Engines – Power

Piel CP.90 Pinocchio

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The C.P. 90 Pinocchio is a single seat, low wing aircraft designed by Claude Piel. Construction materials are wood & fabric, and the landing gear is a fixed tailwheel configuration.

Engine: 65 hp
Span: 23.6 ft
Length: 19.7 ft
Height: 6.0 ft
Area: 104 sq ft
Empty Weight: 695 – 760 lbs
Gross Weight: 1015 – 1105 lbs
Fuel: 95 lbs
U/C Track: 5.25 ft
Dihedral: 5° 40′
Incidence: 3°
Max Speed: 130 mph
Cruise 75% 5,000 ft: 118 mph
Cruise 65% 5,000 ft: 110 mph
Range: 400 miles
T/O Distance: 580 ft
Landing Distance: 525 ft
Stall Speed: 45 mph
Approach Speed: 65 mph
Vne: 200 mph
Rate Of Climb: 785 fpm
Complete set of plans 2009: US$225

Engine: 90 hp
Span: 23.6 ft
Length: 19.7 ft
Height: 6.0 ft
Area: 104 sq ft
Empty Weight: 695 – 760 lbs
Gross Weight: 1015 – 1105 lbs
Fuel: 95 lbs
U/C Track: 5.25 ft
Dihedral: 5° 40′
Incidence: 3°
Max Speed: 150 mph
Cruise 75% 5,000 ft: 140 mph
Cruise 65% 5,000 ft: 130 mph
Range: 350 miles
T/O Distance: 580 ft
Landing Distance: 525 ft
Stall Speed: 45 mph
Approach Speed: 65 mph
Vne: 200 mph
Rate Of Climb: 1140 fpm
Complete set of plans 2009: US$225

Engine: 115 hp
Span: 23.6 ft
Length: 19.7 ft
Height: 6.0 ft
Area: 104 sq ft
Empty Weight: 695 – 760 lbs
Gross Weight: 1015 – 1105 lbs
Fuel: 95 lbs
U/C Track: 5.25 ft
Dihedral: 5° 40′
Incidence: 3°
Max Speed: 160 mph
Cruise 75% 5,000 ft: 152 mph
Cruise 65% 5,000 ft: 143 mph
Range: 380 miles
T/O Distance: 580 ft
Landing Distance: 525 ft
Stall Speed: 45 mph
Approach Speed: 65 mph
Vne: 200 mph
Rate Of Climb: 1220 fpm
Complete set of plans 2009: US$225

Piel CP.80 Zephyr / Cougar

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CP.80 Zephyr

The Sapphire is a single-seat racing airplane of all-wood construction designed by Claude Piel. The airplane is stressed for the load factors of +12 and 19 C’s at the maximum takeoff weight of 770 pounds. The Saphhire can accommodate any engine from 50 to 100 hp. Its wing is fully cantilevered and tapered for minimum drag and has a tip-to-tip laminated box spar to avoid heavy root fittings and wing alignment problems. The fuselage consists of three bulkheads and is entirely plywood covered. The cockpit is roomy enough to accommodate a large pilot. The landing gear is a fixed tailwheel configuration.

The Cougar is a single-place, high-speed aerobatic monoplane. It utilizes an all-wood design and a 90-hp engine.

In 1980 plans were available from E. Littner, Box 272, Saint Laurent, Quebec H4L 4V6, Canada.

Engine range: 65 to 100 hp
Span: 19.7 ft
Length: 17.3 ft
Height: 5.6 ft
Area: 66.7 sq ft
Empty Weight: 575 lbs
Fuel: 60 lbs
Max Speed: 200 mph
Cruise 75% 5,000 ft: 175 mph
Cruise 65% 5,000 ft: 155 mph
Stall Flaps Up: 60 mph
Approach Speed: 80 mph
Vne: 235 mph
Rate Of Climb: 2350 ft/min
T/O distance: 650 ft
Landing Distance: 650 ft
Range (65%): 280 miles
Complete set of plans 2009: US$225

Zephyr
Engine: Continental C-90, 90 hp
HP range: 65-90
Height: 5.6 ft
Length: 17.3 ft
Wing span: 19.7 ft
Wing area: 66.7 sq.ft
Weight empty: 515 lb
Gross: 840 lb
Fuel cap: 10 USG
Speed max: 200 mph
Cruise: 155 mph
Range: 280 sm
Stall: 50 mph
ROC: 2300 fpm
Take-off dist: 600 ft
Landing dist: 650 ft
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel

Littner Zephyr
Engine: Continental O-100, 100 hp
HP range: 65-100
Height: 5.6 ft
Length: 17.3 ft
Wing span: 19.7 ft
Wing area: 66.7 sq.ft
Speed max: 200 mph
Cruise: 155 mph
Range: 280 sm
Stall: 50 mph
Weight empty: 515 lb
Gross: 840 lb
Fuel cap: 10 USG
ROC: 2300 fpm
Take-off dist: 650 ft
Landing dist: 650 ft
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel

Cougar
Gross Wt. 770 lbs
Empty Wt. 525 lb
Fuel capacity 10 USG
Wingspan 23’8”
Length 20’l0”
Top speed 190 mph
Cruise 160 mph
Stall 67 mph
Climb rate 2300 fpm
Takeoff run 600 ft
Landing roll 600 ft
Range 300 sm

Piel CP.60 Diamant / CP.604 Diamant / CP.605 Diamant

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Diamant

The Diamant is a three- or four-seat version of the Emeraude. This low-wing, high-performance monoplane is powered by a 100-hp Continental engine, It is also available in a four-place model propelled by a 150 Lycoming designated the Super Diamant. Both were created by designer Claude Piel.

The C.P. 60 Super Diamant is a two plus two (2 + 2) seat, low wing aircraft. A rear bench can be added to accommodate an adult (max. 170 lb) or 2 children.

Super Diamant

CP.605 Diamant three/fourseat cabin monoplane (first flown 1964 in CP.604 prototype form) and is certificated for commercial production Construction materials are wood & fabric, and the landing gear can be built in fixed tailwheel or retractable trigear configurations.

Diamant
Engine: 100 hp
Span: 30.5 ft
Length: 21.8 ft
Height: 5.8 ft
Wing area:143.1 sq.ft
Empty Weight: 995 lb
Gross Weight: 1700 lb
Fuel: 130 lb
Undercarriage: Fixed Gear
Dihedral: 5° 40′
Incidence: 4° 10′
Ultimate Load at 1610 lb: +6.6 / -2.64 G
Ultimate Load at 1875 lb: +5.7 / -2.28 G
Max Speed: 134 mph
Cruise 75% 5,000 ft: 127 mph
Cruise 65% 5,000 ft: 122 mph
Range: 1200 miles
T/O distance: 850 ft
Stall Flaps Up: 56 mph
Stall Flaps Down: 51 mph
Approach Speed Flaps Down: 78 mph
Max Speed Flaps Down: 87 mph
Rate Of Climb: 500 fpm
Vne: 175 mph
Landing Distance: 720 ft
Complete set of plans 2009: US$350

Super Diamant
Engine: 150 hp
Span: 30.5 ft
Length: 21.8 ft
Height: 5.8 ft
Wing area:143.1 sq.ft
Empty Weight: 1120 lb
Gross Weight: 1875 lb
Fuel: 250 lb
Undercarriage: Fixed Gear
Dihedral: 5° 40′
Incidence: 4° 10′
Ultimate Load at 1610 lb: +6.6 / -2.64 G
Ultimate Load at 1875 lb: +5.7 / -2.28 G
Max Speed: 160 mph
Cruise 75% 5,000 ft: 154 mph
Cruise 65% 5,000 ft: 143 mph
Range: 1750 miles
T/O distance: 600 ft
Stall Flaps Up: 56 mph
Stall Flaps Down: 51 mph
Approach Speed Flaps Down: 80 mph
Max Speed Flaps Down: 87 mph
Rate Of Climb: 1000 fpm
Vne: 175 mph
Landing Distance: 800 ft
Complete set of plans 2009: US$350

Super Diamant
Engine: 160 hp
Span: 30.5 ft
Length: 21.8 ft
Height: 5.8 ft
Wing area:143.1 sq.ft
Empty Weight: 1150 lb
Gross Weight: 1875 lb
Fuel: 250 lb
Undercarriage: Retractable Tri Gear
Dihedral: 5° 40′
Incidence: 4° 10′
Ultimate Load at 1610 lb: +6.6 / -2.64 G
Ultimate Load at 1875 lb: +5.7 / -2.28 G
Max Speed: 170 mph
Cruise 75% 5,000 ft: 161 mph
Cruise 65% 5,000 ft: 149 mph
Range: 1850 miles
T/O distance: 600 ft
Stall Flaps Up: 56 mph
Stall Flaps Down: 51 mph
Approach Speed Flaps Down: 80 mph
Max Speed Flaps Down: 87 mph
Rate Of Climb: 1100 fpm
Vne: 175 mph
Landing Distance: 800 ft
Complete set of plans 2009: US$350

Pickering-Pearson K.P.2

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The Pickering-Pearson K.P.2 was designed by K.N.Pearson as a single-seat, mid wing monoplane. It was powered by a 40-horsepower Aeronca E.117 pusher engine. The KP.2 was a wooden monoplane with fixed landing gear.

It used no rudder, being equipped with Pearson rotary ailerons, one on each wingtip.

Built by G.L. Pickering at Hamworth in 1933.

It first flew in 1933 as G-ACMR c/n 2.

It was broken up in 1935.

Piasecki PA-97 Heli-Stat

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The Piasecki PA-97 Heli-Stat project began in the mid 1970s with a view to combining the lift capability of a lighter-than-air vehicle with the precise manoeuvrability of the helicopter, and following support from the US Forestry Service and the US Navy, construction of a prototype Heli-Stat began at Lakehurst, New Jersey, in 1979. The hybrid aircraft uses an airship-based envelope, attached via a skeletal structure to the front fuselage portions of four Sikorsky SH-34J helicopters, each powered by a standard Wright radial engine driving the conventional main rotor system and mounted at the four corners of the aircraft. The tail rotors are replaced by large diameter propellers to provide propulsion and full controllability.

At the beginning of 1984 it was expected that the Heli-Stat would fly in 1985, following a redesign of the structure which had failed under load tests. The following data is provisional

Richard Burke, 29.07.2008
I spent 7 years on this project starting first at the MAIN engineering facility drafting this monster along with 15 other people on Island Avenue in Philadelphia and later moved to Lakehurast during the structural pluck tests. I was there up until the ground manuvering tests where being performed. If you have any questions I can answer them I was over every single part of the airframe / Sh34J’s (Modified) and the aerostat (ZPG2 envelope). [The photo] was a roll out for a photo op dog and pony show note the lack of inverted v fins on the aerostat and the lack of pusher props on the helos also US Forrest Service was not painetd on the envelope yet . I am actually in this photo aft center stern of ship next to the guy with the bike, Joe O’Halleren
It was truly a combination of four SH-34 helicopters and a ZP-3 patrol blimp. It had B-52 landing gear and P-51 reduction gear boxes driving H-3 tail rotors as pusher props.

Piasecki Heli-Stat
Engines: 4 x Wright R-1820-84A, 1525shp
Overall width: 60.05m
Overall length: 74.07m
Empty weight: 24895kg
Gross weight: 50469kg
Maximum speed: 132km/h
Service ceiling: 3810m
Range: 3307km
Range with maximum payload: 80km