Alaparma AM.65 Baldo / AM.75 Baldo

The Alaparma Baldo was a two-seat light monoplane produced in Italy shortly after World War II. Designed by Adriano Mantelli, it featured an egg-shaped fuselage with cabin doors that hinged upwards and to the back. The conventional tailplane with single fin and rudder was carried on twin booms, either side of a pusher engine installation. The undercarriage consisted of a single mainwheel under the fuselage pod, a small tailwheel not far behind it, and outrigger wheels on the wingtips.

AM.65 Baldo

Produced 1949-51, approximately 35 were built in two versions: the AM.65 with Walter Mikron engine and AM.75 with Praga D engine.

The Italian Air Force operated 10 aircraft until 1951.

Gallery

AM.75
Engine: 1 × Praga D, 56 kW (75 hp)
Wingspan: 7.00 m (23 ft 0 in)
Wing area: 8.5 m2 (91 sq ft)
Length: 5.08 m (16 ft 8 in)
Height: 1.45 m (4 ft 9 in)
Empty weight: 280 kg (617 lb)
Gross weight: 490 kg (1,080 lb)
Maximum speed: 217 km/h (135 mph; 117 kn)
Cruising speed: 192 km/h (119 mph; 104 kn) (75% power)
Climb to 3280 ft: 5 min
Service ceiling: 15,745 ft
Range: 660 km (410 mi; 356 nmi)
Seats: 2

Alaparma AP.65 Baldo
AM-75

Alaparma AM.12

The Alaparma AM-12 was a two-seat aircraft derived from the Am-8/AM-10, but with a new and larger wing to make the type suitable as powered glider. Further changes compared to the AM-8 and AM-10 were a revised u/c arrangement with small tail wheels under the twin vertical tail instead of a single tail wheel under the rear fuselage.

It was first flown on 12 November 1954 as a glider.

Later it received one 75hp Praga D engine.

The aircraft was evaluated by the Italian AF and possibly up to three or four AM-12s were built.

One of the AM-12 after having been re-engined with one 350lb Turboméca Palas turbojet engine as the AM-12P and it was flown in this form in 1962.

AM-12P

Again, the aircraft was evaluated by the Italian AF. Further development of the AM-12 was halted.

AM-12P

The aircraft established several FAI altitude records attaining 28,661ft with Praga D75 engine and 21.981ft with Palas engine.

Wingspan: 39.375 ft
Length: 18.042 ft
Height: 4.667 ft

Alaparma AM-11 Albatross            

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

Alaparma A.M.10

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

Akrotech Europe

A subsidiary of Aeronautical Service, Akrotech Europe has taken over assets of Avions Mudry et Cie, continuing production of the CAP 10B two-seat aerobatic and club trainer (first flown 1968) and CAP 232 single-seat aerobatic competition monoplane (first flown July 1994). Also produces the CAP 222, a version of the US AkroTech Giles G-202 two-seat kit-built aerobatic competition aircraft and trainer.

Akrotech Aviation Giles G-202

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