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

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

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.

Piaggio PD-808

Under an agreement signed in 1961, Piaggio and Douglas Aircraft developed the PD-808 for military and commercial use. Originally designed by the Douglas Aircraft Company of Long Beach, California, as a business jet. No orders were received, and the complete project was bought by Piaggio, which flew the first prototype in 29 August 1965.

Piaggio PD-808 Article

The PD-808 was powered by Bristol Siddeley Viper turbojets mounted on the sides of the rear fuselage. Piaggio also failed to secure any worthwhile commercial interest, but a few examples were taken by the Italian air force.

After appearing at the Paris Air Show it was modified.

Only 27 examples of this type, with low-set wings and aft-mounted turbojet engines, were produced, and 25 of these went to the Italian air force. The first aircraft were configured for the utility role (navaid calibration, navigation training for three pupils, and light transport of up to eight passengers or an equivalent freight load), but the last six aircraft were completed as electronic warfare platforms with cabin accommodation for specialist Elint (electronic intelligence) equipment and its three operators.

Power increased in 1966 to 3,300 lbs. s.t. The PD-808 differed from the original model by having larger tip tanks, a longer dorsal fin, and a forward-sliding nose fairing. By 1972, the aircraft was available in several versions: a five-seat executive version, a seven-seat executive transport, a six-seat version for the Italian Air Force, and one powered by 3,500-lb. s.t. AiResearch turbofans. Other PD-808s are powered by twin 3,360-lb. s.t. turbojets drawing from two integrated tanks of 511 gallons total capacity and wingtip tanks with 473 gallons total capacity.

Four versions were produced for the Italian Air Force as the PD-808 VIP six-seater for government and military VIP transport duties; PD-808 TA nine-seat transport and navigation trainer; PD-808 ECM electronic-countermeasures version; and the PD-808 RM radio-calibration version that is equipped for medium- and high-altitude calibration of navigation aids.

Engines: two Rolls-Royce Bristol Viper Mk 526 turbojets, 3,368-lb. s.t / 1524kg
Wingspan: 13.2 m / 43 ft 4 in
Length: 12.85 m / 42 ft 2 in
Height: 4.8 m / 16 ft 9 in
Wing area: 20.9 sq.m / 224.97 sq ft
Max take-off weight: 8165 kg / 18001 lb
Empty weight: 4830 kg / 10648 lb
Max. speed: 850 km/h / 528 mph
Cruise 497 mph
Stall 104 mph
Service ceiling: 13700 m / 44950 ft
Range w/max.fuel: 2100 km / 1305 miles
Initial climb rate: 5,400 fpm
Takeoff distance (35′): 3,180 ft
Landing distance (50′): 2,990 ft
Seats: 5-9

PD-808ECM
Five-seat electronic warfare plane
Engines: two 3,360-lb (1,524-kg) thrust Piaggio built Rolls-Royce (Bristol Siddeley) Viper Mk 526 turbojets
Maximum speed 529 mph (851 kph) at 19,685 ft (6,000 m)
Initial climb rate 5,415 ft (1,650 m) per minute
Service ceiling 44,950 ft (13,700 m)
Range 1,322 miles (2,128 km)
Empty weight 10,648 lb (4,830 kg)
Maximum take-off weight 18,001 lb (8,165 kg)
Wing span 43 ft 3.75 in (13.20 m)
Length 42 ft 2in (12.85 m)
Height l5ft 9in (4.80m)
Wing area 224.97 sq ft (20.90 sq.m)
Armament: none

Piaggio P.180 Avanti

At the 1983 NBAA convention in Dallas, Texas, Piaggio announced a new twin turbo-powered business aircraft. Design work on the P.180 Avanti had begun at Piaggio’s Genoa headquarters in 1979. Seating six to 10 passengers it was a radical departure from anything the company had previously produced. The major design feature of the aircraft is its use of three lifting surfaces. The main wing is fitted above the mid-set position in the fuselage, with the main spar running behind the passenger cabin. Its straight leading edge is broken only by the engine nacelle inlets and the wing has a slight dihedral of 2 degrees. The T-tail and elevator act as the second lifting surface, in addition to being orthodox control surfaces. The foreplane is not a simple canard, but provides a positive lift component in addition to that produced by the wing. This in turn allows the wing to be reduced in size, thus decreasing overall weight and drag.

Piaggio P.180 Avanti Article

Piaggio P.180 Avanti 2 HB-LUS

The engines were originally specified as Pratt & Whitney Canada PT6A-66A turboprops, but these were later changed in favour of more powerful PT6A-61s. Each drives a five-bladed Hartzell fully-feathering reversible-pitch propeller with spinner. The engines are mounted in composite-material nacelles. The Avanti makes considerable use of composites. Carbonfibre and a Graphite/ Epoxy mix represent about 10% of the aircraft’s weight, and all of these components are built by Sikorsky arid Edo. Wings and tail sections are produced by Piaggio at Genoa, while the forward fuselage is the responsibility of Piaggio Aviation in Wichita. Final assembly is completed in Italy. Aircraft intended for the American market are flown ‘green’ to the US to a specialist outfitters and there are plans to eventually assemble all aircraft in the United States.
The cockpit is fitted with a Collins EFIS system, comprising three CRTs and Col-lins navigation and weather radar systems are standard. The aircraft is certified for single pilot operations. The main cabin is pressurised and air conditioned, is fitted with a galley and folda-way tables. An emergency exit is situated at the front on the starboard side with the airstairs on the port side.

In 1983 Gates Learjet became a partner in the project, but withdrew for economic reasons in January 1986. All the tooling and the forward fuselages of the three pre-production Avantis which were on the line at Wichita, were then transferred to Italy.

Assembly of the first P.180 began on Piaggio’s Finale Ligne plant in 1986 and the first flight was made on 23 September 1986 (I-PJAV). This was followed by the second aircraft (I-PJAR) on 14 May 1987. The Avanti was certified by the Italian authorities in March 1990, and in May of that year the first production aircraft was rolled out. The final hurdle of US certification was passed in October 1990 and the first customer delivery took place the following September.

By early 1993 only 20 Avantis had been delivered.

Gallery

Engines: two Pratt & Whitney PT6A-66, 850-shp / 1107kW
TBO: 3000 hrs
Props: 5 blade 85in counter-rotating Hartzell
Wingspan: 14.03 m / 46 ft 0 in
Wing area: 172.2 sq.ft / 16.0 sqm
Length: 14.41 m / 47 ft 3 in
Height: 3.94 m / 13 ft 11 in
Max ramp weight: 5262 kg
Max take-off weight: 5080 kg / 11200 lb
Empty weight: 3384 kg / 7460 lb
Max ldg wt: 4965 kg
Max zero fuel: 4310 kg
Max fuel: 1170 kg
Max wing loading: 67.1 lbs/sq.ft
Max pwr loading: 6.79 lbs/hp
Service ceiling: 12500 m / 41000 ft
Vmo: 260 kt
Mmo: .67 Mach
Max speed: 395 kts
Stall (MLW): 93 kt
ROC: 2950 fpm
SE ROC: 2950 fpm
TO dist (50 ft): 2850 ft
Ldg dist (50 ft): 2860 ft
Max range with res: 1400 nm
Seats: 7-11
Cabin ht: 5 ft 9 in
Cabin width: 6 ft 1 in
Cabin length: 14 ft 7 in

Piaggio Aero P.180 Avanti II
Price: $6.8 million 2009
Engine: 2 Pratt & Whitney PT6A-66B: 850 shp (derated from 1630)
Max Takeoff Weight: 12,050 lb
Useful Load: 4300 lb
Max Payload: 2000 lb
Empty Weight, Std: 7800 lb
Wing Span: 46.03 ft
Cabin Height: 5.74 ft
Cabin Width: 6.07 ft
Cabin Length: 14.93 ft
Rate Of Climb: 2950 fpm
Max Certified Altitude: 41,000 ft
Max IFR Range: 1507 nm
Max Cruise Speed: 402 KTAS
Takeoff Distance: 2850 ft
Landing Distance: 2860 ft

Piaggio P.166 / Kearney and Treck­er Royal Gull

Piaggio P.166

The P.166 first flew on 28 November 1957. Introduced in 1959 for executive use, the P.166 had a rear baggage compart with a capacity of 300 lb.

Piaggio P.166 Article

Thirty-two examples of the P.166 twin-engined light transport were produced together with 51 P.166M general-purpose military counterparts (for the Italian Air Force); five P.166B Portofinos; two P.166Cs; 20 P.166S radar-equipped search, surveillance and coastal-patrol aircraft (for the South African Air Force as the Albatross).

P166B ZK-DAI

Production of the Piaggio P.166 in its several piston-engined variants ended in 1973.

Piaggio P.166 Air Test

The last version was the ten-seat P.166-DL3. A first flight was recorded by the Piaggio P.166 DL3 prototype (I-PJAG) on 3 July 1976. It differed from earlier versions by introducing 438kW Avco Lycoming LTP 101-600 turboprop engines, but these were still mounted in pusher configuration, and was produced for service in the transport role with the Somali Air Force. Four P.166DL-3SFMs were delivered to the Italian Ministry of Merchant Marine to serve as maritime and ecological research aircraft, carrying radar in a 360-deg scan installation under the nose, plus other sensors. The 1987 production version of the P.166, the DL3 can be configured for light tactical transport, medevac, multi engine training, armed counterinsurgency with four underwing pylons, SAR, and maritime reconnaissance with an integrated search/detection / identification / plotting / reporting system.

Kearney and Trecker Royal Gull

The Royal Gull, a twin engine pusher amphib (nee Piaggio P.166) was assembled and distributed by Kearney and Trecker during the late 1950s and early 1960s. Two models offered a choice of a 270 hp or a supercharged 340 hp Lycoming.

Gallery

Brian Heath
28 Jul 13
Kearney & Trecker Milling Machine Company was — probably still is — located in Milwaukee, Wisconsin. In the 1950’s and 60’s they leased 2 hangers on the west side of General Billy Mitchell Field in Milwaukee next to the Air National Guard with it’s F-86’s. The north hanger housed the business aviation division of the milling machine company. They had a DC-3, a Cessna 182, a Piaggio Royal Gull, and an aero-coupe. Hope I got the names right.

I was 10 years old in 1958 and my dad was the mechanic for the operation, co-pilot on the DC-3, and pilot on the others. They flew milling machine sales people and maintenance people around the eastern U.S. And they often flew the company owners and brass on vacations and fishing trips.

The south hanger housed Kearney & Trecker’s other business investment — a contract with Piaggio in Italy to assemble and sell Royal Gulls. Later the P-166 executive plane was added. My recollection is that the first P-166 at Mitchell Field was a prototype. It was the only one I ever saw, but I did ride in it several times. While the two businesses were legally separate, the mechanics/pilots often consulted with each other.

I recall being there one day when a lively discussion was held between 4 or 5 people about the length of the main forward hull that floats. Mid ship there was a step, and the rear part of the fuselage was not in the water. Some of them, including dad, thought the plane would take off and land better if the floating part of the hull extended back a foot or so. Not everyone agreed, but there was a consensus to try the idea by building a block (out of wood, I think) that would extend the floating hull back. They did that and tried it out. It worked and I think that Piaggio accepted the idea and modified the design.

I went to the airport with dad when there was a vague hope of getting a plane ride. Perhaps he was going to do a short test flight after doing some work. Or perhaps he was flying a low level company person that he knew would not mind a kid on the trip. Sometimes he had to deliver a milling machine part to a customer in, say, New York. On some of those trips I got the right hand seat — several times on the Gull.

I believe it was in the early 60’s that Kearney & Trecker sold a dozen or so of the Royal Gulls to Peru’s air force. They were looking for pilots to deliver the planes and for someone to teach Peru’s pilots and mechanics how to fly and maintain them. Dad volunteered and was selected to fly one plane from Milwaukee to Peru, and then spend a month or so teaching before returning. No, I was not invited. But I thought that what he did was cool. They bought the supercharged engines for going over mountain passes and landing on mountain lakes at over 12,000 feet. Neat planes. Sounds like Kearney & Trecker got out of the airplane business shortly after dad left.

P.166-DL3
Engines: 2 x Lycoming LTP 101-600, 600 shp / 447kW.
Props: Hartzell 3-blade, 95-in.
Seats: 6/12
Length: 39 ft 4 in
Height: 16 ft 5 in / 5 m
Wingspan: 48 ft 2 in / 14.69 m
Wing area: 285.9 sq.ft / 26.56 sq.m
Wing aspect ratio: 7.3
Maximum ramp weight: 9480 lb
Maximum takeoff weight: 9480 lb
Standard empty weight: 4960 lb
Maximum useful load: 4520 lb
Zero-fuel weight: 8377 lb
Maximum landing weight: 8377 lb
Wing loading: 33.2 lbs/sq.ft
Power loading: 7.9 lbs/hp
Maximum usable fuel: 1698 lb
Best rate of climb: 2100 fpm
Certificated ceiling: 20,000 ft
Maximum single-engine rate of climb: 650 fpm @ 95 kt
Single-engine climb gradient: 411 ft/nm
Single-engine ceiling: 12,500 ft
Maximum speed: 225 kt
Normal cruise @ 10,000ft: 212 kt
Fuel flow @ normal cruise: 530 pph
Endurance at normal cruise: 2.7 hr
Stalling speed clean: 79 kt
Stalling speed gear/flaps down: 66 kt
Turbulent-air penetration speed: 157 kt

Piaggio P.166

Piaggio P.150

Built to compete against the Fiat G.49 and Macchi M.B.323 as a replacement for the North American T-6 used widely by the Aeronautics Militare Italians, the Piaggio P.150 made its first flight in November 1952. An all-metal cantilever low-wing monoplane with square cut wingtips and tailplane, the P.150 had wide-track inward-retracting main landing gear legs. Pupil and instructor were housed in tandem with dual controls, under a long glazed canopy. The original powerplant was a 447kW Pratt & Whitney Wasp R-1340-S3H1 radial engine, which gave a maximum speed of 380km/h. A later version was fitted with a geared Alvis Leonides engine, but the type was not considered suitable to be built in quantity for the Italian air arm.

Engine: 1 x Pratt & Whitney Wasp R-1340-S3H1, 447kW / 600 hp
Wingspan: 42 ft 4.5 in
Length: 30 ft 4 in
Height: 9 ft 2.5 in
Empty weight: 4277 lb
Loaded weight: 5600 lb
Max. speed: 380 km/h / 236 mph at 5000 ft
Cruise: 195 mph
ROC: 1663 fpm
Service ceiling: 25,200 ft
Range: 880 mi

Piaggio P.149

The Piaggio P.149 was a 4-seat touring development of the P.148 with many of the same structural components. A 2-seat side-by-side all metal trainer with a fixed tailwheel undercarriage.

Piaggio P.149 Article

The prototype of the P.149 (I-PIAM c/n 171) with a 260 hp Avco Lycoming GO-435-C2 engine and a retractable tri-gear flew first on 19 June 1953. Two years later the P.149 was selected by the Federal German Air Force as a standard basic training and liaison monoplane.

To meet their requirements a 2-seat military trainer version of the P.149 with glazed cabin roof, deeper rear fuselage and a 280 hp Lycoming GO-480 engine was developed, designated P.149-D. The Federal German Air Force (Luftwaffe der Bundesrepublik Deutschland) ordered 265 Piaggio P.149D for use as a 2-seat primary trainer and 5-seat liaison aircraft.

92+13 Piaggio P-149 D 309

Piaggio built 76, including one which was written off before delivery. Focke-Wulf built 190 under licence from Piaggio. The first Piaggio built P.149D (AS+401 c/n 250) was delivered to Memmingen Air Base in May 1957. In the mean time Focke-Wulf had started production in Bremen, Germany and delivered its first example in November 1957.

Accommodation was provided for five, reduced to two for aerobatic flying.

P.149D
Engine: 1 x Avco Lycoming GO-480, 201kW / 270hp
Prop: 3 blade constant speed
Wingspan: 11.12 m / 37 ft 6 in
Length: 8.8 m / 29 ft 10 in
Height: 2.9 m / 10 ft 6 in
Wing area: 18.85 sq.m / 202.90 sq ft
Empty weight: 1160 kg / 2557 lb
Max take-off weight: 1680 kg / 3704 lb
Max. speed: 305 km/h / 190 mph
Cruise: 165 mph
Ceiling: 6050 m / 19850 ft
Range: 1090 km / 677 miles