| M22 Mustang | |
|---|---|
 | |
| The second Mooney M22 Mustang displayed at the Paris Air Show in June 1967 after flying nonstop from New York in 13 hours 10 minutes | |
| Role | Light aircraft |
| National origin | United States of America |
| Manufacturer | Mooney Aircraft Company |
| First flight | September 24, 1964 |
| Produced | 1965-1970 |
| Number built | 36 |
| Developed from | Mooney M20 |
The Mooney M22 Mustang is the first attempt at a pressurized single engine aircraft by the Mooney Aircraft Company of the United States.
The Mustang was developed to be a top-of-the-line model to supplement Mooney's successful Mooney M20 high-performance light aircraft. It is a five-seat pressurized single-engined aircraft with a wider and longer fuselage than the M20E Super 21 and a taller fin and leading edge fillet. [1] It is a low-winged monoplane with a retractable nosewheel undercarriage, with a similar wing to that used on Mooney's earlier M20 Ranger.
The first prototype flew on September 24, 1964, with the type being certified on September 26, 1966. [2] First deliveries commenced in 1965, continuing until 1970. 36 aircraft were completed before the line was closed. [3] It was produced and sold at a loss, which contributed to the bankruptcy of Mooney. [4]
The "Mark 22" name had previously been applied to a 1957 Mooney M20 experimental aircraft built with twin engines, a nose cone, and an enlarged tail surface. That aircraft did not go into production. [5]
The Model 22, although produced in fairly small numbers, has been operated by private and commercial owners in several countries including the United States and Australia. Its Garrett AiResearch cabin pressurization system gives the equivalent of 11,000 feet (3,400 m) at the aircraft's operational ceiling of 24,000 feet (7,300 m). [6] As a demonstration of its high performance, the second production aircraft was flown non-stop from New York to the Paris Air Show in June 1967, the flight taking 13 hours 10 minutes. The achievement is recorded on the display board in the accompanying photograph. The aircraft had been fitted with an extra fuel tank for the flight. In 2001, 24 aircraft remained in service. [7]
Data from Jane's All The World's Aircraft 1969-70 [8]
General characteristics
Performance
The Beechcraft 60 Duke is an American-built twin-engine fixed-wing aircraft designed and produced by Beechcraft. The aircraft has retractable tricycle landing gear and a pressurized cabin. The two piston engines are turbocharged and the turbochargers also pressurize the cabin with bleed air.
The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor.
The Aeronca Model 9 Arrow was a low-wing all-metal cabin monoplane with retractable landing gear. It was marketed to returning pilots from World War II and unveiled in 1947 but never went into production.
The Agusta AZ.8L, or Agusta-Zappata AZ.8L, was an Italian airliner prototype first flown on 9 June 1958. It was of conventional low-wing monoplane configuration with tricycle undercarriage and all-metal construction. Filippo Zappata's design grew out of a twin-engined transport designated AZ.1 that was never built.
The Air Tractor AT-300 is a family of agricultural aircraft that first flew in the United States on September 1973. Type certification was awarded to Air Tractor in November the same year, and serial production commenced in 1976. Of low-wing monoplane taildragger configuration, they carry a chemical hopper between the engine firewall and the cockpit.
The Cessna Model 411 is an American twin-engined, propeller-driven light aircraft built by Cessna Aircraft. It was that company's largest business aircraft to enter production when it first flew in 1962.
The Anahuac Tauro is a Mexican agricultural aircraft built in small numbers in the late 1960s and 1970s. The first prototype flew on 3 December 1968, with Mexican Type certification following on 8 August 1969. It was a low-wing braced monoplane of conventional configuration with fixed tailwheel undercarriage. The wing was of constant chord and had spray bars installed along its trailing edge.
The Auster Avis was a four-seat light aircraft developed from the Auster Autocrat. It featured a redesigned fuselage incorporating four doors and a circular cross-section towards the tail, new undercarriage, and new wing flaps. It was planned in two versions, the Mk 1 for civil use, and the Mk 2 for military and air ambulance duties. However, only two prototypes were built, and Auster abandoned the project in favour of the Auster J-5 Autocar.
The Aviamilano P.19 Scricciolo was a light civil trainer aircraft built in Italy in the 1960s.
The CAB GY-30 Supercab was a two-seat light aircraft built in France in 1954, as a further development of the CAB Minicab. The design was performed by Yves Gardan, a onetime employee of French aeronautical company SIPA. Changes incorporated in the Supercab included a more powerful engine, greater wingspan, manually retractable undercarriage, and slotted flaps that replaced the split flaps of the Minicab.
The Boisavia B.260 Anjou was a four-seat twin-engine light aircraft developed in France in the 1950s. It was a low-wing cantilever monoplane of conventional configuration with retractable tricycle undercarriage. Intended by Boisavia as a touring aircraft, it did not find a market and only the single prototype was constructed. At this point, the firm sold the design to SIPA, which modified the design and re-engined it with Lycoming O-360 engines, but found that they could not sell it either. At a time when the twin-engine light plane market was already dominated by all-metal American aircraft, the Anjou's fabric-over-tube construction was something of an anachronism, and all development was soon ceased. Plans to develop a stretched version with three extra seats and Potez 4D engines were also abandoned.
The Brditschka HB-3, HB-21 and HB-23 are a family of motor gliders of unorthodox configuration developed in Austria in the early 1970s.
The Funk F-23 was an agricultural aircraft produced in the United States during the 1960s. It was designed by Donald Funk using the fuselage frame of military surplus Fairchild PT-23 trainers as a starting point. The resulting aircraft was a low-wing cantilever monoplane with fixed, tailwheel undercarriage and all-metal construction. The main structural changes were in the wing, which had all-new outer panels. The space occupied by the forward cockpit of the PT-23 was used to accommodate a 200 U.S. gallon hopper for chemicals. Production continued until 1970, when manufacturing rights to the design were purchased by Cosmic Aircraft. The new owner, however, produced no further examples of the type.
The DINFIA IA 46 Ranquel, IA 46 Super Ranquel, and IA 51 Tehuelche were Argentine utility aircraft developed in the late 1950s.
The Vulcanair SF.600 Canguro was a feederliner developed in Italy in the late 1970s. Despite a number of attempts to put the aircraft into series production, only a small number were ever built. The Canguro was a high-wing cantilever monoplane of conventional configuration with a fuselage of rectangular cross-section and a high-set tail. The tricycle undercarriage was not retractable, and its main units were carried on sponsons on the fuselage sides. SIAI Marchetti provided funding towards the construction of the prototype, and constructed this aircraft at the former Aviamilano plant. After flight testing proved positive, the type was put on sale, but failed to attract buyers in any number, even when the original piston engines were exchanged for turboprops and retractable undercarriage was offered as an option.
The IAR-827 was an agricultural aircraft built in Romania in the 1970s and 1980s. The penultimate member of the family of designs that began with the IAR-821, it was, like the others, a conventional low-wing monoplane with fixed, tailwheel undercarriage, and shared the all-metal construction of the IAR-826. The prototype flew in 1976, powered by a Lycoming IO-720 engine, but the production examples that followed all had the PZL-3S.
The SAI KZ IV was a light twin-engined aircraft first built in Denmark in 1944 for use as an air ambulance.
The GY-80 Horizon is a French four-seat touring monoplane of the 1960s designed by Yves Gardan and built under licence, first by Sud Aviation, and later by that company's SOCATA subsidiary.
The Varga 2150 Kachina is an American all-metal, low-wing, fixed-gear, two-seat light aircraft fitted with a tricycle undercarriage.
The Aviamilano F.14 Nibbio is a four-seat, single engine cabin monoplane built in Italy in the late 1950s. Only ten production aircraft were completed.