You are right,I fixed it.
Dear all,
during the never-ending (and fruitless) story of making order in my archives, I found some poor photos of section and three-view drawings of the Piaggio P.140 and P.141, together with some even more poorly typed sheets with some information I think interesting.
The P.140 is labelled as (I translate) Four-engined transport aircraft. The paper is dated Septmber 10, 1943, and the proof that the project is definitely post-war is in the selection of the power plant: four Bristol Hercules Series 630/639 rated at 1.715 HP at take-off; notwithstanding taht, the accompanying text reads: The aircraft is derived form the projects of the family of the wellknown military and civil four-engined aircraft built by Piaggio company.
Main specs are: max payload 12,000 kg; cargo doors for light trucks, bay doors for parachute launch; max range 2,500 km.
Other relevant specs: wingspan 37.00 m, lenght 30.00 m, height (on the ground) 10.50 m, wing area 144.00 sq. m, empty weight (equipped) 20,000 kg, max TO weight 33,000 kg. Estimated performance are: max speed 485 km(h at 2,700 m, cruise speed 350 km/h at 3,000 m.
The section labelled Image 1 shows a load of two Jeep and two light truck Dodge WC-52 and the retractable tail ramp.
Section of Image 2 is quite interesting as seems a SAR version with an A-3 light alloy boat and two dinghies for parachute launch from the belly bays.
The P.141 in the three-view drawing bears the same September 1948 date and is labelled Four.engined aircraft for passengera and freight transport.
The project is based on the P.108C but powered by four Pratt & Whitney R-1830-92 Twin Wasp S1C3-G, rated at 1,215 HP for Take-off.
Estimated specs are: wingspan 37.00 m, lenght 26.00 m, height 8.70 m, wing area 144.00 sq m, equipped empty weight with accomodation for 5 crews and 30 passengers, max TO weight 24,500 kg, max cruise speed 370 km/h.
As far as I can tell the P.140 and the P.141 remained on paper and were not even built as mock-ups.