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Mooney M20

The Mooney M20 is a family of piston-powered, four-seat, propeller-driven, general aviation aircraft, all featuring low wings and tricycle gear, manufactured by the Mooney International Corporation.

Development
Al Mooney had been developing preliminary designs for the four-seater M20 for some time, while the single-seat M-18 Mite was in production in the late 1940s and early 1950s. When in early 1953 the company moved from Wichita, Kansas, to Kerrville, Texas, and when it became clear that the Mite was nearing the end of its production, development of the M20 accelerated. The first M20 flight took place on September 3, 1953, and it was certified on August 24, 1955. During 1955, the company sold 10 of the M20 airplanes. Due to start-up costs, they lost about $3000 on each airplane. In 1956, they delivered 51 airplanes, and in 1957 the total was 105. The airplane gained attention because it was able to achieve speeds up to with a Lycoming O-320 engine. The combination of speed and efficiency was noteworthy. In 1958 the M20A joined the lineup with a larger Lycoming O-360-A1A engine, and by 1959, this was the only model offered, 231 units were sold that year. 1959 was also the first year that the company made a profit. The M20A continued production into 1960, when 166 were delivered. These were the last of the Mooneys to have wooden structures in the wings and tail. Early in the model's history, several incidents of wooden tails breaking up in flight occurred due to water damage and the resulting rot. Consequently, most tails have now been replaced with all-metal copies, as required by Mooney Service Bulletin M20-170A and the FAA Airworthiness Directive 86-19-10. Without the possibility of metal fatigue, the wooden wing has an indefinite life expectancy and is considered by some pilots to provide a smoother ride in turbulence. 1960s In January 1960, the Mooney company convinced Ralph Harmon to leave McDonnell Aircraft in St. Louis, Missouri, and take over management of the engineering efforts. He insisted on replacing the wood in the M20 with aluminum, and the all-metal M20B was completed by the end of 1960, less than a year after his arrival. In 1961, the company sold 222 M20B airplanes. The following year, the M20C was introduced and 336 were sold that year. Also known as the Mark 21 and later the Ranger, the M20C had several improvements over the M20B, including greater deflection on control surfaces, reduced cowl flap openings for better engine cooling, improved exhaust scavenging with a Hanlon and Wilson exhaust system, new battery access door, more powerful landing light, lightweight floor, an increased gross weight of , lighter empty weight, new instrument panel layout, and a higher maximum flap angle of 33 degrees. In 1964 the M20E Super 21 was introduced. It was also based on the M20C but with a more powerful Lycoming fuel-injected engine. The company sold 366 M20E units that year. In 1965, a new feature was introduced to the M20. It was called "positive control" and was a single-axis autopilot produced by Brittain Industries. It maintained the wings of the airplane in a level position unless a button on the control wheel was depressed for turns and banks. It was a controversial feature, liked by some pilots and disliked by others. Production and sales of the M20 continued to increase. In 1966, a total of 760 units were delivered, including 280 of the M20C Mark 21 planes and 473 of the M20E Super 21s. A new model, the M20F Executive 21, offered more legroom due to a increase in cabin length which also allowed for a third fuselage side window. The M20G Statesman, a version of the M20F with less-powerful engine, was released in 1968. It had a larger airframe than the M20C, but the same engine, and as a result was slower. It was not as successful as the M20F and was produced for only three years, from 1968 to 1970, with a total production run of 189 units. Despite strong sales, Mooney was short of cash. The company went into chapter 7 bankruptcy in early 1969, and was acquired by American Electronics Laboratories and then Butler Aviation International. Sales that year were less than half of the previous year's figures, although a new version of the M20E Chaparral was released with electrically operated flaps and landing gear. Butler Aviation also acquired the troubled Aerostar company and combined it with Mooney in an attempt to save both. The Mooney name was dropped in 1970, as was the M20 designation; the planes were called Aerostars. 1970s Butler Aviation closed the Mooney plant in early 1971, and it remained closed for more than two years. In October 1973, Mooney was purchased by Republic Steel. Robert Cumming, a general manager at Republic Steel, had owned a Mooney M20F Executive for years and flew it frequently, and wished to put the Mooney M20 back into production. This began in January 1974 with the reintroduction of the M20F Executive. Roy LoPresti, formerly of Grumman American, had been hired as the vice president of engineering. Through the efforts of his engineering group, various improvements were made to the M20 with the goal of increasing its speed, and the M20J was introduced in July 1976. It was also known as the Mooney 201 because it was capable of with its engine. The 201 was a big seller, and a turbocharged version was developed later that year. The next year, 1977, three models were offered: the M20C Ranger, the M20F Executive, and the M20J 201. By 1979, the M20C had been dropped, ending production of the short-body M20. The same year, 1979, the company's first turbocharged M20 was released: the M20K 231, so designated because its top speed was . It was based on the earlier 201 with further improvements. It had a wider wingspan and a six-cylinder Continental engine, and the fuel capacity was increased to . This year, a total of 439 airplanes were delivered—fewer than the top years of the 1960s, but these deliveries resulted in healthy profits. From this point through 1986, the M20J and the turbocharged M20K were the only two models offered. 1980s General aviation manufacturing experienced a significant downturn starting in 1982. Mooney was affected along with other manufacturers and was forced to downsize through temporary layoffs. Despite the recession, development work continued. The 201 and 231 received more improvements, including significant reductions in cabin noise levels. In 1982, deliveries fell to 218 units, and in 1983 only 154 aircraft were produced. The United States Air Force announced a competition to develop a replacement for the Cessna T-41 trainer, and Mooney immediately began to develop a military trainer based on the 231. While the company was dealing with the recession, Republic Steel was acquired by the Ling-Temco-Vought corporation and dropped Mooney. The company ended up in the hands of Armand Rivard of Lake Aircraft and Alexandre Couvelair, a Mooney dealer from Paris. Sales continued to fall, totaling 143 in 1984 and 99 in 1985. The next new model, the M20K 252, appeared in early 1986 with a top speed of . It replaced the 231 and achieved its higher speed with the same engine. It featured a new 28-volt electrical system to power additional equipment and to improve cold-weather starting. The Continental TSIO-360-GB engine in the 231 had required specific pilot training and modified takeoff and climb procedures to operate at acceptable engine temperatures in hot weather. Because of this, the 252 received an intercooled TSIO-360-MB engine. The various improvements were copied to the 201 airframe, and the new 205 model was released in 1987. The fuselage was stretched to form the first long-body M20. One new feature on this airplane was the replacement of the throttle, mixture and propeller controls with a single power control; mixture and propeller rotation speed were automatically adjusted based on the setting of this single control. The Mooney PFM did not last, a total of 41 units having been manufactured in 1988 and 1989. Most M20Ls no longer use this unique engine, as factory support ceased in 2005. In February 1989, the next M20 model was released: the M20M TLS (Turbocharged Lycoming Sabre). It was powered, as the name hinted, by a turbocharged Lycoming six-cylinder engine that produced at 2,575 rpm, and it had a three-bladed propeller. It was capable of cruising at and had a range of and a maximum climb rate of per minute. The first year, the TLS accounted for 30 of the 143 aircraft delivered, and in 1990, this increased to 61 units. Also in 1989, Mooney released a trainer model based on the M20J. Beech, Cessna, and Piper had all stopped production of trainers throughout the 1980s, and the 201AT was designed to fill this gap. From 1989 to 1992, 20 units were delivered. 1990s The next Mooney M20 model was the M20J 201, also designated the MSE, released in 1990 (although few were actually delivered prior to 1991). This was a non-turbocharged model that incorporated many features from the TLS. In early 1991, Mooney decided to offer its Enhanced Flight Screener Trainer model to the general public, given that the Air Force was slow to make a decision on its trainer. It was to have a Lycoming O-540 engine and would be rated for aerobatics. However, it generated little public interest. The TLS continued production through 1995, and the MSE continued, too, until it was replaced by the M20R Ovation in 1994. Once again, Mooney was offering two models: one offering high speed (the TLS) and the other offering high efficiency. 2006 The M20T Predator, a canopy-equipped version of the basic M20 design powered by a Lycoming AEIO-540 engine, was Mooney's entrant in the USAF Enhanced Flight Screener competition. The prototype, built in 1991, displayed in a tiger-stripe paint scheme. The sole prototype, registered N20XT, was flown in the Experimental – Market Survey category and was still owned by Mooney Aircraft in 2013, although its registration had expired November 30, 2013. The competition for the Enhanced Flight Screener program was finally held in 1992, and the Slingsby T67 Firefly was chosen instead of the Mooney EFS. Sales continued to drop, only reaching 64 units in 1993. The San Antonio location was sold and all operations returned to Kerrville. Development of the M20 continued, however, and the M20R Ovation was released in 1994. It was designed to fill a gap between the normally aspirated MSE and the turbocharged TLS, and it was powered by a Continental IO-550 engine. Of the 91 Mooney aircraft manufactured in 1995, 54 were Ovations. This model was named Flying's single-engine plane of the year in 1994. The M20S Eagle, released in 1999, was powered by a Continental IO-550-G. It was followed in 2001 by the Eagle 2. This model included refinements such as a standard leather interior. The Eagle 2 also used the same 3 blade propeller as the original versions of the M20R and was produced from 1994 to 1999. 2000s The M20TN Acclaim was released in 2006, powered by a turbonormalized Continental TSIO-550-G powerplant with twin turbochargers and dual intercoolers. The Acclaim replaced the Mooney M20M Bravo in the company product line. Mooney laid off 60 employees in June 2008 and cut production, citing a weak economy and sales inhibited by high fuel prices. Later that year, in November, all production was halted. 2010s More employees were laid off in late 2010. The stated goal was to have fewer than 10 employees at the start of 2011, who were to provide parts and support to existing aircraft owners while the company searched for new investment. Later that year, the M10T and the M10J were announced, both to be powered by Continental diesel engines. Two new models were released in 2016: the M20U Ovation Ultra and the M20V Acclaim Ultra. The M20U was based on the M20R, and its first flight was on June 4, 2016. It was the first M20 to have a pilot-side door. It also featured a composite shell forward fuselage which replaced the traditional aluminum skin. The M20V, which was developed from the M20TN Acclaim, had those features, as well. The company closed its doors and laid off all staff on November 12, 2019. The company reopened and staff returned to work on December 2, 2019. ==Design==
Design
With the exception of the earliest models which had wings and tails with wooden frames, M20s are constructed entirely of metal. All are low-wing aircraft, and the wing skin is aluminum. Slotted flaps cover 70% of the trailing edge. Earlier models use a hydraulic hand pump to extend the flaps, while later models have electrically operated flaps. The forward fuselage has a steel-tube cabin structure covered in aluminum skin; the aft portion of the fuselage is of semi-monocoque design. In many places on the skin of the airplane, flush-mounted rivets are used to reduce drag. The landing gear on the Mooney M20 are made of heat-treated chrome-molybdenum steel. The main landing gear is attached to the main wing spar, while the nose gear is mounted to the tubular steel frame. Stacks of rubber shock discs act as shock absorbers. All models, with the exception of the M20D Master, came with retractable landing gear; on these models, the nose wheel retracts rearwards and the main wheels retract inwards. Early models use a hand-operated lever system to raise and lower the gear. The manually actuated landing gear are raised by unlocking the lever, which is called a "Johnson Bar" (named after the Johnson Bar (locomotive)), from just below the throttle, rotating it to the floor, and locking it into a fixture on the floor. Lowering the landing gear require the same operations in opposite order. Al Mooney got his start working as young man for the railroad industry, hence the borrowing of a steam locomotive term for use in describing part of an aircraft. The Mooney M20 has medium aspect-ratio tapered wings with 1.5 degrees of washout and 5.5 degrees of dihedral. Later models were equipped with stall strips to improve the stall characteristics. All M20s store fuel in two separate "wet wing" tanks, which are located in the inboard sections of each wing. Fuel is driven from the tank to the injectors or carburetor by an engine-driven pump, backed up with an electric boost pump. ==Operational history==
Operational history
In August 2017, 6,748 Mooney M20 aircraft were registered with US Federal Aviation Administration, 342 with Transport Canada, and 33 in the United Kingdom with the Civil Aviation Authority. As of July 2018, 154 M20 aircraft were registered with Australia's CASA. In June and July, 2017, pilot Brian Lloyd flew his Mooney M20K 231 around the world, commemorating Amelia Earhart's attempted circumnavigation which took place 80 years earlier in 1937. Lloyd followed a route similar to the one taken by Earhart. ==Variants==
Variants
;M20 Mark 20 :Initial variant with mostly wooden construction and manually retracting landing gear. The 1953 prototype, registered N4199, was originally powered by a Continental C-145-2H engine. The prototype was later re-engined with a Lycoming O-320 engine driving a two-bladed Hartzell constant-speed propeller, which became standard on production aircraft. Despite the engine change, the cowling was not redesigned, leading to sub-optimal intake air pressure; a problem that would not be fixed for many years. During its four-year production run, the M20 received numerous improvements. Certified August 24, 1955. ;M20A Mark 20A :Introduced in 1958 with a Lycoming O-360-A1A engine, though also certified for the O-360-A1D. As with the M20, Airworthiness Directive 68-25-6 required that all M20As be fitted with a metal tail. Electrically retracting landing gear was introduced as an option in 1965, while a single-axis Brittian Industries autopilot marketed as "positive control" or "PC" was added as standard equipment. At some point during production, the rounded windows of the Mark 21 were redesigned to a more rectangular shape. :* M20C Ranger, replaced the Mark 21 in 1968 with a one-piece windshield, fixed cowl flaps and entrance step, and the dorsal fin removed. In 1969, a new power quadrant was added, and the formerly optional electrical flaps and landing gear were made standard. Mooney branding was dropped in 1971, and no Rangers were produced in 1972 and 1973. When Ranger production restarted in 1974, it reverted to the Mooney branding. 530 total built; 196 (1968), 97 (1969), 88 (1970), 37 (1974), 39 (1975), 33 (1976), 25 (1977), and 15 (1978). :* Aerostar 200 Ranger, rebranding of the M20C with an ornamental appendage on the tip of the vertical tail, a streamlined stinger tail cone, and an improved air distribution system. 9 built, all in 1971. Mooney offered a factory conversion to replace the fixed gear with retractable units, which a majority of M20Ds underwent. Unlike the M20C and M20E, the 1965 and 1966 M20D did not receive the "positive control" autopilot. Like the M20C, the M20E received the "positive control" autopilot system in 1965. Gross weight remained at . Certified September 4, 1963. :* Aerostar 201 Chaparral, rebranding of the M20E with an ornamental appendage on the tip of the vertical tail, a streamlined stinger tail cone, and a more efficient engine cooling system. ;M20F :* M20F Executive 21, stretched M20E introduced in 1967. Powered by the same Lycoming IO-360-A1A engine as the Super 21, the M20F's fuselage was lengthened by , the cabin was stretched by , and gross weight was increased to . The 1969 model introduced a one-piece windshield, a new power quadrant, and electrical flaps and landing gear as standard. :* Aerostar 220 Executive, rebranding of the M20F with an ornamental appendage on the tip of the vertical tail, a streamlined stinger tail cone, and a more efficient engine cooling system. 12 built, all in 1971. No Executives were built in 1972 and 1973. ;M20G Statesman :Stretched M20C introduced in 1968. Powered by the same Lycoming O-360-A1D engine as the Ranger, the M20G's fuselage was lengthened by , the cabin was stretched by and a third side window was added, and gross weight was decreased to . ;M20H :Engineering prototype ;M20J :* M20J 201, introduced in 1977 to replace the M20F. Powered by a Lycoming IO-360-A1B6D engine, the M20J introduced many changes to reduce drag. These changes included a streamlined engine cooling system, landing gear doors that cover the wheel wells, flush airframe access panels, a new exhaust stack, flaps with faired-in hinges and gap seals, and a more efficient McCauley propeller. In 1978, the engine was swapped for a similarly-powered Lycoming IO-360-A3B6D, and a power quadrant replaced the original push-pull engine controls. The 1981 model introduced the redesigned wingtips of the M20K to the M20J, as well as improved soundproofing. Soundproofing was further improved in 1982 with the addition of double-pane door windows as well as extra stiffeners and insulation in the cabin. The 1984 model introduced improved instrument and circuit breaker panels and a streamlined composite belly panel. Wing-mounted air brakes were made available as an option in 1985. In 1989, the interior was redesigned to improve comfort, a 28V electrical system and electrically-operated cowl flaps were added, and the windows were revised with rounded corners. Certified September 27, 1976. :* M20J 201LM, "Lean Machine" version introduced in 1985. As M20J 201 but with simplified equipment package. Production figures between 1985 and 1987 were grouped with the standard M20J 201, while 44 201LMs were built in 1988. :* M20J 201SE, "Special Edition" version introduced in 1985. As M20J 201 but with a luxury interior. Production figures were grouped with the standard M20J 201. In 1992, the aircraft was redesignated to M20J AT for its final year of production. Production figures for the final year were grouped with the M20J MSE. :* M20J 205, introduced in 1987. As M20J 201 but with airframe changes from the M20K 252 which increased its top speed by . Other changes included a 28V electrical system and revised windows with rounded corners. 57 built. :* M20J 205SE, "Special Edition" version introduced in 1988. As M20J 205 but with a luxury interior. 22 built. :* M20J MSE Limited, introduced in 1991. As M20J MSE but with packaged optional equipment. Produced from 1991 to 1993, but production figures were grouped with the standard MSE. :* M20J Allegro, renamed MSE for final year of production in 1998. 19 built. ;M20K :* M20K 231, introduced in 1979. The first production M20 variant to feature a six-cylinder engine, the M20K 231 is powered by a Continental TSIO-360-GB engine with a Rajay turbocharger and push-pull power controls. Fuel capacity was increased to , a dorsal fin air scoop was added to cool the cabin, and new curved wingtips were introduced. The 1981 model featured improved soundproofing, which was further improved in 1982 along with the addition of a new exhaust resonator and pressurized magnetos. In 1984, the engine was swapped for the Continental TSIO-360-LB1B, and the improvements from that year's M20J were added as well. The 1985 model also introduced the changes from its M20J counterpart. :* M20K 231SE, "Special Edition" version introduced in 1985. As M20K 231 but with a luxury interior. Production figures were grouped with the standard M20K 231. :* M20K 252TSE, replaced the 231 in 1986. Powered by a Continental TSIO-360-MB1 with a Garrett variable wastegate controller, the 252TSE also introduced curved side windows. :* M20K Encore, introduced in 1997 with a Continental TSIO-360-MB7B. Gross weight was increased, and the landing gear from the M20M and M20R was installed to compensate. Gross weight was increased to . :* M20M TLS Bravo, replaced the TLS halfway through 1996. As TLS but with a Lycoming TIO-540-AF1B engine. The 1996 model introduced an option for a TKS ice protection system, which could be retrofitted to older M20Rs. :* M20R Ovation 2, introduced in 2000. As Ovation but with a dual Garmin 430 panel, a KFC-225 autopilot, a leather interior, and a two-bladed McCauley propeller. The dual Garmin 430 panel was replaced with a similar Garmin 530/430 panel in 2001. 131 total built; 55 (2000), 12 (2001), 8 (2002), 28 (2003), and 28 (2004). ;M20TN :* M20TN Acclaim, circular engine cooling intakes and winglets. Certified March 28, 2017. ;M22 Mark 22 :Twin-engine development of the M20 with strengthened wings, an enlarged vertical stabilizer, and powered by two Lycoming O-360 engines. One prototype was built in 1958, but further development was abandoned after flight testing. Not to be confused with the unrelated Mooney M22 Mustang. ;Rocket 305 :In 1990, Rocket Engineering Corp. of Spokane, Washington, modified an M20K 231 model by replacing the standard turbocharged Continental TSIO-360 engine and two-blade propeller with a turbocharged Continental TSIO-520-NB and a McCauley three-blade propeller. This engine and propeller combination had previously been proven on the twin-engined Cessna 340 and Cessna 414. Marketed as the Rocket 305, this variant delivered a 228-knot speed and 1,600 feet/minute rate of climb. By September 2017, the Rocket conversion had been discontinued by Rocket Engineering. ==Aircraft on display==
Aircraft on display
as part of a memorial to Robin Miller The Mooney M20H engineering prototype is on display at Jandakot Airport in Jandakot, Western Australia. The aircraft is painted to represent the M20E used by Robin Miller, an Australian female pilot known as the "Sugar Bird Lady" for her work in distributing the polio vaccine across Australia. ==Specifications==
Specifications
These are the specifications for the 2016 M20 Acclaim Ultra. ==See also==
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