp two cylinder model made by ACE. A Continental A40 could be purchased for an extra $200.[1] Specifications {{Aircraft specs |ref=Popular aviation{{Full citation needed|date=February 2017}} |prime units?=kts |genhide= |crew=1 |capacity=1 |length m= |length ft=20 |length in=6 |length note= |span m= |span ft=36 |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=5 |height in=8 |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= |empty weight note= |gross weight kg= |gross weight lb= |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=ACE |eng1 type=2 Cylinder horizontally opposed |eng1 kw= |eng1 hp=42 |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=2 |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note= |rot number= |rot dia m= |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh= |max speed mph=82 |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph=75 |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=28 |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= |climb rate note= |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= }}Notes{{Empty section|date=February 2012}}References1. ^{{cite journal|title=none|magazine=Popular Aeronautics|date=February 1932|page=70}}
{{refend}} 2 : United States civil utility aircraft 1930–1939|High-wing aircraft |