
A low wing two seater.

A low wing two seater.
The A-20 of 1929 was a two-seat twin-engined aircraft.

Albert built T.E.1 piloted by Thoret participated in the French Light Plane Competition, Orly, in September 1928. He is ranked fifth.
Five TE-1 were built, with a 40hp Salmson 9-Ad. Some Albert planes crashed due to wing flutter—still rather unknown at the time and particularly affecting cantilever wings insufficiently rigid in torsion.
Bellanca acquired the license and planned to build it in the USA as “Baby Columbia,” but apparently the project failed. At least one TE-1 demonstrator must have reached the USA.
The Albert TE-1 parasol monoplane is the subject of an 8-page 1926 report (perhaps a NACA paper, though the source is identified as “CASI”) available from NASA’s archives, entitled: “Albert TE-1 training airplane.” Their online report server summarizes the abstract as: “The TE-1 is designed for the economical training of pilots and is a single seat parasol cantilever monoplane. It is nearly entirely made of wood, using a 40 HP. air-cooled Salmson A.D. 9 engine, and weighs 255 kg empty.” The report Document ID is 19930089227 and Accession ID is 93R18517 and Report Number is NACA-AC-23. The NASA notes say related information is found in L’Aeronautique, April, 1926. . “December, 1926.”.; and in NACA Aircraft Circular 23.
Formed 1926 as Avions Albert to build Albert (license Tellier- Duhamel) high-wing light monoplanes. Renamed Albert Aeronautique; in early 1930s built A-61 and A-70 two-seat monoplanes and A-140 racer for 1933 Coupe Deutsch de la Meurthe, though this latter machine was not completed in time. Construction was of wood. A-20 of 1929 was a two-seat twin-engined aircraft.
Avions Albert went bankrupt in 1935.

The Da-24 has a varying laminar profile with plant tapered, and an integrated fixed slat in the profile for around 70% of the wing, fowler flap and ailerons.
Stall: 27 kt / 31 mph / 50 kmh
Cruise: 122 kt / 140 mph / 226 kmh
VNE: 154 kt / 177 mph / 285 kmh
Empty Weight: 280 kg / 617 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 1450 ft/min / 7 m/s
Take-off distance (50ft obstacle): 450 ft / 137 m
Landing distance (50ft obstacle): 500 ft / 152 m

The 1913 Albatross Taube / Dove monoplane was designed and built by AlbatrosCompany in Germany.

The 1913 Albatros RE 1 monoplane was designed and built by Albatross Company in Germany.
The 1913 Albatross K351 2-seater biplane was designed and built by Albatross Company in Germany.
Span: 53’5″
Length: 29’6″
Weight empty: 2072 lbs

The 1913 Albatross EE 2-seater monoplane
Span: 45’11”
Length: 33’5″
Weight empty: 1323 lbs
Speed: 51 mph
1913 Albatross DL1 biplane was designed and built by Albatross Company in Germany.
Span: 46’11”
Length: 28’4″
Weight empty: 1614 lbs
Speed: 59 mph