Piel

Piel Aviation Sa
Avions Claude Piel

Claude Piel produced a series of light aircraft from the early 1950s, most famous of which was the Emeraude two-seater with, in its original CP.30 form, a 65 hp Continental engine. Hundreds of Emeraudes of varying types were built under license by companies in a number of countries. This company (instead of original Piel Aviation SA) continues to market Piel aircraft in plans form, including single-seat CP.80 Zef racing monoplane, CP.90 Pinocchio single-seat monoplane (single-seat variant of Emeraude), CP.328 Super Emeraude (also has been commercially built), CP.402 Donald single-seat high-wing cabin monoplane (first flown 1953), CP.605 Diamant three/four-seat cabin monoplane (first flown 1964 in CP.604 prototype form) and is certificated for commercial production, CP.751 Beryl tandem two-seat monoplane, and CP.1320 Saphir three-seat monoplane.
An aeronautical engineer, he designed a complete family of aircraft. Claude Piel died in August 1982.

1983: Madame Vetive Piel, 104 cote de Beulle, chemin des Alouettes, 78580 Maule, France.

Phoenix Industries Model CV

Manufactured in the US, kit prices (US$7590) includes the engine and prop. The wing was available in two sizes, and nose wheel steerable.

Engine: Zenoah G25, 22 hp
Height: 5 ft
Length: 6 ft
Wing span: 30 ft
Wing area: 315 sq.ft
Empty weight: 120 lb
Gross weight: 360 lb
Fuel capacity: 2.5 USG
Cruise: 20 mph
Range: 30 sm
Rate of climb: 350 fpm
Takeoff dist: 150 ft
Landing dist: 0-10 ft
Service ceiling: 5000 ft
Seats: 1

Phoenix Air Phoenix Motorglider

Phoenix Air’s honcho Jim Lee counts 14 more aircraft on his backordered list—a major LSA success story. The 49-foot span, Rotax 912ULS-powered low-wing taildragger won Sun ‘n Fun’s Best Commercial LSA award in 2012 and received three more sales. Base price 2012: $149,000.
Phoenix Air was rolling out a new Phoenix S-LSA motorglider every 18 days. They registered 10 aircraft in the US in 2012.

Under development in 2012 was the all-electric ePhoenix, using an in-house built motor and electronic flight controller. So far, flights have yielded one-hour durations, this is a two-seat LSA.

Phase 3 Eclipse

Single seat single engined high wing mono¬plane with conventional three axis control. Wing has elliptical planform and tapering chord; inverted V tail. Pitch/yaw control by elevon; roll control by wing warping; control inputs through stick for pitch/roll and pedals for yaw. Cantilever wing; wing profile; double surface. Undercarriage has three wheels in tricycle formation; suspension on all wheels. Push right go right nosewheel steering connected to yaw control. No brakes. Aluminium tube framework, without pod. Engine mounted below wing driving pusher propeller.

Conceived by J Bruce Emmons, the Eclipse was one of the new releases at Sun ‘n’ Fun of March 1983 at Lakeland, Florida. The Eclipse is also the first rigid wing ultralight to use wing warping for roll control (with the possible exception of the British Ladybird, which is not yet in production). With the Eclipse, the accent has been put on flight stability. The strength of the airframe has not been neglected, this ultralight having been static tested to as much as ± 9 g, more than the requirements for a light aircraft to be classed in the aerobatic category. The wings can be placed parallel with the framework by removing three bolts; demounted like that the machine can be transported either on a trailer or a roof rack. All the pieces in the kit are delivered pre formed, cut and drilled. Sold for $5495 in 1983, the kit thus provided is claimed to need only 30 h for completion.

Engine: KFM 107, 25 hp at 6000 rpm
Propeller diameter and pitch 54×23 inch, 1.37×0.58m
V belt reduction, ratio 2.0/1
Max static thrust 175 lb, 79 kg
Power per unit area 0.22 hp/sq.ft, 2.4hp/sq.m
Fuel capacity 5.0 US gal, 4.2 Imp gal, 18.9 litre
Length overall 14.0 ft, 4.27 m
Height overall 5.0ft, 1.52m
Wing span 32.2ft, 9.80m
Chord at root 4.0 ft, 1.22 m
Dihedral 0 deg
Tailplane span 8.0 ft, 2.44 m
Total wing area 114 sq.ft, 10.6 sq.m
Wing aspect ratio 9.1/1
Wheel track 4.0 ft, 1.22 m
Wheelbase 6.0 ft, 1.83 m
Nose¬wheel diameter overall 11 inch, 27 cm
Main wheels diameter overall 11 inch, 27 cm
Empty weight 165 lb, 75kg
Max take off weight 465 lb, 211kg
Payload 300 lb, 136kg
Max wing loading 4.071b/sq.ft, 19.9kg/sq.m
Max power loading 18.6 lb/hp, 8.4kg/hp
Load factors +6.0, 6.0 design; +9.0, 9.0 ulti¬mate
Max level speed 63 mph, 103kph
Max cruising speed 55 mph. 88kph
Economic cruising speed 50mph. 80kph
Stalling speed 25mph, 40kph
Best glide ratio with power off 15/1 at 35mph. 56kph
Range at average cruising speed 150 mile, 241 km