Aircraft

Paradise Aircraft P-1

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The Paradise P-1 complies with all aspects of the Light Sport Aircraft (LSA) ASTM standards, that specify the design and performance requirements of the two types of LSA aircraft. Special Light Sport Aircraft (SLSA) and Experimental Light Sport Aircraft (ELSA). Easy to service and maintain and if registered as an E-LSA can have even the annual inspection made by the owner. 2009 Price: US$108300

The P-1 is constructed using 4130 steel tube frame welded and is covered with aviation grade aluminum. Powered by a 100 HP Rotax 912 ULS, it offers short field take off and landing performance, with excellent climbing rate and cruise speed. The cowling can be removed by one person making it easy to access every component for inspection and maintenance

It is a high wing, two seat, side by side aircraft similar to a Cessna 150, but that is where the similarity ends.
The combination of its wing design and large moving horizontal tail (stabilator) produces a very gentle yet stable aircraft with a good stall characteristic. This, coupled with the ruggedness of its landing gear, dual control system, and a wide range of optional, makes it an excellent trainer. Taxiing is easy with the pedal steered nose gear and large hydraulic brake system.

The large cabin width (43.3 inches), panel mounted yoke, unhindered floor space providing lots of leg room, with, the standard leather upholstery can accommodate two large occupants in plush comfort.

The behind the seat baggage space (largest of its category), with 75 lbs of load capacity and over 18 cubic ft of available space can carry a lot of luggage, including 2 golf bags plus a cooler or perhaps your fishing and camping gear. No hotel, remove the seat, place a sleeping bag for a 6 ft + person to sleep in comfort.
The inherent “nose down” level flight characteristic, offers a superb ahead and all around visibility.

2009 Paradise P-1
Engine: Rotax 912 ULS, 100 hp
Propeller: 3-blade Warp Drive
Gross weight: 599 kg / 1320 lb
Empty weight, std: 370 kg / 815 lb
Useful load, std: 505 lb
Usable fuel, std: 26 USG
Vne: 125 kt
Best rate of climb, SL, two passengers: 800 fpm / 4 m/s
Best rate of climb, SL, one passenger: 1000 fpm
Max cruise speed: 105 kt
Stall: 35 kt / 40 mph / 64 kmh
Range: 630 nm
Takeoff ground roll, one passenger: 260 ft
Landing over 50 ft. obstacle: 760 ft
Glide Ratio: 13/1

Papa 51 Thunder Mustang

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The Thunder Mustang was originally designed by Martin Hollmann for Dan Denny in 1988. Martin later finished the design and performed the flutter analysis for high performance aircraft.

Papa 51 Inc has produced kits to build Thunder Mustang two-seat 75 percent-scale representation of P-51 fighter, first flown 1996. Papa51 Co. Ltd., the original manufacturer of the Thunder Mustang is no longer in business.

The Thunder Mustang was not in production. The Thunder Builders Group L.L.C. acquired the assets required to manufacture the Thunder Mustang through foreclosure on a loan. These assets were posted as for sale.

First flown in 1996, the two seat Thunder Mustang offers its owner a unique blend of speed, maneuverability and mystique. Given the power to weight ratio, it outperforms the original North American P-51D fighter at a fraction of the cost.

Thunder Mustang kits are complete, containing everything from the spinner, prop and engine to the tail wheel, less your choice of instruments, avionics, paint and upholstery. Extensive prefabrication helps reduce construction time and eliminate hassles. The complete use of carbon fiber in the structure produces incredible strength and light weight.

The 8 foot diameter, constant-speed 4-blade prop is manufactured by MT Propellers. The gear box ratio of 2.8:1 turns the prop at 1607 RPM for the optimum ratio for the best prop efficiency and high speed with the V-12 turning 4500 RPM. The 100 lb. propeller is of composite construction utilizing a wood core, which is self-dampening and non-fatiguing. This saves weight compared to metal propellers and reduces the gyroscopic effect of the prop on takeoff.

Walter-powered Thunder Mustang

Thunder Mustang
Powerplant: Falconer V-12, 640hp
Displacement: 601 cubic inches
Propeller: MT 94″ 4-blade constant speed
Length: 24.2 ft
Frontal Area: 8.1 sq. ft
Wing Span: 23.8 ft
Wing Area: 104 sq. ft
Height: 9.4 ft
Maximum Level Speed @ Sea Level: 326 kts (375 mph, 603 kph)
Cruise Speed: @ 75% Power: 300 kts (340 mph, 547 kph)
Vne (never exceed): 439 kts
Vsl (stall, clean): 77 kts
Vso (stall, in landing config.): 68 kts
Range: 1300 nautical miles
Rate of Climb @ gross: 5200 ft/min
Takeoff distance: 1000 ft
Landing distance: 2500 ft
Service Ceiling: 25,000 ft.
Gross Weight: 3200 lb
Empty Weight: 2200 lb
Useful Load: 1000 lb
Payload w/full Fuel: 400 lb
Basic Fuel Capacity: 102 gallons (in wings)
Baggage Capacity: 50 lb
Wing Loading: 28.84 lbs/sq.ft
Power Loading: 4.69 lbs/hp
Design Limit Load Factor: +9g / -6g @ 2600 lb / +7.3 / -4.9 g @ 3200 lb
Vx (best angle of climb): 87 kts
Vy (best rate of climb): 156 kts
Va (design maneuvering): 222 kts
Vfe (max flaps extended): 165 kts
Vle (max landing gear extended): 148 kts
Best Glide: 153 kts
Seats: 2

Engine: Falconer V-12, 640 hp
Wing span: 7.25 m
Wing area: 9.57 sq.m
MAUW: 1361 kg
Empty weight: 907 kg
Fuel capacity: 401 lt
Max speed: 603 kph
Cruise speed: 555 kph
Minimum speed: 109 kph
Climb rate: 26 m/s
Seats: 2
Kit price (1998): $195,000

Papa 51 Inc.

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Has produced kits to build Thunder Mustang two-seat 75 percent-scale representation of P-51 fighter, first flown 1996.

1997-8: 102 N. Kings RD. Nampa, ID 8368, USA.

Papa 51 Co. Ltd., the original manufacturer of the Thunder Mustang is no longer in business.
The Thunder Mustang was not in production. The Thunder Builders Group L.L.C. acquired the assets required to manufacture the Thunder Mustang through foreclosure on a loan. These assets were posted as for sale.

Panzl PAN

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Despite its superficial resemblance to a Pitts S-2, the Panzl Pan 1 N11ZL is an original 1987 homebuilt experimental biplane. It was a two-place cabin biplane, powered by a Franklin 6V-335.

The one built, N11ZL c/n ZL-1, won the EAA Champion Custom-Plans Built award at Oshkosh in 1990.

It was substantially damaged on March 18, 2003 during impact with terrain following a forced landing attempt near Vernal, Utah. The commercial pilot, who was the sole occupant on board, received minor injuries.

Pander Multipro

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Designed by Theo Slot, who was responsible for all of Pander & Sons original designs, the Multipro is variously described as a side-by-side two seat or three seat light aircraft. It had high and almost constant chord wings, braced on each side by a V-form pair of struts fixed to the lower fuselage longerons. The fuselage was a rounded, plywood skinned structure, contemporaries remarking, as they had with other Panders, at the quality of the finish.

It was powered by a Pobjoy R 7-cylinder radial engine; the two blade propeller was driven via spur gears that reduced its speed and placed the output shaft above the engine centre, an unusual arrangement for a radial. The cabin was under the wing with a deep starboard-side access door and multi-panel glazing. The fuselage tapered aft, with the tailplane set half way up it and its fin and rudder together were almost triangular apart from a rounded tip. The Multipro’s conventional undercarriage was fixed, with the mainwheeels on V-sruts attached to the lower longerons and stabilized laterally by an inverted V-strut jointed at the fuselage central underside.

The Multipro flew for the first time in September 1932.

In all three Multipros were built. The first (PH-AIU c/n 42) and third (PH-AIX c/n 44) were rapidly sold to private individuals; the second (PH-AIV c/n 43) remained registered to the Pander works until 1937, when it too was bought privately. All remained on the Dutch civil aircraft register until at least 1939. One, the second aircraft, is known to have been destroyed by German bombing during the invasion of the Netherlands on 10 May 1940.

Engine: 1 × Pobjoy R 7-cylinder, 63 kW (85 hp)
Wingspan: 11.30 m (37 ft 1 in)
Length: 7.80 m (25 ft 7 in)
Gross weight: 720 kg (1,587 lb)
Maximum speed: 175 km/h (109 mph; 94 kn)
Capacity: 2 or 3