We do know he kept improving his prototypes and put out a new and improved model each of the next several years. L'Ala, an Italian magazine, published a description of his PL-2C, dubbed the Aerauto, in its October 1946 issue. Here's an excerpt, translated by Google and left untouched by me, despite some resulting confusion.

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The PL 2 C is an entirely metallic tourism aircraft, very interesting from several points of view: in it, in fact, are various summaries architectural and instrumental features, which should make it very convenient and economical use. From the constructive point of view it is possible notice how its structure has been greatly simplified especially about the fuselage, compared to that of a normal aircraft. This naturally it is well reflected on the cost of manufacturing and therefore on the sale price, as well as on the cost of any repairs. More given that with folded wings, its dimensions are about 2.20 m width for 6 m of length it can easily move on one normal road, always with the propeller thrust, with the possibility then to bring the pilot to the front door and then be admitted to one normal garage.

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The PL 2 C structure is of a particular type. Indeed we believe that it is patented and actually can not be denied that it is Interesting. The fuselage can be considered composed of a part of force, a real chassis, consisting of a tubular beam in welded sheet steel and a durall bodywork. On the beam are welded the castle in tubes that support the wing and the engine, as well as all the attacks of the controls, the cart, the seats and the empennages. There durall fairing covers the front of the beam and provides a to connect the wing to the engine and to the beam, as well as to form the cabin it is equipped with two side doors and is easily removable. The wing is cantilever monolongherone divided into a fixed central trunk, and in two collapsible semis. The folding is very easy; the folded wing remains suspended with the front attachment to the central trunk of the wing and fixed on special attacks placed on the corresponding drift. Structure the wing is entirely durall and the cover is 8/10 mm. The attacks are instead steel. Rivets were widely used in the wing tubulars, rather than nails, which were limited to more joints solicited. The ailerons have a metal frame in durall and a cover in canvas; they can be simultaneously lowered so as to work from flaps. The horizontal plane is of a similar structure to the wing; there fixed part (whose incidence is adjustable in flight with handwheel) is covered in durall, the mobile one is intelata. The vertical plane, split, is structurally similar to the horizontal. The trolley is tricycle with low pressure wheels, the rear wheels are equipped with brakes, while the front is connected to the pedals for the

ground displacements. The prototype engine is a 60-volt Valter that drives a propeller in a fixed step. The use of a CNA D IV is also envisaged.

 

The controls are of the usual bar and pedal type, the instrument panel the usual equipment of instruments, the brake is a pedal.

 

Features: 9,80m wingspan, 5,70m length, 1,60m height, wing surface 12sqm, elongation 8, weight empty 340kg, payload 210, total weight 550kg, wing load 45.8kg / sq m, maximum speed 190 (a 2000m), cruising 160kmh, minimum 70kmh, road speed 60kmh, practice altitude 4000m, autonomy 600km at cruising speed, max 750km, takeoff with ipersostentatori120m, landing 60m; consumption fuel 15 l / h, (ie the same as an 1100 or Ardea). The cost is 460,000 L without engine.