The Alaparma AM-11 Albatross was a single seat largely based on the AM-10.
The prototype was built by Alaparma with one 22hp SAI-Ambrosini P-25 engine.
The A-11 model was also built in Argentina under the name Albatross by OMA (Officina Meccanica Aeronautica) and this aircraft was a prototype only which first flew 28 March 1951 was reportedly powered by one McCulloch two stroke engine.
The AM-11s built in Italy used one Ambrosini P-25 or one 28hp Hirth F-10A engine.
LV-X8
Wingspan: 32.808 ft
The Alaparma AM.10 was a two-seater designed by Adriano Mantelli.
The AM-10 used the increased area wings as on the AM-9. The prototype was built by Alaparma with one 45hp Praga B-2 engine and was first flown in 1945 or 1946.
The engine was also reported as one 65hp Continental A65 and as CAN C-2 and the name Baldo was also reported for the AM-10.
At least one aircraft was built in Argentina by Mr. Mantelli with help from Mr. Robert Madsen with a Continental A65 engine and registered LV-X7.
This aircraft was referred to as the Trieste and featured twin fins rather than the usual single central fin.
Wingspan: 36.089 ft
Length: 16.404 ft
2-seat
A single example of the Alaparma AM-9 Tucano was built. It was based on the AM-8, but had slightly increased wing area and one 38hp CNA C-2 engine.
Ultralight designed by Adriano Mantelli and derived from the AM-6, but with slightly larger wings, only 3 examples were built with one 39hp ABC Scorpion, one 38hp CNA C-2 and one 22 hp Macchi B-2 engine respectively.
The first AM-8 flew on 24 July 1946.
Wingspan: 22.966 ft
Length 16.404 ft
Single seat
twin-boom aircraft with engine of pusher configuration, first built 1942.
designed by Adriano Mantelli.
Engine: Rotax 503, 46 hp
hp range: 46-65
Fuel capacity: 4.5 USG
Empty weight: 70.5 lb
Gross weight: 475 lb
Height: 8 ft
Length: 6.5 ft
Seats: 1
First flown in 1995, the G-202 is a two seat development of the single seat G-200. A tandem carbon fibre aerobatic machine.
Akrotech Europe produces the CAP 222, a version of the US AkroTech Giles G-202.
Variation:
Mudry CAP 222
Engine: Lycoming IO-360, 200 hp.
Height: 5.58 ft
Length: 19.75 ft.
Wing span: 22 ft.
Wing area: 90 sq.ft.
Fuel cap: 58 USG.
Weight empty: 950 lbs.
Gross: 600 lbs.
Speed max: 253 mph.
Cruise: 203 mph.
Range: 900 sm.
Stall: 58 mph.
ROC: 2500 fpm.
Take-off dist: 400 ft.
Landing dist: 700 ft.
Seats: 2.
Landing gear: tail wheel.
Engine: Lycoming AEIO-360EXP, 235 hp.
Loading: +/- 12g.
Engine: Lycoming, 220 hp
Wing span: 6.7 m
Wing area: 8.3 sq.m
MAUW: 726 kg
Empty weight: 431 kg
Fuel capacity: 220 lt
Max speed: 407 kph
Cruise speed: 327 kph
Minimum speed: 93 kph
Climb rate: 12.5 m/s
Seats: 2
Fuel consumption: 40 lt/hr
Price (1998): $120,000
Kit price (1998): $59,500
First flown in 1992.
Engine: Lycoming AEIO-360, 200 hp.
HP range: 180-200.
Speed max: 253 mph.
Cruise: 212 mph.
Range: 1000 sm.
Stall: 65 mph.
ROC: 3550 fpm.
Take-off dist: 300 ft.
Landing dist: 600 ft.
Fuel cap: 48 USG.
Weight empty: 750 lbs.
Gross: 1300 lbs.
Height: 5.33 ft.
Length: 18 ft.
Wing span: 20 ft.
Wing area: 75 sq.ft.
Seats: 1.
Landing gear: tail wheel.
The fs35 Harpyie was created by the Stuttgart Academic Aviation Group in 2003 as a motor glider designed for glider towing with good climbing performance and a large fuel tank, after Porsche had announced the discontinuation of model support for the PFM 3200 aircraft engine for 2005. This engine was installed in the club’s Robin DR 400 tow plane. The following requirements were defined: high aerodynamic quality in aircraft towing in the speed range 90–150 km / h, short take-off roll distance, use of an efficient diesel engine, approval as a motor glider and design as a two-seater with dual controls for training.
The design of the wing began with the assumption of 120% of the fuselage resistance of the Diamond HK36 Super-Dimona and the drive with a Thielert Centurion 1.7 with 125 hp (approx. 90 kW). The two-part Dimona wing was chosen, which was extended inwards, swept and provided with winglets. In April 2007, the moulding of the three-part half-span master model began, and in 2009 the construction of the fracture wing with integrated strain gauges began in the resulting negative form. A load test of this component on November 4, 2010 failed because the wing broke at 80% of the load to be verified. The wing construction began after reinforcement of the original construction and its mathematical proof of strength in April 2011.
The wing consists of a carbon fiber sandwich shell with carbon fiber belts and GRP -Steg. The I-shaped spar merges into a box spar in the spar stub.
The fuselage is also based on the Dimona, but the position of the wing had to be moved forward because of the heavier engine. The four-cylinder in-line engine Centurion 2.0s, now called the Continental CD-155, serves as the drive as a further development of the Centurion 1.7.
The vertical tail of the Dimona was built with the Eppler profile E 522 and increased profile depth as a GRP shell with CFRP belts in the spar. At the end of the fuselage tube, a tow coupling is installed on a boom under the tail unit.
The main landing gear comes from the Van’s Aircraft RV-8, the nose landing gear from the Super Dimona.
The first flight of the aircraft with the aircraft registration D-KTOW took place on August 13, 2019 in Schwäbisch Hall, the tug trials started at the Idaflieg 2020 summer meeting in Stendal-Borstel.
Engine: Continental CD-155, 155 hp (approx. 110 kW)
Wingspan: 17.67 m
Wing area: 16.9 m²
Wing extension: 18.5
Wing profile: FX 63-K-137 (mod)
V position: 3°
Empty weight: 600 kg
MTOW: 850 kg
Top speed: 270 km / h
Crew: 1 + 1
Designed by a group from the Akademische Fliergruppe Stuttgart, the Institute of Mechanics and Aircraft Design of Stuttgart University, and Wolf Hirth GmbH, the Fs-28 Avispa research aircraft was undergoing flight test in 1974.
The Fs-28 is constructed of resin-bonded honeycomb sandwich plastic and has a 115 hp Lycoming O-235E-2A installed in the rear. An inverted V tail is attached to twin booms. A special three-bladed propeller was developed with Hoffman to educe noise level.
The cockpit seats two side-by-side; the doors are two swing-up side panels. Fowler flaps are fitted.
Engine: 115 hp Lycoming O-235E-2A
Cruise 75%: 155 mph
Max speed: 167 mph
Landing speed: 50 mph
Range: 620 mi with 30 min res
