- Design and development
- Operational history
- Specifications
- Notes
- References
The Aero-Club des Cheminots Aerofer was a French-built light utility aircraft of the mid-1950s. name=Aerofer | image=Aerofer edited-2.jpg | caption=The sole Aerofer at Guyancourt airfield near Paris in June 1963 }}{{Infobox Aircraft Type | type=light utility aircraft | national origin=France | manufacturer=Aero-Club des Cheminots | designer=Aero-Club des Cheminots | first flight=1954 | introduced=1954 | retired= | status=no longer registered | primary user=aero club | more users= | produced= | number built=1 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
Design and developmentThe Aerofer was designed and built by members of the Aero-Club des Cheminots as a co-operative project. It was a small single-seat low-winged aircraft. The Aerofer had a two-spar wooden wing with fabric covering. The fuselage was of wooden construction with a combination of fabric and plywood covering. The tailwheel undercarriage was fixed. The aircraft was powered by a 50 h.p. Walter Mikron four-cylinder air-cooled engine built by Aster.[1] Operational historyThe Aerofer was completed in 1954 and was operated until 1964 by the members of the Aero-Club des Cheminots, based at Guyancourt airfield (now closed) to the west of Paris.[2] Its extremely small dimensions meant that it was semi-aerobatic, despite the low-powered engine fitted. Only one example of the design was completed.[3] By 1965 the aircraft, registered as F-PERS with a Certificat de Navigabilite Restreint d'Aeronef (CNRA)[4] was owned by the Aero-Club Etienne Boileau and based at Fontenay-Tresigny airfield.[5] It was no longer on the CNRA register by March 1983.[6] Specifications{{Aircraft specs |ref=Green |prime units?=imp |genhide= |crew=1 |capacity=1 |length m= |length ft= |length in= |length note= |span m= |span ft=26 |span in=0 |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= |empty weight note= |gross weight kg= |gross weight lb=1112 |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=Walter Mikron I |eng1 type=4-cyl. inverted air-cooled piston engine |eng1 kw= |eng1 hp=50 |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= |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=90 |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= |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=
|armament= |guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |other armament= |avionics= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
Notes1. ^Green, 1965, p.34 2. ^Butler, 1964, p.115 3. ^Green, 1965, p.34 4. ^Burnett, 1983, p.111 5. ^Green, 1965, p.34 6. ^Burnett, 1983, p.112
References{{refbegin}}- {{cite book|last=Butler|first=P.H.|title=French Civil Aircraft Register 1964|year=1964|publisher=Merseyside Society of Aviation Enthusiasts|isbn=}}
- {{cite book|last=Burnett|first=I.P.|title=Civil Aircraft Registers of France 1983|year=1983|publisher=Air-Britain (Historians) Ltd|isbn=0-85130-104-5}}
- {{cite book|last=Green|first=William|title=The Aircraft of the World|year=1965|publisher=Macdonald & Co (Publishers) Ltd|isbn=}}
{{refend}} 4 : French civil utility aircraft 1950–1959|Low-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1954 |