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IN CELEBRATION OF OUR 20TH YEAR SPECIALIZING IN MOONEY AIRCRAFT; Get your BRAND NEW PRE-PUBLISHED BOOK AVAILABLE FOR YOU NOW! "THOSE MOONEY AIRPLANES" by Richard Zephro; studying the Mooney since 1974; 38 year private pilot/owner of Mooneyland and author of the articles within this website. FLYING IS NOT CHEAP! Within this book we will discuss not only how to save money while owning your own airplane, we will discuss ways to save big bucks on purchase, ownership, maintenance, appearance (lipstick), and upgrades. Further; we will discuss matters of safely operating your prized BIRD, why Mooney is the safest (by far) in its class, and aid in the pure FUN of owning your own airplane. BOOK INCLUDES 25 CHAPTERS OF INFORMATION FOR MOONEY ENTHUSIASTS, OWNERS, AND ASPIRING OWNERS OF MOONEY AIRCRAFT IN PARTICULAR, APPLICABLE TO ALL AIRCRAFT OWNERS IN GENERAL AND INCLUDES 100 HOUR/ANNUAL INSPECTION GUIDE AND ALL ABOUT MOONEY AIRCRAFT; HOW TO KEEP THEM SAFELY FLYING (ON THE CHEAP) DO IT YOURSELF STUFF, WHAT TO WATCH FOR, AND INCLUDES 124 FULL SIZE PAGES OF INFORMATION AND PHOTOS. (Includes some reprints and references from Mooneyland and tons of NEW information at your fingertips)            2 NEW CHAPTERS JUST ADDED: "HOW MUCH DOES IS COST TO OWN AN AIRPLANE" and "MEMOIRS OF A MOONEY BUYER".

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Differences In Early Mooney Models

Click on Thumbnail Photos and then hit the BACK Button

                                        

   

Some relatively "unknown" Mooneys to look at as well....Enjoy! BTW, be sureto see the Mooney Video at the end of this page! Thanks Mr. Mooney! new!

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Okay, I'm no expert on the Mite So you'll have to contact Boyd Maddox in Houston for that, but I do know you can just about reach the engine in flight to fine tune it! :o)

Original M20 Body stretched two more times over the years.

Fixed Gear M20D (Mooney Master) Same as M20C otherwise.

M20E (Same airframe as the M20C)

M20F (Executive) Became the 201 in 1977 (M20 stretched 10")

M20J (201)

 

 M22 Mustang (Pressurized 5 Place Seating!) See article below..

A-2, M-5 1930 = Similar to A-1 with 125hp Kinner B-5; span: 36'6" length: 21'0" load: 1000#. POP: 1 [X463N], flown by Mooney on a non-stop transcontinental attempt from Glendale CA to Long Island NY as a promotional effort, but only made it to Fort Wayne IN when his fuel pump failed.

M17 (Culver V) 19?? = ClwM; 90hp Continental C-90. Featured a one-piece flap underneath the fuselage and linked to the elevator in a system Mooney called "Simpli-Fly."

Gladys Davis' 1950 Powder Puff Derby entry [N122CX] (William T larkins)

M18-C aka "Wee Scotsman" 1949 (803) = 65hp Continental A-65-8 or -12; span: 26'11" length: 17'9" load: 270# v: 140/125/43 range: 390. $2,325.

M19 1950 = M18-L modified as a mini-fighter, complete with two .30 machine guns and rocket launchers. POP: 1 as a demonstrator for the AF, but no interest was expressed

 

M10 Cadet aka Mooney-Coupe 1969 = Single-tail version of Alon Aircoupe. 90hp Continental C-90-16F; span: 30'0" length: 20'8" load: 438# v: 118/110/46 range: 555 ceiling: 15,500'. $8,295-8,995; deluxe version $10,340

(Japanese Mooney named AEROSTAR)

MU-2 = Licensed production or Japanese Mitsubishi MU-2 twin.

(There WAS actually a genuine TWIN MOONEY built based on the M20 airframe but later scrapped). That was an UGLY airplane and if anyone knows where I can get a photo of the Twin Mooney,  please let me know... (Thanks to Lance W. who sent in these photos of the M20-Twin) Check out the awkward dorsal fin!

     

    

Twin Mooney taxi and in flight photos courtesy of Paul Kehner at Mooney Aircraft Company

Click for larger version  Mooney M.22 Mustang / OE-KGE

An old Friend of the zef, Frenchman; Marc Mosier "Peppy Le Pieu" affectionately is a pilot who often makes his living transporting aircraft across the Atlantic. At one point after delivering a plane to Europe, he bought at Mooney Mustang and crossed back over with it. He liked the plane very much, but was quoted by Flying Magazine that it was a "macho-man's plane" as it took his foot to close the cowl flaps! The Mustang has yet to have a single AD affecting the airframe! There were about 31 of these built from1967-1970, and while the first one's built cost $33,950 finishing up in 1970 at $46,320, the COST for Mooney to build each one was over $65,000!  Long story, but the market would not handle over $65K at the time, thus the demise of the way-ahead-of-its-time (MOONEY ON STEROIDS) the Mooney Mustang!

PERFORMANCE
Max level speed @ 24,000 ft. (kts./mph): 223/256
Standard day @ 24,000 ft.:
Best power - cruise speed (kts./mph):
75% power: 199/229
65% power: 186/214
Best economy - cruise speed (kts./mph):
73% power: 197/226
65% power: 185/215
Max range @ 24,000 ft. (w/ opt. fuel, 45-min. reserve) (nm/sm):
Best power
75% power: 723/832
65% power: 805/926
Best economy
75% power: 837/962
65% power: 907/1043
Fuel consumption (gph):
Best power
75% power: 18.6
67% power: 16.7
Best economy
75% power: 16.1
65% power: 14.1

Did you know that there was once a PRESSUREIZED MOONEY called the 301? (Note the similarities to the TBM airframe) Thank the former French owners for its demise. The six place 301 would probably have been the hottest seller on TODAY'S NEW AIRCRAFT MARKET!!! ARE YOU LISTENING MOONEY?

Mooney 301 (TMB700)

The original Mooney 301 brochure. Target price: $955,000.

In December of 1973, just three months after buying Mooney Aircraft, Republic Steel Corporation hired Roy LoPresti as Vice President of Engineering. Among the many projects developed by Mooney during the next years, the design of a pressurized single was determined to be necessary. In 1980, in response to the Cessna P210 already in production, and to the pending offerings from Beech and Piper (in development) Mooney began design work on the M30 which was designated the MX-1 in engineering.

The M30 was to be powered by a Lycoming TSIO-540 producing 360 horsepower. It would have a top speed of 262 knots, which was equal to 301 mph, and because Mooney was into using speed as a name - it became the Mooney 301.

The M30 was a completely new design for the Mooney engineering department with no similarity to any M20 previously produced. It had high aspect ratio, natural laminar flow wings, and large-span, Fowler type flaps which covered 90 percent of the wings trailing edge. Roll control was to be spoilers augmented by small ailerons on each wing. It would have a service ceiling of 25,000 feet and a cabin pressurized to 5 psig. This would give a 9000-foot cabin altitude at FL250.

N301MX now belongs to an Aviat Husky . . .

The TBM evolution began in late 1973 when the Republic Steel Corporation hired the renowned "Speed Guru" Roy LoPresti as Vice President of Engineering. With the Mooney M20F (Executive) model in its 7th year of production; Roy set out to refine and improve that model resulting in the M20J or (201) where early models of the J were up to 10 knots faster on the same horsepower and cabin size. Together with Roy LoPresti; Mooney recognized the need and began to develop a Pressurized Six Seater powered by a Lycoming TSIO-540 six cylinder engine rated at 360 HP. The new "M30" was designed to have a top speed of 262 knots or 301 MPH; thus the formal designated name of the Mooney 301. The Mooney 301 was a wonderful design keeping the legendary Mooney efficiency intact. This was a NEW MOONEY that shared little to nothing with its M20 brethren, and was a completely new design. The wing was magnificent and had the flavor of a Boeing 727 crossed with the Mitsubishi MU-2 as it had Fowler type flaps along most of the wings trailing edge and the ailerons were comparatively small because roll control was mostly accomplished by spoilers such as found in the MU-2. The first flight was in the spring of 1983, and production was scheduled to begin in 1985.

Within a short time Mooney was sold by Republic Steel and then sold again to a group of French investors headed up by a former Mooney Dealer in France; Alec Couvelaire in association with Armand Rivard; owner of Lake Aircraft. Together they decided to discontinue the production of the 301 in favor of a larger and faster airplane design idea, the TBM700 propjet, and thus the Mooney 301 was unfortunately scraped, but every TBM out there shares parts from the 301 and carries to this day the "M" in "TBM" which stands for "Mooney". "TB" stands for Tarbes, France and "M" is for Mooney. TBM700, cousin of the Mooney 301, uses a 700HSP Pratt & Whitney engine,

 

TBM700 Mooney 301, uses a 700hsp Pratt & Whitney engine

Mooney 301 Specifications:

Cabin: 6-place, pressurized
Top speed: 301mph / 262 knots / 484kmh
Cruise, max altitude, 75% power: 270 mph / 235 knots / 435 kmh
Fuel consumption at cruise: 19.7 gph / 74.6 lph
Fuel capacity: 100 gallons / 379 liters
Range, at cruise, 45 min. reserve: 1,134 miles / 986 nm / 1,825 km
Max. certified altitude: 25,000' (7,620 m)
Rate of climb: 1,400 fpm / 7.1 m/sec
Gross weight: 4,000 lb / 1,814 kg
Useful load: 1,600 lb / 726 kg
Wing span: 37' 0" / 11.3 m
Length: 29' 8" / 9.0 m
Height: 9' 10" / 3.0 m
 

M301cap.jpg - 8383 Bytes

 

Promotional cap from the Mooney 301 marketing program

Had Mooney gone ahead and produced the 301, they would be sitting pretty today considering where Gen Av is headed. What a shame. z

     

The TBM 700 first flew in 1988 and French certification followed in 1990. The TBM 700 was designed together with MOONEY but Mooney withdrew from the project (yeah right..) shortly after certification. In the designation TBM, TB stands for Tarbes, the city in France in which Socata is located, the "M" stands for MOONEY (the intital "M" was kept in the model designation even though Mooney was never involved in the production of the airplane). The TBM 700 also comes in a cargo variant. The TBM 700 uses a Pratt & Whitney PT6A-64 engine delivering 700shp.

The TBM 850 is a more powerful version of the TBM 700 using a Pratt & Whitney PT6A-66D engine flat-rated at 850hp. This extra power gives it a higher cruising speed than the TBM 700 models. The cruise speed now comes close to that of light business jets which are more expensive to operate than a single engined turboprop, hence the slogan Jet Performance at Turboprop Economy. The price of a "typically equipped" TBM 850 in 2006 is listed as 2.8 million US dollars. The outside appearance of the TBM 850 has remained the same as that of the TBM 700.          (Socata bills its TBM-850 turboprop as the fastest production single-engine aircraft available. The 850 is a larger, faster version of the TBM-700).

As of the spring of 2007, over 370 TBMs have been produced.

Specifications given are for the TBM 850

 General characteristics

  • Crew: 1 or 2 pilots
  • Passengers: 4 to 6 (including one passenger in the cockpit if there is no co-pilot)
  • Powerplant: 1 x Pratt & Whitney PT6A-66D with 850hp
  • Wing span: 12,68m (41,6ft)
  • Length: 10,65m (35ft)
  • Height: 4,36m (14,3ft)
  • Empty weight: 2,132kg
  • Loaded maximum: 3,370kg (3,354kg max take-off)

 Performance

  • Long Range Cruise speed: 252kts
  • Maximum Cruise speed: 320kts
  • Ceiling: 31.000ft (maximum certified altitude)
  • Climb rate: 2380 ft/min
  • Time to Climb to 26,000 ft: 15 min
  • Range: 2870km (1550nm) (1,784 mi)

  

 The Mooney M20-L PFM (Porsche Mooney) was a wonderful idea and the greatest advancement in general aviation since the removal of wing struts (sorry 172 owners). Not only did the plane have the aviation version of the Porsche 911 engine (220 HP), but it was all electric and no vacuum system aboard. It used an electric 3 buss 2 battery system to drive everything aboard including the most expensive and outright beautiful and special operating instruments where each instrument looked like a fine Swiss watch makers' result. My understanding at the time was that to replace those instruments would run in the neighborhood of $16,000.00 which was a lot of geetum back in 1988. There were a total of 40 PFM's made in 1988 and 1 in 1989 before Mooney called it quits for the PFM. There were several reasons for its demise and a loss of MILLIONS in development costs for Mooney as well as Porsche. Some of those reasons were COST: Not wanting to sell the plane in the RED as was the case with the Pressurized Mooney M-22 Mustang, Mooney sold the PFM for about $190K on average out the door price while the much faster 252 was selling for about 5 grand less, and after all, it’s all about speed right? Some of the other factors were the composite prop which had a blade life of 1500 hours and a heavy cost of replacement blades as well as an automatic $5800.00 (at the time) to overhaul the gear reduction system, again each 1500 hours. It was to my thinking a good trade-off as Porsche had a program to do a FREE top overhaul at about 1,000 hours and a guarantee to sell you a BRAND NEW engine for only $20,000.00 once your old one reached the 2,000 hour TBO. Porsche was in the process to up the TBO to 4,000 hours once they could prove to the FAA what they already knew, that it was a very strong, bullet proof engine! Porsche was also in the process of upping the horse power of that engine to over 250 and put a turbo charger on it. That would have really been a GOER! Proper marketing did not take place in my opinion of this fabulous airplane that I for one was much saddened to see it go. The PFM was about the easiest HIGH PERFORMANCE airplane to ever take to the sky. There was no MIXTURE nor PROPELLER control! There was just this sexy POWER SLIDE BAR that you would push right in as fast as you wanted and linkage (not computerization as many thought) would regulate the mixture and prop setting. Very ingenious! And because the 911 style engine had its own cooling fan, there was never a worry of shock cooling that engine. You could easily and worry free pull off all of the power for descent if you wanted, so “SLAM DUNK” approaches were made much easier than any previous Mooney ever made. While I am not the most avid fan of the “super stretch” Mooney body (12" more than the 252, and 22" total stretch over the original M20 airframe) that ALL new Mooney use today, the PFM was the first to get that body. The windows were the same size as the 252 instead of the much larger viewing area used today, but as I said the body is the same. Because of the shape of the engine, the PFM’s cowl was more streamlined looking than any other Mooney, in fact it looked much like a Turbine engine was under the bonnet. I loved flying the PFM and found it to exceed the specs in the owners manual and even though it had the super stretch, heavier body, the performance to me was more than admirable on not much more horsepower than the 201. Cruising in the low to mid 160 KT range was an easy achievement and my feeling was that when (if) the turbo version would have made it to fruition, we would have had a 200 KT Porsche. I miss that engine; it was as easy to start as any automobile and the sound if the PFM taxiing by was pure Porsche 911! The yokes, the instrumentation, the fit and finish, the engine, the sound, the flying qualities………….man I miss that Model and I miss what it could have become; so next time you start complaining that today’s aircraft engines are actually 1940’s design, remember the (ahead of its time) ENGINE DESIGN we all let get away!

EPILOG: April 2009. Porsche contacted the FAA and said that they no longer support the PFM engine and therefore there will be no parts available and requested the FAA remove the PFM's Type Certificate. The FAA wasn't all that "knee jerk" this time and DID NOT ground the PFM, but it did state that should the engine require parts at maintenance and none were available, that would in effect ground the airplane and that particular one would lose its Type Certificate and so on until every last remaining PFM requires parts, so it's as good as over and they airframes will need a conversion. Problem is that no one I know is doing that "Ovation" conversion to the PFM any longer, and while you can get parts to do it, you cannot order the log book supplement that has to accompany the conversion. You remaining PFM guys are going to have to get creative or get stuck with a very heavy and beautiful paper-weight....end.

OH! VATION

THE NEWER MOONEYS are based on the stretched once again original PFM airframe. Stretching the airframe once again somewhat took away from the legendary Mooney strength apparently as maneuvering speed was reduced from 134 kts Va speed of the original M20 body to 118-124 Va of the newest models depending on whom you ask. Don't worry however, any Mooney is about twice as strong as the competition!

Glass Panel Mooney's!

    How Many of you would be interested in purchasing the fully aerobatic "TIGER-PREDATOR" short M20 Body with super high performance motor?! I dunno, maybe if they took the E model body and put the Ovation IO-550 engine in that bad boy.....

The Tiger, formally known as the Mooney Predator, was created to compete for the Air Force’s

primary trainer contract in 1989-1990. Mooney hoped to win the contract, use the government’s cash

to certify the aircraft, and then develop a civilian version. The aircraft wasn’t selected for the

contract, however, and languished for the next five years in the back of a Mooney engineering test

hangar. Stripped of its engine, canopy and cowling, the two-seater plane was left for dead.

Enter Tom Bowen, then Mooney’s vice president of engineering. After examining the flight data,

Bowen felt the airplane’s quick spin ability would make the Predator an ideal aerobatic aircraft for

Mooney. He and a small group of colleagues committed themselves to rebuilding it. In 1996, the

extensive refurbishment process began. A 300 hp Continental IO-550 engine filled the empty engine

compartment. A new prop and canopy was fitted. The original red-and-white paint scheme was

replaced by black-and-orange stripes, creating the appearance of a Bengal tiger. The Tiger roared

into the 1996 Oshkosh Air Show and became an immediate crowd favorite. The cat was ready to

prowl the skies.

Mooney began preparing the Tiger for the category of aerobatic operation. However, the airplane

wasn’t certified. It would take at least three years and approximately $5 million to reach certification

requirements. Due to the high cost, Mooney refocused its attention to other projects and once again

the little plane was caged back at the hangar.

This sleek aircraft combines benefits from several Mooney models – a short body from the M20C

and M20E, a tail from the M22 Pressurized Mustang and the M20J 201 wing. A canopy replaces the single door and sticks

substitute for regular controls. The big Continental engine makes the Tiger fast. It reaches speeds

up to 180 ktas, only 10 ktas less than Mooney’s Ovation2 GX. A spartan interior with no insulation

gives the aircraft a race-car sound.

“Even as a bare-bones aircraft, the Tiger maintains the famous Mooney stability,” said David

Copeland, Mooney Airplane Company vice president of sales and marketing. “Design and

engineering efforts such as those taken with the Tiger have helped further our work – and success –

with other models, such as Mooney’s new Ovation2 GX and Bravo GX models.”

Tiger statistics

Maximum speed 180 ktas

Rate of climb 1,400 ft./min.

Maximum altitude 20,000 ft.

Stall speed 56 ktas

Take-off distance to 50 feet 1,500 ft.

Landing distance over 50 feet 2,100 ft.

Range 450 nm

Endurance 3 hrs.

Wing span 36’1”

Max gross take-off weight 2,900 pounds

Aircraft empty weight 1,916 pounds

Useful load 984 pounds

Usable fuel 471 pounds

78.6 USG in two wing tanks

  

SETTING THE RECORD STRAIGHT on a Mooney Discussion Forum:

It was stated at one of the Mooney forums that a test pilot had not bailed out of a 1961 B model as cited in my article below (The B Model) to the contrary, and one forum member asked a former Mooney Factory man who is now the head of a popular Mooney periodical if it were true what Mooneyland had stated; that a test pilot had to bail out and he said "NEVER". Once I read that I re-checked my facts and below is the reply from Boyd Maddox; a Houston Mooney expert:

Sorry Trey but Rich is correct
One and only one (test pilot) did have to bail out and here is why......
The test pilot that the FAA had was fresh out of the military and did not have a checkout in the aircraft.
He tried A spin at aft cg and it went flat.
He did not dump the aft ballast nor did he use the spin chute. He kicked the door off the hinges without pulling the release.
Technically you are right he was NOT a MOONEY TEST PILOT but rather an FAA TEST PILOT.
Boyd Maddox



Fri, 12 October 2007 19:18
Michael Brown
Messages: 45
Registered: August 2005


Mooneyland's site states that a Mooney test pilot had to bail out of an M20B after entering a flat spin:

http://www.mooneyland.com/Mooney%20Models.htm

Could Rich be wrong?
Michael
1966 M20E
N435DB
KOSU


Fri, 12 October 2007 10:39
trey_hughes
Messages: 254


Which leads me to the question, how many Mooney test pilots have ever had to
bail out in a chute over the years?

NONE

Regards,
Trey

The B model was available for only one year, and that was 1961.  That model was a good Mooney, but had a tendency of getting in to a flat spin when spun, in fact, the test pilot (FAA test pilot, not Mooney test pilot as I had previously reported) had to bail out of that model when spin testing.  After a C.G. change, that potential problem was alleviated.  There is nothing wrong with the B model so long as it was not spun.  It had the same engine/prop combination as the subsequent C models, which is the 180 H.P. carbureted Lycoming engine.  That engine has been known to go up to 4000 SMOH on some flight school aircraft.  This engine is probably the most “bulletproof” engine of its class. 

However, because it is carbureted, it is subject to carb-ice, so, it has a carb heat knob to check on run-up, as well as when ever you suspect carb-icing.  Both the O-360 and IO-360 Lycoming's have a 2000 hour TBO, but you should not exceed that by more than about ten percent, in the E's F's and J's, even if still running great, whereby the C's 0-360 can sail past TBO if taken care of and watched closely once past TBO.  TBO is based on an average of all uses of a particular engine, and is not mandated to overhaul at TBO unless operated on FAA's part 135.  There are just too many variables, which help determine when an engine should get an overhaul.

Because the O-360 is carbureted and not fuel injected as the 200 horse power version of the same basic engine, it tends to run a bit rougher than the fuel injected version, which distributes fuel exactly to each cylinder, making it a smoother running engine.  The C model will give you a pretty good shudder when you shut it down vs. the E, which shuts down a bit smoother.

Many people prefer the C model, as it is the most simple engine/airframe, and normally less expensive than the E model, which has 20 more horse power and smoother running engine.  There is no difference in airframe and prop between the C and E model Mooney other than the engine and horse power.  There is nothing inherently wrong with either model, as they both do their respective missions with speed and efficiency.  Amazing speed and efficiency actually.

The D model was originally a fixed gear version of the C model with the same horsepower, but most have been converted to retractable gear, thus when you see C/D Mooney, it was formally the fixed gear which was converted, making it about the same aircraft.

If you were to do a drag race between the C and E model at full power, you would see about a 6-8 knot difference favoring the E model with more horse power obviously.  In the real world, however, most C model types will fly the C averaging 2350 and 24 Squared, as the faster you turn it, the more it vibrates as a rule, conversely, many people run the E models at 25 squared because the faster you turn the injected engine, the smoother it seems, so with that, you will see about low to mid 140 knot range in the C vs. 150-155 KTAS in the E model.  You will really appreciate the E model’s smoothness when flying at high altitudes where you can run up to 2700RPM smoothly to get the more horse power needed in a normally aspirated engine, so like I said, in real life, the E out performs the C, but because of the potential longevity of the properly maintained engine, the hourly cost of operation can be substantially lower than it’s close cousin, should you choose to keep it running well beyond TBO as many do with this engine.

One other difference between the two is the fact that the E model has what is called “ram air”.  This is a “poor man’s” turbo charger.  You would normally open the ram air above 5,000’, in clear, clean, not IMC air where 75%power is no longer possible.  You may pick up as much as 1-1/2” additional manifold pressure using the ram air.  What is ram air?  There is a small rectangular door that you can open to bypass the air filter, and inject ram air directly in to the engine in a straight line through a venturi, which will allow air to reach the injector directly without having to go around any corners as when through the filter, thus more dense air enters the engine more efficiently creating more horsepower at the higher altitudes.  Flying through IMC with the ram air opened can cause an engine failure due to super freezing the air through the venturi, because of the increase in moisture as found in the clouds.  In any event, remember to shut the ram air when entering IMC.

You should not use it on the ground unless you can be certain that the air is very clean and you will not pick up dust on take off.  The only time you would consider using the ram air in that situation is when taking off at a very high altitude airport with high density altitude where the difference in horse power may make the difference in getting off the ground or not.  Rule of thumb however, is to remember not to use it on the ground, and only in clean, clear air.

If you lower the landing gear while forgetting to shut the ram air off, you will get a very bright orange light to remind you to shut it off.

The F model Mooney, also known as the Executive was stretched ten inches, with about5” more rear seat leg room and the rest in the baggage compartment.  It uses the same engine as the E model, the IO-360-A1A.  “I” standing for Injected.  The 180 horse power engine is the O-360, non injected, or carbureted.  Both engines have 360 cubic inches, which for a 4 cylinder engine, is a huge capacity.  The pistons are huge in those engines.  Many automobile V-8 engines do not have that much capacity.

So, you get more length in the F model, as well as 64 gallons usable fuel, vs. 52gallons usable in the C and E models.  Of course, the F model has a higher gross weight and a longer airframe, so you will burn more fuel in the F model.  It all varies with altitude and load, but expect about 9-9-1/2 GPH in the E model, about half a gallon less in the C, and about 1-1/2 GPH more in the F model.  The F model will fly about the same speed as the C model, even though it has 20 more horsepower, however, you get a bit more range due to the extended fuel capacity.

Strength of the tail feathers was increased in the F model to handle the longer, heavier load by using larger and corrugated skins on the elevator and rudder as opposed to more simple to construct flat skinned short bodies.  The F model also has a heavier feel to it, a bit more stable on approach, but also a bit more nose heavy and a slightly lower roll rate.

The G model uses the C model’s lower horse powered engine, with the same lower fuel capacity of the C, and the same non corrugated tail feathers.  Some consider the G model to be a bit underpowered while others really like the G’s extra room with their favorite O-360 engine.

You can fly with 4 people after checking the load weight in all M-20’s, but if your trips usually fill 4 seats, you may want to consider the F model size for a bit more leg room.  However, I have loaded the short bodies with 4 people, and once they are in, seem to have as much leg room as your average airliner, and just a bit more in the stretched body.

The short bodies have lighter, more crisp handling however, than the stretched versions, but tend to “fishtail” a bit more in some types of turbulence, but nothing as bad as the V tail Bonanza however.  You can usually alleviate that by placing both feet on the rudders.  The short body Mooney’s remain the most popular with economical buyers.

The F model is virtually the same airframe as the 201 or J model.  Same fuel capacity and same horsepower.  However, all pre J models have individual dual mags, while the J model uses what is called, the single dual mag.  Both mags are housed within one housing.  While they have proven to be reliable, there are a few, fairly rare things that can go wrong to short out the entire dual mag rendering you “magless” and consequently, engine powerless.

The F model became the J model with some factory speed mods and a bit of LoPrestimagic.  I say magic because if you were to install the same mods on the earlier F model as the J had, you still won’t go as fast in the F as the J for some reason in my experience.  Weird huh?  Suffice to say that all Mooney’s have some magic in them.  It’s a wonder to go as fast as Mooney’s can go for the horsepower, but that’s the Mooney mystique.

The early J models also had ram air, but the gain of M.P. was only about half to ¾inch gain, as the entire induction system was improved with that model.  Later J models like the MSE had eliminated ram air, and yet were the fastest J models.

The 201 or J model was the first production aircraft to go one mile per hour per horsepower on the test aircraft.  In real life, the early J models would fly at about the same speed as the lighter, shorter E model, about 155 knots optimum speed, but doing so in the longer, bit more comfortable (to rear seat passenger) stretched body as in the J. Widths are nearly the same on all models, which is wider than even Bonanza’s and the Piper PA-28series……..surprise!!!!  So much for the “tight” Mooney myth.  You simply sit a bit lower, as in a sports car for instance, and have the necessary amount, but not more head room than you need which translates in to drag outside the plane.  Personally, I love the feeling of being a part of the machine, and Mooney gives you that feeling just like a fine sports car.

The K model, or 231/252 airframe is the same basic airframe as the F and J models.  The elevator has an extended tab to help compensate for the longer, heavier six cylinder Continental engine which is turbo charged.  You have 210turbo'd horsepower available, and up to 220 in the late 252 called the Encore.  You should expect to see speeds of up to 225 MPH at the higher altitudes in the K model, more in the 252 K model, and more yet in the Encore.  Fuel capacity is more also.  About 76 gallons usable in the K series.  However, you can expect to burn between 12 and 14 GPH at cruise in the K models, depending on altitude, load, and flight conditions.

About half of the 1800 TBO Continental’s require top overhauls at about half life expectancy.  The difference is how the plane is flown and at what altitudes.  The higher they run (up to 24,000’ service ceiling” the hotter they run, and thus, the more likelihood of needing a top half way through TBO.  There seems to be little difference in longevity whether you have the original GB vs. the LB, and even MB engines.  Plan not to exceed TBO with these engines in any event.

On the upside, the six cylinder engine is easier to start, and runs smoother and quieter than the 4 banger brethren.

The 201, 231, and 252 were named after the test aircraft’s top speed, down low, full throttle, and mostly a stripped aircraft, yet to have the weight of radio’s and the drag of antenna’s.  However, the 252 production aircraft, can really attain that speed in MPH on production aircraft, and just may be the best Mooney overall to come out of the factory.  Downside is the acquisition prices, yet they remain a great deal speed for speed on the market.

All Mooney’s are basically hand built and vary in both directions from plane to plane.  Proper rigging also plays a significant role in the speed of any Mooney.

What all of these Mooney’s have in common, is the brilliant design of Al Mooney& company, as well as the legendary strength and the near fool proof and unbreakable airframe.  They all share that wonderful steel tubing “roll cage” that surrounds the passenger compartment.  The fact that all Mooney’s have that wonderful, but heavy (80+lb.)  “roll cage” to protect you, makes any Mooney a wonderful buy on today’s market.

The turbo TLS Bravo as well as the normally aspirated Ovation are much different aircraft than the ones mentioned above.  In 1988, Mooney saw fit to once again stretch the Mooney fuselage with the introduction of the PFM Porsche powered Mooney.  This additional stretch made these Mooney’s have a much different feel than the earlier versions of the M-20 airframe, but we’ll leave that for a future examination.

It is our hope that this article helps you understand the basic differences between the various Mooney models.  Hey, buy anyone you wish, just be sure to buy a MOONEY!  There is nothing out there that can match them overall for speed and efficiency, and in my opinion, safety in passenger protection, and if you want the real skinny on these remarkable aircraft, don’t listen to the rumors of non Mooney types.  Ask a Mooney owner next time you see one on the ramp.  You’ll get an entirely differing perspective.  Most Mooney pilot/owners can indeed be affectionately referred to as “Mooniacs”.  It only takes one flight to convert most to love this stable, reasonably docile and super efficient brand of speedsters.

Fly safe,

Richard Zephro

Pressurized six pax MOONEY 301

The following table of Mooney models through the TLS is below and was reprinted from the Mooney Events website in which we at Mooneyland aided them on their research to include this information on their site.

When printing these tables, "landscape" mode is preferred, as they are 750 pixels wide.

A: average retail price, including popular options

Year Model Serial # Description No. built Factory price
1948 M18 Mite 02 to 12 25hp Crosley auto engine -- later converted to Lycoming 65hp O-145. Single place. Mite features listed here at Dave Rutherford's Mitesite.
Mite #1 was N3199K, now hanging at Smithsonian Institution, Washington, DC.
Mite #3 was N3159K, now at Sun 'n Fun Museum in Florida.
11 $1,995
1949 M18L Mite 02 to 67 Lycoming 0-145-B2. Single place. Michael Bolinger's N246MM. Early Mite panel. 66 $2,795
1950 M18L Mite 68 to 82 Lycoming 0-145-B2. Single place.. 15 $2,795
1950 M18C Mite 201 to 240 Continental A65-12 or -8. Single place. 40 $2,965
1951 M18LA Mite 101 to 114 Lycoming 0-145-B2. Gross weight increase from 780lb. to 850 lb. Maneuvering, max structural cruising, flaps extended speeds increased to match M-18C Mite. Single place. Photo of N60MM. 14 $2,965
1951 M18C Mite 241 to 249 Continental A65-12 or -8. Single place. 9 $2,965
1952 M18LA Mite 115 to 135 Lycoming 0-145-B2. Single place. 21 $2,995
1952 M18C Mite 250 to 277 Continental A65-12 or -8. Single place. Christopher Byrd's N4075V. 28 $2,965
1953 M18LA Mite 136 to 145 Lycoming 0-145-B2. Also known as "Wee Scotsman." Single place. 10 $2,840 - $3,029
1953 M18C Mite 278 to 299 Continental A65-12 or -8. Also known as "Wee Scotsman." Single place. Steve McGuire's restored N85PM was the first aircraft produced in 1953. 22 $2,965
1954 M18C Mite 300 to 322 Continental A65-12 or -8. Single place. Vernon Flacksberth's N4147. 23 $2,965
1955 M18C55 Mite 323 to 357 Continental A65-12 or -8. High-canopy models. Single place. 35 $2,965
1955 M20 Mark 20 1001 to 1010 Lycoming 0-320 (150HP). Wood wing. Four place. 10 $12,500
1956 M20 Mark 20 1011 to 1061 Lycoming 0-320 (150HP). Wood wing. Four place. 51 $15,590A
1957 M20 Mark 20 1062 to 1166 Lycoming 0-320 (150HP). Wood wing. Four place. 105 $15,950A
1958 M20 Mark 20 1167 to 1200 Lycoming O-320 (150HP). Wood wing. Four place. 34 $
1958 M20A Mark 20A 1201 to 1303 Lycoming 0-360-A1A (180 HP). Wood wing. Four place. 103 $14,750 - $17,656A
1959 M20A Mark 20A 1304 to 1534 Lycoming 0-360-A1A (180 HP). Wood wing. Four place. Thomas Jaekel's D-EMRG in its hangar in Germany. 231 $15,450
1960 M20A Mark 20A 1535 to 1700 Lycoming 0-360-A1A (180 HP). Wood wing. Four place. 165 $

All aircraft manufactured to this point had wings and tail made of wood covered with fabric (the body cage was always steel, with aluminum skin).
Aircraft after S/N 1701 had metal wings and tail.

* Master models in the following table were fixed landing gears.

Year Model Serial # Description No. built Factory price
1961 M20B Mark 21 1701 to 1924 Lycoming 0-360-A1A (180 HP) or -A1D (impulse coupled mags). Four place. 223 $15,995 - $18,000A
1962 M20C Mark 21 1940 to 2276 Lycoming 0-360-A1D(180 HP). Click here for detailed change list in C model. Four place. 336 $15,995 - $19,000A
1963 M20C Mark 21 2297 to 2622 Lycoming 0-360-A1D(180 HP). Four place. 328 $20,000A
1963 M20D Master 101 to 200* Lycoming 0-360-A1D(180 HP). Four place. 100 $13,995
1964 M20C Mark 21 2623 to 2806 Lycoming 0-360-A1D(180 HP). Four place. 183 $21,000A
1964 M20D Master 201 to 251* Lycoming 0-360-A1D(180 HP). Four place. Chris Nowak's N1916Y. 51 $15,814
1964 M20E Super 21 101 to 469 Lycoming I0-360-A1A(200 HP). Bendix fuel injection. Altitude power boost. Four place. 366 $18,450 - $22,000A
1965 M20C Mark 21 2807 to 3184 Lycoming O-360-AlD(180 HP). Positive Control (PC). Four place. 379 $22,000A
1965 M20D Master 252 to 259* Lycoming 0-36O-AlD(180 HP). Four place. 8 $
1965 M20E Super 21 470 to 831 Lycoming I0-360-A1A(200 HP). Bendix fuel injection. Altitude power boost. Positive Control (PC). Four place. Colin Bitterfield's N3218S exterior and panel. 363 $23,000A
1966 M20C Mark 21 3185 to 3466 Lycoming 0-360-A1D(180 HP). Positive Control (PC). Four place. 280 $23,000A
1966 M20D Master 260 only Lycoming 0-360-AlD(180 HP). Four place. 1 $
1966 M20E Super 21 832 to 1301 Lycoming IO-360-A1A(200 HP). Bendix fuel injection. Altitude power boost. Positive Control (PC). Four place. 473 $24,000A
1966 M20F Executive 660001 to 660003 Lycoming IO-360-A1A(200 HP). Fuselage extended by 1', cabin by 10". Bendix fuel injection. Altitude power boost. Positive Control (PC). Four place. 3 $21,995
1966 M22 Mustang 660004 to 66006 Lycoming TI0-541-A1A(310 HP). Turbosupercharged, fuel injection, pressurized. PC, power quadrant. Five place. Charles Reeves' N7735M, from forward and aft. 3 $33,950
1967 M20C Mark 21 670001 to 670149 Lycoming 0-360-A1D(180 HP). PC. Four place. 149 $24,000
1967 M20E Super 21 670001 to 670062 Lycoming I0-360-A1A(200 HP). Bendix fuel injection. Altitude power boost. Positive Control (PC). Four place. 62 $25,000A
1967 M20F Executive 670001 to 670539 Lycoming I0-360-A1A(200 HP). Bendix fuel injection. Altitude power boost. Positive Control (PC). Four place. 536 $21,995 - $26,000A
1967 M22 Mustang 670001 to 670004 Lycoming TI0-541-A1A(310 HP). Turbosupercharged, fuel injection, pressurized. PC, power quadrant. Five place. 4 $42,437A
1968 A2-A Cadet B-261 to B-298 Continental C90-16F(90 HP). Aircoupe dual-fin tail. Two place. 38 $8,295
1968 M20C Ranger 680001 to 680198 Lycoming 0-360A1D(180 HP). Replaces Mark 21. Cowl flaps fixed, dorsal fin removed, entrance step fixed, 1-piece windshield. PC. Four place. 198 $25,000A
1968 M20F Executive 680001 to 680206 Lycoming I0-360-A1A(200 HP). Bendix fuel injection. Altitude power boost. Positive Control (PC). 1-piece windshield. Four place. 206 $25,294A
1968 M20G Statesman 680001 to 680164 Lycoming 0-360A1D(180 HP). Long (F model) fuselage, fuel 52 gallons, PC, 1-piece windshield. Four place. 164 $18,790 - $26,000A
1968 M22 Mustang 68001 to 68015 Lycoming TI0-541-A1A(310 HP). Turbosupercharged, fuel injection, pressurized. PC, power quadrant. Five place. 15 $55,584A
1969 M10 Cadet 690003 to 690011 Continental C90-16F(90 HP). Now single-tail. Two place. 9 $11,310A
1969 M20C Ranger 690001 to 690098 Lycoming 0-360-A1D(180 HP). Electric gear, flaps. New power quadrant. Dorsal fin removed, entrance step fixed, 1-piece windshield. PC. Four place. 98 $26,000
1969 M20E Chaparral 690001 to 690073 Lycoming I0-360A1A(200 HP). Shortened (by 10" F model) with electric gear, flaps, PC, 1-piece windshield, 1969 power quadrant. Fuel: 52 gals. Four place. 73 $27,000A
1969 M20F Executive 690003 to 690092 Lycoming I0-360-A1A(200 HP). Bendix fuel injection. Altitude power boost. Positive Control (PC). 1-piece windshield. Four place. 90 $28,000A
1969 M20G Statesman 690001 to 690020 Lycoming 0-360-A1D(180 HP). Long (F model) fuselage, fuel 52 gallons, PC, 1-piece windshield. Four place. 20 $26,500A
1969 M22 Mustang 690001 to 690005 Lycoming TIO-541-A1A(310 HP). Turbosupercharged, fuel injection, pressurized. PC, power quadrant. Five place. 5 $
1970 M10 Cadet 700001 to 700050 Continental C90-16F(90 HP). Mooney 1-piece tail. Two place. 50 $12,010A
1970 M20C Ranger 700001 to 700091 Lycoming 0-360-A1D(180 HP). 1-piece windshield, PC, electric gear, flaps. Four place. 91 $18,995 - $27,000A
1970 M20E Chaparral 700001 to 700061 Lycoming IO-360-A1A(200 HP). 1-piece windshield, PC, electric gear, flaps. Four place. Brian Wilson's re-painted N9493V from aft and forward. 61 $28,000A
1970 M20F Executive 700001 to 700072 Lycoming I0-360-A1A(200 HP). 1' longer cabin, 1-piece windshield, PC, electric gear, flaps, 64 gal. fuel. Four place. 72 $29,000A
1970 M20G Statesman 700001 to 700006 Lycoming 0-360-A1A (180 HP). 1-piece windshield, PC, electric gear, flaps, 52 gal. fuel. Four place. 6 $27,500A
1970 M22 Mustang 700001 to 700006 Lycoming TI0-541-A1A(310 HP). Turbosupercharged, fuel injection, pressurized. PC, power quadrant. Five place. 6 $55,584A
1971 M20C Ranger 20-0001 to 20-0009 Lycoming 0-360-A1D(180 HP). Aerostar markings, new air venting for cabin. Four place. 9 $19,995 - $28,000A
1971 M20E Chaparral 21-0001 to 21-0023 Lycoming I0-360-AlA(200 HP). Aerostar markings. New cooling for engine. Four place. 23 $21,995 - $29,000A
1971 M20F Executive 22-0001 to 22-0012 Lycoming I0-360-A1A(200 HP). Only long cabin in 1971, sold as Aerostar 220 Executive. Four place. 12 $23,995 - $30,000A

Republic Steel Corp. purchased Mooney Aircraft from Butler Aviation on Oct. 4, 1974 and officially reopened the production line on Jan. 1, 1975.

Year Model Serial # Description No. built Factory price
1974 M20C Ranger 20-0010 to 20-0046 Lycoming 0-360-A1D(180 HP). Electric gear & flaps, cowl flaps fixed, no dorsal fin, fixed step, PC. Four place. 36 $30,000A
1974 M20E Chaparral 21-0024 to 21-0060 Lycoming I0-360-A1A(200 HP). Electric gear & flaps, PC, 1-piece windshield. Four place. 37 $31,000A
1974 M20F Executive 22-0013 to 22-0078 Lycoming I0-360-AlA(200 HP). 1' longer fuselage. Electric gear & flaps, PC, 1-piece windshield. Four place. 66 $32,500A
1975 M20C Ranger 20-1147 to 20-1185 Lycoming 0-360-AlD(180 HP). Electric gear & flaps, cowl flaps fixed, no dorsal fin, fixed step, PC. Four place. 39 $31,000A
1975 M20E Chaparral 21-1161 to 21-1180 Lycoming I0-360-A1A(200 HP). Electric gear & flaps, PC, 1-piece windshield. Four place. 20 $32,500A
1975 M20F Executive 22-1179 to 22-1305 Lycoming I0-360-A1A(200 HP). 1' longer fuselage. Electric gear & flaps, PC, 1-piece windshield. Four place. 127 $34,500A
1976 M20C Ranger 20-1186 to 20-1218 Lycoming 0-360-A1D(180 HP). Electric gear & flaps, cowl flaps fixed, no dorsal fin, fixed step, PC. Four place. 33 $33,000A
1976 M20F Executive 22-1306 to 22-1432 Lycoming I0-360-A1A(200 HP). 1' longer fuselage. Electric gear & flaps, PC, 1-piece windshield. Four place. 127 $36,500A
1977 M20C Ranger 20-1219 to 20-1243 Lycoming 0-360-A1D(180 HP). Electric gear & flaps, cowl flaps fixed, no dorsal fin, fixed step, PC. Four place. 25 $35,000A
1977 M20F Executive 22-1433 to 22-1439 Lycoming I0-360-A1A (200 HP). 1' longer fuselage. Electric gear & flaps, PC, 1-piece windshield. Four place. 7 $38,500A
1977 M20J 201 24-0001 to 24-0377 Introduction of J model. Lycoming I0-360-A1B6D(200 HP). Drag reduction to F model by Roy LoPresti increases speed by 21 knots. Prop is squared-off; original gear-down 120 mph. Four place. Click here for Mark Napier's detailed Mooney 201 evolution, starting in 1977. 377 $41,200 - $45,500A
1978 M20C Ranger 20-1244 to 20-1258 Lycoming 0-360-A1D(180 HP). End of short-cabin era. Four place. 15 $37,500
1978 M20J 201 24-0378 to 24-0757 Lycoming I0-360-A3B6D(200 HP). Long fuselage (24'8" or 7.6m) now standard. Push-pull power controls. Changes from '77 J model: engine model, fuel selector; panel; landing light mounting; landing gear motor; landing gear speed now 150 mph; prop rounded. Four place. Photo of Jim Murphy's N201XG with original exterior and a slightly modified panel. 380 $43,500 - $86,675
1979 M20J 201 24-0764 to 24-0900 Lycoming I0-360-A3B6D(200 HP). New 1978 configuration. Strengthens cowl flap mounting. Four place. 137 $53,500A
1979 M20K 231 25-0001 to 25-0246 Continental TSI0-360-GB(210 HP). First 6-cylinder engine. Turbocharged with Rajay fixed wastegate. Fuel increased to 75 gallons. Dorsal fin airscoop. Curved wingtips, enclosed lighting. Four place. 246 $51,975
1980 M20J 201 24-0901 to 24-1037 Lycoming I0-360-A3B6D(200 HP). New 1978 configuration. Four place. 137 $58,500A
1980 M20K 231 25-0247 to 25-0446 Continental TSI0-360-GB(210 HP). Same configuration as 1979. Four place. 200 $63,500A
1981 M20J 201 24-1038 to 24-1213 Lycoming I0-360-A3B6D(200 HP). Sculpted wingtips added, 201 number now on tail fin. Four place. 176 $63,500A
1981 M20K 231 25-0447 to 25-0612 Continental TS10-360-GB(210 HP). Soundproofing improved, 231 number on tail fin. Four place. 166 $69,000A
1982 M20J 201 24-1214 to 24-1326 Lycoming I0-360-A3B6D(200 HP). Double plane door window, sound insulation added. Four place. 113 $68,000A
1982 M20K 231 25-0613 to 25-0717 Continental TS10-360-GB(210 HP). Pressurized mags added, improved exhaust resonator. Four place. 105 $76,000A
1983 M20J 201 24-1327 to 24-1417 Lycoming I0-360-A3B6D(200 HP). Only change to 1982 was paint design change. Model numbers dropped from tail fin. Four place. 91 $76,000A
1983 M20K 231 25-0718 to 25-0780 Continental TSI0-360-GB(210 HP). Same paint design changes as made to 201. Four place. 63 $85,000A
1984 M20J 201 24-1418 to 24-1499 Lycoming I0-360-A3B6D(200 HP). Composite 1-piece belly, 2" power gauges, internally lit instruments. Four place. 82 $123,795A
1984 M20K 231 25-0781 to 25-0841 Continental TSI0-360-LB1(210 HP). Same changes as 1984 201, plus new engine with redsigned fuel distribution, nitrited cylinders, steel belted pistons, new rod design. Four place. 61 $139,915A
1985 M20J 201 24-1500 to 24-1550 Lycoming I0-360-A3B6D(200 HP). First wing-mounted speed brakes (Precise Flight). Special Edition introduces upgraded interiors. Four place. 51 $145,640A
1985 M20K 231 25-0842 to 25-0889 Continental TSI0-360-LB1(210 HP). Same changes as 1985 J models. Four place. 48 $169,925A
1986 M20J 201 24-1551 to 24-1588 Lycoming I0-360-A3B6D(200 HP). Lean Machine and Special Edition marketed. Four place. 38 $145,640
1986 M20K 252 25-1000 to 25-1066 Continental TSI0-360-MB(1) (210 HP). Replaces 231 with intercooled engine, Garrett variable wastegate. First model with curved side window. Also, enclosed landing gear; 28V electrical. Four place. 67 $123,400 - $154,000A
1987 M20J 205 24-3000 to 24-3056 Lycoming I0-360-A3B6D(200 HP). Features from 252 added to 201: enclosed landing gear; 28V electrical and rounded side windows. Four place. 57 $149,440A
1987 M20J 201 (LM) 24-1589 to 24-1641 Lycoming I0-360-A3B6D(200 HP). Unchanged from 1986. Four place. 53 $
1987 M20K 252 25-1067 to 25-1157 Continental TSIO-360-MB(1) (210HP). Same as 1986. Four place. 91 $177,500A
1988 M20J 205 24-3057 to 24-3078 Lycoming I0-360-A3B6D(200 HP). Uses Special Edition interior of 252 -- new seats, center armrests. Four place 22 $134,330A
1988 M20J 201 24-1642 to 24-1685 Lycoming I0-360-A3B6D(200 HP). Last of square-cornered windows. Four place. 44 $102,970A
1988 M20K 252 25-1158 T0 25-1198 Continental TSI0-360-MB(1) (210 HP). FlightSafety training offered. Four place. 41 $179,845A
1988 M20L PFM 26-0001 to 26-0040 Porsche PFM 3200 N03 (217 HP). Porsche 911 derivative engine. Fuselage length adds 20" and cabin 12". First of long body aircraft -- that becomes standard body in 1999. 40 $142,900
1989 M20J 201 24-3079 to 24-3143 Lycoming I0-360-A3B6D(200 HP). Curved window corners; 28V electrical, new interior. Four place. Gordon Cowles' 201 exterior and panel, stock with a KLN89 and Strike finder added. 65 $129,735A
1989 M20K 252 25-1199 to 25-1220 Continental TSI0-360-MB(1) (210 HP). Same as 1988 model. Four place. 22 $185,825A
1989 M20J 201AT 24-1686 Lycoming I0-360-A3B6D(200 HP). Trainer with dual brakes; aux power plug; stanby vac; more durable interior. 14V electrical. Four place. 1 $119,900
1989 M2OL PFM 26-0041 Porsche PFM 3200 N03 (217 HP). Last ad for PFM ran in March, 1990. Extra long body. 1 $193,375
1989 M20M TLS 27-0001to 27-0035 Lycoming Tl0-540-AFIA (270 HP). 26'4" body, rear seats 4" aft (extra long body introduced in PFM mode). 35 $177,500
1990 M20J 201AT 24-1687 to 24-1706 Lycoming I0-360-A3B6D(200 HP). Advanced trainer, unchanged from 1989. Four place. 20 $119,900A
1990 M20J 201 24-3144 to 24-3207 Lycoming I0-360-A3B6D(200 HP). Sold as MSE. New paint design. Four place. 64 $138,000A
1990 M20K 252 25-1221 to 25-1230 Continental TSI0-360-MB(1) (210 HP). Unchanged from 1989. Four place. 10 $203,165A
1990 M20L PFM 26-0042 Porsche PFM 3200N03 (217 HP). Extra long body. Four place. 1 $
1990 M20M TLS 27-0036 to 27-0084 LycomingTI0-540-AFIA (270 HP). Extra long body. Mid-year paint change. Four place. 49 $251,650A
1991 M20J 201 24-3208 to 24-3245 Lycoming I0-360-A3B6D(200 HP). Sold as MSE and MSE Limited. Four place. 38 $173,460A
1991 M20M TLS 27-0085 to27-0125 Lycoming Tl0-540-AFIA (270 HP). Paint scheme adds 1 extra pinstripe. Extra long body. Four place. 41 $261,720A
1992 M20J MSE 24-3246 to 24-3286 Lycoming IO-360-A3B6D (200 HP). MSE, MSE Limited and AT (Advanced Trainer). 41 $185,000A
1992 M20M TLS 27-0126 to 27-00146 Lycoming TIO-540-AFIA (270 HP). Unchanged from 1991. Extra long cabin 21 $302,090A
1993 M20J MSE 24-3287 to 24-3320 Lycoming IO-360-A3B6D (200 HP). Unchanged from 1992, though AT model disappears. 34 $196,750A
1993 M20M TLS 27-0147 to 27-0173 Lycoming TIO-540-AFIA (270 HP). Same as 1992. Extra long cabin. 27 $241,000 - $334,420
1994 M20J MSE 24-3321 to 24-3354 Lycoming IO-360-A3B6D (200 HP). Same as 1993. 34 $208,915A
1994 M20M TLS 27-0174 to 27-0193 Lycoming TIO540-AFIA (opt. AFIB) -- (270 HP). Unchanged from 1993. 19 $340,345A
1994 M20R Ovation 29-0001 to 29-0021 TCM IO-550-G (280 HP). Normally aspirated with large 6-cylinder engine. Flying Magazine's single-engine plane of the year for 1994. Extra long body. 21 $205,750
1995 M20J MSE 24-3355 to 24-3373 Lycoming IO-360-A3B6D (200 HP). Unchanged from 1994. 19 $211,295
1995 M20M TLS 27-0194 to 27-0208 Lycoming TIO-540-AFIA (opt. AFIB) -- (270 HP). Unchanged from 1994. Extra long body. 15 $297,970A
1995 M20R Ovation 29-0022 to 29-0075 TCM IO-550-G (280 HP). Unchanged from 1994. Extra long body. A photo of Norm Clemmer's N995K flaring and his factory panel. 54 $297,970A
1996 M20J MSE 24-3374 to 24-3393 Lycoming IO-360-A3B6D (200 HP). Unchanged from 1995. 20 $245,705A
1996 M20M TLS 27-0209 to 27-0220 Lycoming TIO-540-AFIB (AFIA for s/n 209, 210). TKS option available. TLS Bravo added. Extra long body. 12 $395,155A
1996 M20R Ovation 29-0076 to 29-0095 TCM IO-550-G (280 HP). TKS also becomes available. Extra long body. 20 $332,915A
1997 M20K 252 25-2001 to 25-2008 TCM TIO-360MB1 (210 HP). Reintroduces 252 with improved engine, 230 pound gross weight increase. 8 $381,900A
1997 M20K Encore 25-2000 and 25-2009 to 25-2017 TCM TIO-360-SB2 (220 HP). Encore model re-introduces 252 10HP+ in engine, 230 pound gross weight increase. 9 $391,900A
1997 M20M Bravo TLS 27-0221 to 27-0240 Lycoming TIO-540-AFIB (270 HP). Unchanged from 1996. Extra long body. Ron Gilbert's N355RZ exterior, with TKS de-icing. 20 $446,900A
1997 M20R Ovation 29-0096 to 29-0131 TCM IO-550-G (280 HP). Unchanged from 1996. Extra long body. 36 $368,900A
1997 M20J MSE 24-3394 to 24-3412 Lycoming IO-360-A3B6 (200 HP). Unchanged from 1996. 19 $276,550A
1998 M20J Allegro 24-3413 to 24-3431 Lycoming IO-360-A3B6 (200 HP). Renamed J model; last year of production for J body. 19 $286,500A
1998 M20R Ovation 29-0132 to 29-0172 TCM IO-550-G (280 HP). Long body (standard after 1998). 41 $378,900A
1998 M20K Encore 25-2018 to 25-2035 TCM TIO-360-SB2 (220 HP). Uses same body as J model -- both discontinued at year-end. 18 $386,900A
1998 M20M TLS Bravo 27-0240 to 27-0257 Lycoming TIO-540-AFIB (270 HP). Long body. 17 $364,950 - $436,700
1999 M20R Ovation 29-0173 to 29-0199 TCM IO-550-G (280 HP). Long body. 27 $384,000
1999 M20M TLS Bravo 27-0258 to 27-0281 Lycoming TIO-540-AFIB (270 HP). Long body. 25 $439,000
1999 M20S Eagle 30-0001 to 30-0039 TCM-IO-550-G (244 HP). Moritz gauges; 2-axis STEC autopilot; 75 gal. tanks. Long body. 39 $319,000
2000 M20R Ovation2 29-0200 to 29-0269, excluding 29-0260 and 29-0268 TCM IO-550-G (280 HP). 2-blade McCauley and 190-knot cruise. Dual Garmin 430s, KFC-225 autopilot, leather interior. Long body. 55 $399,000 - $498,400
2000 M20M TLS Bravo 27-0282 to 27-0310, excluding 27-0304 Lycoming TIO-540-AFIB (270 HP). Dual Garmin 430s; KFC-225 autopilot, leather interior. Long body. 26 $459,000 - $530,800
2000 M20S Eagle 30-0040 to 30-0055 + 30-0057 TCM-IO-550-G (244 HP). Moritz gauges; 2-axis STEC autopilot; 75 gal. tanks. Long body. 19 $299,000 - $437,700
2001 M20R Ovation 2 29-0260, -0268 and 29-0270 to 29-0279 TCM IO-550-G (280 HP). 2-blade McCauley and 190-knot cruise. Dual Garmin (530/430) nav/com/GPS, KFC-225 autopilot, leather interior. Long body. 12 $445,000B
2001 M20M TLS Bravo 27-0304, 27-0311 to 27-0316 Lycoming TIO-540-AFIB (270 HP). Dual Garmin (530/430) nav/com/GPS, KFC-225 autopilot, leather interior. Long body. 7 $505,000B
2001 M20S Eagle 2 30-0056, 30-0058 to 30-0062 Upgrades in 2001 include 3-bladed prop (and 100 lb. gross weight increase); single Garmin GNS430 GPS/Nav/Com; leather interior; rudder trim, ground power plug. Still uses TCM-IO-550-G (244 HP). 6 $360,000B

Mooney Aircraft Corporation's entering Chapter 11 on July 27, 2001 halted production of aircraft that year at 29. The company remained in bankruptcy proceedings until 2004, but AASI purchased the company in April 2002, then renamed itself Mooney Aerospace.

Production resumed during 2004 of the Ovation 2 DX and the high performance Bravo DX models. In late 2004 GX models of both the Ovation 2 and Bravo were type-approved became the first glass cockpit Mooney models, using the Garmin GX1000 integrated avionics. These were first delivered in 2005.

Year Model Serial # Description No. built Factory price
2002 Ovation 2 29-0280 to 29-0287 TCM IO-550-G (280 HP). 2-blade McCauley and 190-knot cruise. Dual Garmin (530/430) nav/com/GPS, KFC-225 autopilot, leather interior. 8 $349,500 to $445,000 (mid-year price reduction)
2002 Eagle 2 30-0064 and 30-0065 TCM-IO-550-G (244 HP) with McCauley 3-blade prop. 2 $360,000 to $299,950
2003 Ovation 2 29-0288 to 29-0315 TCM IO-550-G (280 HP). 2-blade McCauley and 190-knot cruise. Dual Garmin (530/430) nav/com/GPS, KFC-225 autopilot, leather interior. 28 $299,450
$384,950 (DX)
2003 TLS Bravo 27-0317 to 27-0323 Lycoming TIO-540-AFIB (270 HP). Dual Garmin (530/430) nav/com/GPS, KFC-225 autopilot, leather interior. 7 $434,950
2003 Eagle 2 30-0063 TCM-IO-550-G (244 HP) with McCauley 3-blade prop. 1  
2004 Ovation 2 29-0316 to 29-0321, 29-0323 to 29-0332, 29-0334 to 29-0335, 29-0337 to 29-0339, 29-0342, 29-0344 to 29-0346, 29-0348, 29-0352 to 29-0353 TCM IO-550-G (280 HP). 2-blade McCauley and 190-knot cruise. Dual Garmin (530/430) nav/com/GPS, KFC-225 autopilot, leather interior. 28 $319,950
$389,950 (DX)
$409,950 (GX)
2004 TLS Bravo 27-0323 to 27-0330 Lycoming TIO-540-AFIB (270 HP). Dual Garmin (530/430) nav/com/GPS, KFC-225 autopilot, leather interior. 8 $439,950 (DX)
$459,950 (GX)
2005 Ovation 2 DX   TCM IO-550-G (280 HP). McCauley 2-blade prop. 1 $397,750
2005 Ovation 2 GX 29-0354 to 29-0407 TCM IO-550-G (280 HP) with Garmin GX1000 glass cockpit. Hartzell 3-blade prop. 64 $438,000
2005 Bravo GX 27-0331 to 27-0350 Lycoming TIO-540-AFIB (270 HP) with Garmin GX1000 glass cockpit. McCauley 3-blade prop. 20 $478,000
2006 Ovation 2 GX   Ovation 2 becomes the 11,000th Mooney shipped by the factory in February, 2006. Mooney hit the 10,000 level in 1995.   $438,000

2007 ACCLAIM Mooney's fastest ever and the fastest in its class! Well equipped $650K

Top Speed - 25,000 ft. 237 ktas
Rate of Climb (sea level, max. wt.) – fpm 1,240
Long Range – Std. Fuel (with res.) – nm 1,445
Long Range – Optional Tanks (with res.) – nm 1,840
Max. Operating Altitude – feet 25,000
Take-off Run (max. wt.) 960'
Engine TCM TSI0-550-G Turbo-normalized Twin turbo Dual intercoolers
Horsepower 280 BHP
TBO 2,000 hours
Propeller Hartzell Three-Blade
Fuel Capacity – Standard (usable) 100 USG
Fuel Capacity With Optional Tanks (usable) 128 USG
Max. Gross Weight - lb. 3,368
Approx. Useful Load – lb 1,000

 

Footnotes:

A: average retail price, including popular options
B: base price

Special thanks to:
* Mooney Airplane Co. and Roger Munt for confirming recent shipment numbers
* Shipments for 2005 taken from
GAMA data.
* Richard Zephro, Coast to Coast Aircraft Sales, for assistance with historical pricing, www.mooneyland.com
* Keith Vasey, Pacific-Mooney and salesmen par excellence, for confirming 1999 production.
* Larry Ball, author of
Those Remarkable Mooneys, for adding valuable model-by-model detail. Selected information reprinted by permission of Ball Publications.

Model List per Mooney Aircraft Corporation

 

Recent query:  (answers to Bruce's questions in dark caps)

Rich,
Let me first start out by telling you that since I started flying 1968, I have, at most, two hours in a Mooney of any vintage. I probably don't even have a hangar-flyer's knowledge of the ins and outs of the Mooney product line. The retract time I have as pilot in command is about 25 hours, 20 in Cherokee Arrows, and the balance in Bellanca Vikings and a Bonanza. I've ridden in a Ranger. I found it to be a delight to fly, but no faster than a 180hp Arrow. I had heard that the rigging on 68-69 Rangers was spotty from the factory, so I could attribute the lower than advertised cruise speeds.

So, with that in mind, the questions I have for you are:

Is an older Ranger capable of cruising near it's advertised cruise speed?

DIFFERING SPEEDS ARE ADVERTISED. REAL WORLD CRUISE SPEED ON AVERAGE IS 147 KTS AT 75% POWER AND ABOUT 9GPH DEPENDING ON ALTITUDE

Do they respond well to mods?

TOUGHIE! SOME DO, SOME DON’T! MODS CERTAINLY ADD TO THE LOOKS AND MODERNIZING BUT I TELL THOSE WHO WANT TO MOD THEIR BIRDS, DO IT FOR ESTHETICS AND IF YOU GET SPEED INCREASES, ALL THE BETTER. ALL MOONEYS ARE HAND MADE AND SEEM TO RESPOND DIFFERENTLY. I SOLD ONE OF SOUTHWEST TEXAS AVIATION’S C MODEL DEMONSTRATORS SOME YEARS BACK AND IT HAD ALL THE MODS. I THINK WE GOT ABOUT 155 KTS OUT OF HER, ABOUT LIKE THE STOCK E MODEL. ON THE OTHER HAND, I JUST SOLD A MODIFIED E THAT ZOOMED AT 165 KTS FROM THE 155 KTS NORMAL. ON THE OTHER HAND, MY FIRST MOONEY WAS A STOCK ‘65E AND IT KEPT UP WITH SWTA’S MODIFIED E THEY HAD AT THE TIME, SO GO FIGURE. MEANWHILE, YOU DON’T WANT AN EARLIER MOONEY THAN 1965. TOO MANY IMPROVEMENTS MADE BY THEN AND PRICES AREN’T THAT MUCH HIGHER FOR ’65 AND NEWER. STAY AWAY FROM 1961 IN ANY CASE, THE B MODEL. TEST PILOT HAD TO BAIL OUT DUE TO UNRECOVERABLE FLAT SPIN. THAT WAS THE ONLY YEAR OF THE REAR CG PROBLEM.


What company's mods do you recommend?

MOONEYLAND! Duh! :o)  (Check out our “ride pimping section”).


Can a 54 year old guy who's flying experience is mostly C-172s and Piper Archers fly a Ranger safely? Or am I too old?

HELL YES! I’M 59 SONNY! DON’T LET YOURSELF GET OR FEEL OLD NO MATTER WHAT! OUR GENERATION IS NOT GOING OUT QUIETLY AND THAT’S A FACT! HEY, WE STARTED ROCK AND ROLL, MICKEY MOUSE CLUB, MUSCLE CARS, MODERN PLANES, JET AIRLINERS, FLOWER CHILDREN, THE PILL, PROTESTING, BIMBO’S AND HOOLA-HOOPS FOR HEAVEN’S SAKE! Get rid of that “am I too old” attitude!


Thanks, Rich. Love the website!

Best regards,

Bruce S

YOU’RE WELCOME. I may put your questions on my website, but I’ll keep your last name private) Good questions!

RICH

 

Al Mooney and His Wonderful Flying Machines

Mooneyland highly recommends Tom "TJ" Johnson for any and all AVIATION INSURANCE NEEDS.

www.airpowerinsurance.com *** www.warbirdinsurance.com

Or call Tom Johnson "TJ" direct at: 602 628-2701. Tell TJ to give you the great and personal service he has given so many of our Mooneyland customers. zef said so! CLICK HERE for more information and testimony about TJ.

 

You need THIS and THIS and THIS

Mooney Aircraft Trio of   Information

    

 $155.94 for the Complete Set

 

Thanks! zef

Hey now, who's got your back? MOONEYLAND! You know dats right!

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email- mooneyland@gvtc.com

Office (830) 899-2600

Cell     (210) 685-3793

 

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Last modified: February 02, 2011