Weymann 66
title: "Weymann 66" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1930s-french-military-aircraft", "weymann-aircraft", "twin-boom-aircraft", "trimotors", "high-wing-aircraft"] topic_path: "geography/france" source: "https://en.wikipedia.org/wiki/Weymann_66" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::data[format=table title="Infobox aircraft"]
| Field | Value |
|---|---|
| name | 66 |
| aircraft_type | multipurpose military aircraft |
| national_origin | France |
| manufacturer | Société des Avions C.T.Weymann |
| number_built | 1 |
| first_flight | 1933 |
| :: |
| name = 66 | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = multipurpose military aircraft | aim = | outcome = | related = | national_origin = France | manufacturer = Société des Avions C.T.Weymann | design_group = | designer = | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 1 | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 1933 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded =
The Weymann 66 was a French multipurpose biplane built for colonial work in the 1930s. It had a low ground clearance cabin, three engines and twin tailbooms.
Design and development
Charles Terres Weymann of Paris, France is best known as the designer of a briefly popular type of aircraft-style coachwork for fully enclosed cars, one of his businesses remaining active as a manufacturer of coaches and buses, but between 1929 and about 1934 the French company Societe des Avions C.T.Weymann designed at least a dozen aircraft. None of them reached production. The Weymann 66 was one of the last, appearing in 1933. It was designed to take part in a competition for a multirole aircraft suitable for policing operations in the French Colonies; the competition became known as Col. 3, and this was often attached to the designation both of the Weymann (as the Weymann 66 Col.3) and to the names of other competing machines. The Weymann 66 was intended to be capable of reconnaissance, including wireless and photographic work; ambulance and troop carrying; and bombing.
The layout of the Weymann 66 was determined by the wish to place the cabin as close as possible to the ground in order to provide easy access. It was a twin boom biplane, with the cabin mounted on the lower wing and with booms and its three engines at upper wing level. The flat sided cabin was a fabric covered, welded steel tube structure. Two pilots sat side by side and provided with dual control, well ahead of the leading edge. The radio operator and navigator sat behind, with the bomb aimer's position further aft. Long side windows stretched rearwards from the cockpit almost to the end of the cabin, which was about halfway between the trailing edge and the tail. The undercarriage was intended to be robust enough for rough field operation: long travel Messier oleo legs ran upwards in front of the lower leading edge to the start of the boom, forming a split axle undercarriage bearing large wheels with their centres (when parked) not far below the fuselage floor. A tailwheel was mounted under a fairing at the extreme rear of the cabin. There was also a wheel or bumper under the nose.
It was a staggered biplane with parallel chord wings of equal span. The wings had twin metal spars and were fabric covered. It was a single bay biplane, braced by N-form interplane struts; the interplane gap was large, with the upper plane well above the cabin top. The booms supporting the tail were steel, again fabric covered and mounted on the underside of the wing where they were at their deepest. At the forward end they merged into the fairings and mountings of the two outer engines, 300 hp (225 kW) Lorraine Algol radials. A third Algol was mounted centrally, on top of the wing and displaced longitudinally so the airscrew discs overlapped. Rearwards, the booms became more slender and carried the steel framed, fabric covered empennage. The tailplane and elevator was enclosed between two large endplate fins of semicircular shape, which carried horn balanced rectangular rudders. Two substantial streamlined struts ran diagonally outwards and upwards from the extreme rear of the cabin to the ends of the booms for support.
Little is known about the operational history of this aircraft, though it seems to have flown in 1933. It did not succeed in the Col. 3 competition, which was won by the Bloch MB.120. Not long afterwards Weymann withdrew from aviation to concentrate on his road vehicle business.
Specifications
|ref=Flight 1934 |prime units?=met General characteristics
|genhide= |crew=3/4 |capacity= |length m= |length ft=38 |length in=7 |length note= |span m= |span ft=50 |span in=4 |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= |width m= |width ft= |width in= |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=688 |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=7700 |empty weight note= |gross weight kg= |gross weight lb=11000 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general= Powerplant
|eng1 number=3 |eng1 name=Lorraine Algol |eng1 type=9-cylinder radials |eng1 kw= |eng1 hp=300 |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= Performance
|perfhide= |max speed kmh= |max speed mph=149 |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph=124 |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=620 |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=18000 |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
|armament= |guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |avionics= |see also= |related= |similar aircraft= |lists=
Notes
References
References
- {{harvnb. Senior. Townsin. Banks. 2002
- ''Flight'' 1 February 1934 p.107
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