Introduced in 
                                    1994, the M20R Ovation was partly a response 
                                    by Mooney Aircraft Corp. to the after-market 
                                    modifiers that were putting bigger and 
                                    bigger engines in the M20 airframe.  By 
                                    ’94, Mooney buyers were used to the “big 
                                    engine” philosophy of the engineers in 
                                    Kerrville.  With the introduction of 
                                    the Lycoming powered, M20M TLSBravo in 1989, 
                                    Mooney had changed from seeking performance 
                                    gains by tweaking the aerodynamics of the 
                                    airframe to going faster with bigger and 
                                    bigger engines.  However, efficiency 
                                    was still important to the airplane maker, 
                                    so when they looked for another normally 
                                    aspirated piston engine, the IO-550 from 
                                    Teledyne Continental Motors seemed like the 
                                    solution. 
                                    
                                    
                                    With the longer 
                                    fuselage of the M20L and M20M available, the 
                                    big block Continental was a logical fit.  
                                    This was an improvement on what was 
                                    available on the after-market as the longer 
                                    airplane had better stability 
                                    characteristics and CG with this engine 
                                    installation as compared to the shorter body 
                                    models.  The Ovation was the first of 
                                    the “theatrically” named Mooneys, and was 
                                    followed by the “wet-head” modification of 
                                    the TLS getting the Bravo name and the 
                                    remake of the M20K – 252 being called the 
                                    Encore.  However, it’s the Ovation that 
                                    is the subject of this report. 
                                    
                                    
                                    Clearly the 
                                    most popular model since it’s introduction, 
                                    the Ovation, and it’s follow-on version the 
                                    Ovation2 (sometimes referred to as the O2) 
                                    easily outsold the other production models 
                                    almost 2 to 1.  Production during 1994 
                                    was limited to 21 airplanes, and the Ovation 
                                    was chosen by Flying 
                                    Magazine as the “Single-engine 
                                    Plane of the Year”.  By 1995, the 
                                    M20R production increased to 46 airplanes as 
                                    more Mooney pilots discovered the 
                                    smooth-running high performance Continental.  
                                    With advertised true airspeeds in the 
                                    mid-180s, the Ovation was seldom passed by 
                                    any single engine, piston aircraft not also 
                                    built by Mooney.   Production 
                                    slipped slightly in 1996 (as did all the 
                                    Mooney models) to only 33 aircraft, however 
                                    with the introduction of the optional TKS 
                                    anti-ice, de-icing system, the Ovation 
                                    became the first normally aspirated single 
                                    engine airplane to win “Flight In Know 
                                    Icing” certification from the FAA.  
                                    This honor followed the turbocharged M20M 
                                    certification the previous year. 
                                    
                                    
                                    In 1997, Mooney 
                                    production of the M20R increased to 34 which 
                                    was pretty amazing considering that during 
                                    that year Mooney also produced the M20J MSE 
                                    (19), the M20K Encore (8), and the M20M TLS 
                                    Bravo (20).  Production of the Ovation 
                                    continued to increase in 1998 with 41 ships 
                                    leaving the Texas Hill Country for all parts 
                                    of the world.  In 1999, Mooney decided 
                                    to build one common airframe and dropped the 
                                    M20J from the production list (much to the 
                                    dismay of most Mooney lovers) and introduced 
                                    in its place the M20S – Eagle.  This 
                                    caused a slight drop in R production as only 
                                    34 aircraft rolled from the plant in ’99.  
                                    The introduction of the Eagle in 1999 caused 
                                    the engineers to re-think the M20R and as a 
                                    result, the Ovation2 was introduced in 2000 
                                    with a 2-blade McCauley propeller specially 
                                    designed for Mooney, which increased the 
                                    book true airspeed to 190 knots.  The 
                                    bullet just got faster!  2000 saw 55 
                                    O2s enter the FAA registry as everyone 
                                    recognized the balance of airspeed and fuel 
                                    efficiency that the M20R possessed.  In 
                                    2001, the last year of the Mooney Aircraft 
                                    Corporation, 15 Ovation2s were completed 
                                    before the factory shut-down during the 
                                    summer as the company entered Chapter 11 
                                    Bankruptcy protection and sought financial 
                                    help.  This put the total M20R 
                                    production at 279 aircraft for it’s first 8 
                                    years.  During this same time, 144 M20M 
                                    and 111 M20J (followed by 62 M20S) aircraft 
                                    were built.  It is easy to see that the 
                                    Ovation has been the crowd favourite.  
                                    Let’s see why.
                                    
                                    
                                    In late 
                                    September, I was fortunate enough to have 
                                    the opportunity to spend several days in a 
                                    brand new, 2002 Ovation2.  The 
                                    aircraft, N1051K S/N 29-0285, was the sixth 
                                    2002 M20R produced and the second aircraft 
                                    delivery for the new Mooney Airplane 
                                    Company.  My luck got better when I was 
                                    asked to deliver the airplane from the 
                                    factory in Kerrville to it’s new home and 
                                    owner in Arizona. 
                                    
                                    
                                    The lucky new 
                                    owner, Marc Danna, had recently sold his 
                                    M20E and was stepping up in size and 
                                    performance with the Ovation.  Since I 
                                    was also staying in Tucson for a few days to 
                                    fly with Marc, I got to see the airplane in 
                                    a variety of flight situations. 
                                    
                                    
                                    But let’s start 
                                    at the beginning.  The first thing I 
                                    notice when I approach the new “Ultra-Long 
                                    Body” Mooneys is how beautiful they really 
                                    are.  The long sleek nose is nicely 
                                    balanced by the long tapering tailcone 
                                    ending in the classic Mooney tail.  The 
                                    airplane sits with about a + 4 ½ degree 
                                    pitch attitude (more on that later) and 
                                    looks ready to leap in the air just sitting 
                                    on the ramp.  The preflight is 
                                    straightforward and common to every other 
                                    Mooney.  However, just like in all 
                                    Mooneys, I recommend sumping the wing tanks 
                                    before beginning any other preflight 
                                    actions.  This removes any chance of 
                                    introducing water into the fuel system when 
                                    the Gascolator is drained during the cockpit 
                                    check.  Also, this is the time to check 
                                    the standard “in-wing” fuel quantity gauges.  
                                      
                                    
                                    
                                    These 
                                    mechanical (no electrical power needed) 
                                    gauges show fuel quantity measurable between 
                                    10 and 30 gallons of useable in the 
                                    respective tank.  Because of the pitch 
                                    attitude on the ground, the cockpit fuel 
                                    quantity indicators do not read the correct 
                                    fuel values.  They will show a higher 
                                    quantity than actually exists.  They 
                                    are calibrated to be accurate during flight 
                                    when the pitch attitude is level.  The 
                                    wing gauges are calibrated to be accurate 
                                    when the aircraft is on the ground, however 
                                    when the Ovation is in flight, these no 
                                    longer read true fuel quantity.  The 
                                    fuel quantity indicators are supplemented by 
                                    red “LEFT FUEL” and “RIGHT FUEL” low level 
                                    warning lights in the annunciator panel that 
                                    will illuminate when approximately 6 to 8 
                                    gallons of useable fuel remains in the 
                                    indicated tank. 
                                    
                                    
                                    Once the wings 
                                    are drained, we can begin in the cockpit 
                                    making sure all the switches are in the 
                                    correct place.  One thing I try to 
                                    teach pilots is to use a checklist during 
                                    shutdown.  If you do this, then all the 
                                    switches are already placed correctly when 
                                    the next flight occurs, and the checks then 
                                    are simple.  If the airplane has been 
                                    flown by someone else, or has just come out 
                                    of maintenance, then certainly, use the 
                                    checklist to make sure that the cockpit is 
                                    set-up properly.  Once set-up, the 
                                    checks prior to each flight can be done in a 
                                    “flow” or logical order and are quite easy.
                                    
                                      
                                      
                                        
                                          | 
                                           
                                          
                                          
                                            
                                          
                                          Moritz 
                                          engine gauges.  | 
                                          
                                           
                                          
                                          
                                            
                                          
                                          Ovation 
                                          cooling air inlets  | 
                                        
                                      
                                      
                                     
                                    
                                    
                                    
                                    
                                    
                                    
                                    Ovation instrument panel
                                    
                                    
                                    Like all the 
                                    other current production Mooneys, the M20R 
                                    has two batteries in the tailcone.  So, 
                                    after checking them both for voltage level, 
                                    you should use the one with the highest 
                                    potential.  If they are the same, use 
                                    the one not used during the last flight.  
                                    The battery that is not selected is kept 
                                    charged through a “trickle-charge” system, 
                                    so that it is fully charged and ready should 
                                    it be needed.  Speaking of the 
                                    electrical system on the Ovation, once the 
                                    engine has been started, the aircraft’s 
                                    electrical needs are supplied by a huge 
                                    100-ampere, 28-volt DC engine-driven 
                                    alternator. 
                                    
                                    
                                    After 
                                    completing the preflight walkaround 
                                    inspection, it’s time to climb in, strap in 
                                    and get the big Continental cooking.  
                                    Engine start is very straightforward if you 
                                    remember one thing.  Fuel…lots of fuel 
                                    is needed to start the 550 when the OAT is 
                                    low.  When it is cold (like below 
                                    40-degrees F) I use the “High Boost Pump” to 
                                    prime for start fuel.  I think it’s 
                                    almost impossible to flood this Continental 
                                    when it is cold outside.  This is one 
                                    place that I disagree with the Mooney 
                                    checklist during cold weather starts.  
                                    The “Low Boost Pump” doesn’t seem to get 
                                    things done and the starts take longer.  
                                    However, since this airplane had been flown 
                                    prior to my departure from Kerrville, I used 
                                    the “Hot Start Procedure” of: 
                                    
                                    
                                    1.     
                                    
                                    Throttle – Full 
                                    Open
                                    
                                    
                                    2.     
                                    
                                    Mixture – Idle 
                                    Cut Off
                                    
                                    
                                    3.     
                                    
                                    Boost Pump - 
                                    High for 5 seconds or Low for 15 seconds
                                    
                                    
                                    4.     
                                    
                                    Throttle – Idle 
                                    (then two half-turns in for the proper idle 
                                    RPM of 800 – 1000)
                                    
                                    
                                    5.     
                                    
                                    Mixture – Full 
                                    Forward
                                    
                                    
                                    6.     
                                    
                                    Starter Switch 
                                    – Turn and Push 
                                    
                                    
                                    This works 
                                    every time for me, so soon the IO-550-G6 was 
                                    making a throaty rumble beneath the long 
                                    sleek cowling.  And the Ovation cowling 
                                    is a true thing of beauty and a design 
                                    marvel.  By paying close attention to 
                                    airflow dynamics, the Mooney engineers have 
                                    designed a cowling for the M20R that doesn’t 
                                    need cowl flaps to aid engine cooling in 
                                    flight.  It has small; oval openings 
                                    behind the propeller that ram the cooling 
                                    air into the upper deck of the engine bay.  
                                    Then, through the use of carefully designed 
                                    baffles, the airflow is directed downward 
                                    across the cylinder cooling fins and then is 
                                    drawn out through two aerodynamically 
                                    designed “blisters” around each exhaust 
                                    pipe.  These blisters create an airflow 
                                    pattern and a “low pressure area” that draws 
                                    the cooling air through the engine bay from 
                                    the top down and out through the bottom of 
                                    the cowling and eliminate the need for cowl 
                                    flaps with their resultant drag.  This 
                                    works quite well during most segments of 
                                    flight, but a word of caution here.  
                                    During hot weather operations, with extended 
                                    ground time, the small openings in the front 
                                    don’t seem to draw enough cooling air into 
                                    the engine bay.  Oil temperatures (the 
                                    same air used to cool the cylinders is used 
                                    to cool the oil in the oil cooler) can 
                                    approach the Red Line, especially if the 
                                    airplane isn’t positioned facing into the 
                                    wind.  In the summer, I work hard to 
                                    reduce the amount of ground time to try to 
                                    control this.
                                    
                                      
                                      
                                        
                                          | 
                                           
                                          
                                          
                                            
                                          
                                          LCD 
                                          instruments.  | 
                                          
                                           
                                          
                                          
                                            
                                          
                                          Garmin GS  | 
                                        
                                      
                                      
                                     
                                    
                                    
                                    Now that the 
                                    engine is running, I can turn-on the Radio 
                                    Master Switch (used to control all the 
                                    avionics) and get my GPS flight plan loaded 
                                    into the Garmin GNS-530 GPS Navigator.  
                                    The panel in N1051K is representative of the 
                                    standard that is today’s high performance 
                                    general aviation “all weather” airplane.  
                                    Central in the avionics suite is a pair of 
                                    Garmins – a GNS-530 sits atop a GNS-430.  
                                    These two radios each feature an IFR Enroute 
                                    and Approach certified Global Positioning 
                                    System Navigator, a VHF communications radio 
                                    and a VOR receiver with Glide Slope.  
                                    Add to this the Bendix King KFC-225 2-axis 
                                    Digital Flight Director Autopilot, a Garmin 
                                    GTX-327 Transponder and GMA-340 Audio Panel 
                                    and we have a very capable IFR traveling 
                                    machine.  N1051K also has the optional 
                                    Wx-500 Stormscope® and the Goodrich Skywatch® 
                                    which both display on the 530 and the 430.  
                                    The other notable options consist of a JPI 
                                    EDM700 Engine Monitoring System, and (very 
                                    important in the hot southwest) Factory Air 
                                    Conditioning. 
                                    
                                    
                                    With the 
                                    KCS-55A Slaved HSI system, polished spinner 
                                    and speed brakes as standard equipment, the 
                                    2002 Ovation2 is a functional and good 
                                    looking cross-country performer.  And I 
                                    get to try it out. 
                                    
                                    
                                    Now that the 
                                    big-bore Continental is running, let’s talk 
                                    a little about this new engine.  The 
                                    IO-550-G6 installation in the Ovation is 
                                    unlike other 550 Continental engines 
                                    installed in other airframes.  In ’94 
                                    Mooney was the first OEM (Original Equipment 
                                    Manufacturer – another name for aircraft 
                                    manufacturer) to use the all-new “balanced 
                                    induction, crossflow head” IO-550 engine.  
                                    Until Mooney, all production aircraft use of 
                                    the 550 was the “straight-pipe” version and 
                                    the tuned induction engine was only in a 
                                    handful of home-built airplanes.  
                                    Mooney also introduced the “soft isolator 
                                    bedmount” system on the Ovation with tuned 
                                    engine isolators.  All this makes for a 
                                    smooth, quiet cockpit even during high power 
                                    operations, and a very efficient engine. 
                                    
                                    
                                    A little 
                                    information about N1051K is necessary.  
                                    With an empty weight of 2397 pounds, 51K had 
                                    a useful load of 971 pounds to bring it to 
                                    the maximum takeoff weight of 3368 pounds.  
                                    This means that 2 FAA Standard 170-pound 
                                    individuals and full fuel (89 gallons 
                                    useable) would leave room for 113 pounds of 
                                    baggage (maximum baggage capacity is 120 
                                    pounds).  However, it is very seldom 
                                    that a pilot will need or want all 89 
                                    gallons of avgas.  With an average fuel 
                                    burn of 14 GPH (at 65% power), 89 gallons 
                                    would give over six hours of endurance.  
                                    This is much more than most pilots will 
                                    want, so something less than full fuel would 
                                    yield an increase in payload.  Drop the 
                                    fuel quantity to 60 gallons (4.2 hours @ 
                                    65%) and you still have a range in no wind 
                                    of over 550 NM with an hour and 12 minutes 
                                    reserve.  With this fuel load, 51K 
                                    could carry 622 pound of people and bags.  
                                    That’s 3, 175-pounders and 50 pounds of 
                                    bags.  Or, Mom and Dad (at 175 and 130) 
                                    plus kid #1 (at 75 pounds) and kid #2 (at 75 
                                    pounds) and still have 120 pounds available 
                                    for baggage.  The Ovation, even 
                                    equipped with air conditioning, can carry a 
                                    wide variety of loading possibilities. 
                                    
                                    
                                    Today, my 
                                    takeoff weight is 123 pounds below maximum, 
                                    so with the conditions at Kerrville 
                                    (temperature 18-degrees C, DA 2500’, no 
                                    wind) – my takeoff distance will be 3200’ 
                                    using under 2000’ of runway for ground 
                                    roll. 
                                    
                                    
                                    With my GPS 
                                    route stored in the Garmin, and a clearance 
                                    from Houston Centre, after a normal run-up 
                                    I’m ready to see what this bird will do.  
                                    Power is smoothly applied until I have full 
                                    throttle and away we go.  Now most 
                                    folks who have flown the original Ovation 
                                    will notice that the O2 doesn’t accelerate 
                                    quite as crisply as its older brother with 
                                    the extra propeller blade.  This is the 
                                    result of the two blades and a low pitch 
                                    stop mandated by a disputed FAA rule 
                                    interpretation during certification.  
                                    It’s funny how much static thrust one 
                                    additional propeller blade adds, however 
                                    this may be more a tactile perception and 
                                    not really true as the takeoff distance 
                                    numbers for the two models are very close. 
                                    
                                    
                                    Back-pressure 
                                    on the control wheel at 65 KIAS and up we 
                                    go.  After confirming a positive rate 
                                    of climb, the wheels come up followed 
                                    closely by the 10-degrees of takeoff flaps.  
                                    With climb power of full throttle and 2500 
                                    RPM set, the VSI settles on 1200 FPM at VY 
                                    of 105 KIAS.  Since 51K has only 8 
                                    hours on it’s hobbs meter and is still in 
                                    ring seating, I reduce the pitch for a more 
                                    “engine cooling friendly” 120 KIAS which is 
                                    cruise climb airspeed.  This results in 
                                    a VSI reading of 1000 FPM as we are quickly 
                                    through 4000 feet enroute to our 8000-foot 
                                    clearance limit.  The following table 
                                    shows the climb rate information for this 
                                    short climb to cruise altitude.  On a 
                                    subsequent flight, I made an unrestricted 
                                    climb from a 1000’ takeoff altitude to 
                                    11,000 feet and that table is also 
                                    included. 
                                    
                                      
                                      
                                        
                                          | 
                                           
                                          
                                          Altitude  | 
                                          
                                           
                                          
                                          IOAT  | 
                                          
                                           
                                          
                                          MP/RPM  | 
                                          
                                           
                                          
                                          Fuel Flow  | 
                                          
                                           
                                          
                                          IAS  | 
                                          
                                           
                                          
                                          ROC  | 
                                        
                                        
                                          | 
                                           
                                          
                                          2000  | 
                                          
                                           
                                          
                                          18 C  | 
                                          
                                           
                                          
                                          FT/2500  | 
                                          
                                           
                                          
                                          23.4  | 
                                          
                                           
                                          
                                          105  | 
                                          
                                           
                                          
                                          1200  | 
                                        
                                        
                                          | 
                                           
                                          
                                          3000  | 
                                          
                                           
                                          
                                          17 C  | 
                                          
                                           
                                          
                                          FT/2500  | 
                                          
                                           
                                          
                                          23.1  | 
                                          
                                           
                                          
                                          120  | 
                                          
                                           
                                          
                                          1000  | 
                                        
                                        
                                          | 
                                           
                                          
                                          4000  | 
                                          
                                           
                                          
                                          15 C  | 
                                          
                                           
                                          
                                          FT/2500  | 
                                          
                                           
                                          
                                          23.1  | 
                                          
                                           
                                          
                                          120  | 
                                          
                                           
                                          
                                          1000  | 
                                        
                                        
                                          | 
                                           
                                          
                                          5000  | 
                                          
                                           
                                          
                                          12 C  | 
                                          
                                           
                                          
                                          FT/2500  | 
                                          
                                           
                                          
                                          23.0  | 
                                          
                                           
                                          
                                          120  | 
                                          
                                           
                                          
                                          985  | 
                                        
                                        
                                          | 
                                           
                                          
                                          6000  | 
                                          
                                           
                                          
                                          11 C  | 
                                          
                                           
                                          
                                          24.2/2500  | 
                                          
                                           
                                          
                                          23.0  | 
                                          
                                           
                                          
                                          120  | 
                                          
                                           
                                          
                                          960  | 
                                        
                                        
                                          | 
                                           
                                          
                                          7000  | 
                                          
                                           
                                          
                                          8 C  | 
                                          
                                           
                                          
                                          23.4/2500  | 
                                          
                                           
                                          
                                          22.6  | 
                                          
                                           
                                          
                                          120  | 
                                          
                                           
                                          
                                          850  | 
                                        
                                      
                                      
                                     
                                    
                                    
                                    Another flight, 
                                    takeoff weight 3358: 
                                    
                                      
                                        | 
                                         
                                        
                                        Altitude  | 
                                        
                                         
                                        
                                        IOAT  | 
                                        
                                         
                                        
                                        MP/RPM  | 
                                        
                                         
                                        
                                        Fuel Flow  | 
                                        
                                         
                                        
                                        IAS  | 
                                        
                                         
                                        
                                        ROC  | 
                                      
                                      
                                        | 
                                         
                                        
                                        1000  | 
                                        
                                         
                                        
                                        20 C  | 
                                        
                                         
                                        
                                        FT/2500  | 
                                        
                                         
                                        
                                        24.6  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        1050  | 
                                      
                                      
                                        | 
                                         
                                        
                                        2000  | 
                                        
                                         
                                        
                                        19 C  | 
                                        
                                         
                                        
                                        FT/2500  | 
                                        
                                         
                                        
                                        24.3  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        1000  | 
                                      
                                      
                                        | 
                                         
                                        
                                        3000  | 
                                        
                                         
                                        
                                        16 C  | 
                                        
                                         
                                        
                                        FT/2500  | 
                                        
                                         
                                        
                                        24.3  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        1000  | 
                                      
                                      
                                        | 
                                         
                                        
                                        4000  | 
                                        
                                         
                                        
                                        14 C  | 
                                        
                                         
                                        
                                        FT/2500  | 
                                        
                                         
                                        
                                        24.1  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        975  | 
                                      
                                      
                                        | 
                                         
                                        
                                        5000  | 
                                        
                                         
                                        
                                        12 C  | 
                                        
                                         
                                        
                                        FT/2500  | 
                                        
                                         
                                        
                                        23.5  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        950  | 
                                      
                                      
                                        | 
                                         
                                        
                                        6000  | 
                                        
                                         
                                        
                                        11 C  | 
                                        
                                         
                                        
                                        FT/2500  | 
                                        
                                         
                                        
                                        23.1  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        950  | 
                                      
                                      
                                        | 
                                         
                                        
                                        7000  | 
                                        
                                         
                                        
                                        8 C  | 
                                        
                                         
                                        
                                        24.1/2500  | 
                                        
                                         
                                        
                                        23.0  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        920  | 
                                      
                                      
                                        | 
                                         
                                        
                                        8000  | 
                                        
                                         
                                        
                                        6 C  | 
                                        
                                         
                                        
                                        23.6/2500  | 
                                        
                                         
                                        
                                        22.8  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        890  | 
                                      
                                      
                                        | 
                                         
                                        
                                        9000  | 
                                        
                                         
                                        
                                        5 C  | 
                                        
                                         
                                        
                                        23.0/2500  | 
                                        
                                         
                                        
                                        22.1  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        860  | 
                                      
                                      
                                        | 
                                         
                                        
                                        10000  | 
                                        
                                         
                                        
                                        3 C  | 
                                        
                                         
                                        
                                        22.1/2500  | 
                                        
                                         
                                        
                                        21.6  | 
                                        
                                         
                                        
                                        120  | 
                                        
                                         
                                        
                                        780  | 
                                      
                                    
                                    
                                    
                                     The KFC-225 
                                    autopilot with altitude preselect, made a 
                                    smooth level-off at 8000 feet just as 
                                    Houston Center cleared me GPS direct to El 
                                    Paso (ELP), direct to destination – Tucson’s 
                                    Marana Northwest Regional.  This 
                                    resulted in almost a straight line 
                                    westbound. 
                                    
                                    
                                    Once level, I 
                                    referred to the Cruise Power Chart on the 
                                    Pilot’s sun visor and set full throttle (I 
                                    couldn’t quite get 75% which was my desire) 
                                    and 2400 RPM and figured that the big 
                                    Continental was producing about 72% power.  
                                    With a fuel flow (leaned to 50-degrees rich 
                                    of peak EGT) of 15.1 gallons of gas per 
                                    hour, and a GPS ground speed of 189 KTS, my 
                                    89 gallons of fuel would take me to the 
                                    destination 646 NM away and leave 31 gallons 
                                    or more than 2 hours of reserve. 
                                    
                                    
                                    Checking TAS 
                                    using the Garmin, we were clocking along at 
                                    187 KTAS, so the wind was not much of a 
                                    factor, being almost a dead crosswind 
                                    component of little velocity.  Since I 
                                    was dealing with a deadline (I hate using 
                                    the word “dead” in an airplane) on my 
                                    arrival in Arizona, a full-out test of the 
                                    airplane’s performance would have to wait 
                                    until the return trip to Kerrville some 4 
                                    days from now. 
                                    
                                    
                                    Instead I 
                                    settled back and enjoyed the flight west.  
                                    The autopilot, talking to the GPS through 
                                    the HSI, kept us moving steadily toward our 
                                    destination, and as the sun set, I was 
                                    wondering if it could possibly get any 
                                    better.  Soon, it was time to turn on 
                                    some cockpit lights, and here is another 
                                    area in which the newer Mooneys shine (no 
                                    pun intended!).  Cockpit lighting is 
                                    superb.  Flight instruments are 
                                    individually lighted and there are small 
                                    post lights for important switches not 
                                    backlit.  In addition, there are two 
                                    glareshield flood lights that can light the 
                                    entire panel from harsh bright (something 
                                    I’d use when in the vicinity of lightening 
                                    flashes) to a soft subtle glow.  I 
                                    don’t think it would be possible not to be 
                                    able to find a combination of instrument and 
                                    glareshield lights that wouldn’t please 
                                    everyone.  Just be careful of one 
                                    thing.  When the navigation lights are 
                                    turned on, the annunciator panel lights 
                                    automatically dim.  This is great at 
                                    night, but forget to turn them off again 
                                    during daylight and your heart rate will 
                                    increase when you can’t see the green “Gear 
                                    Down” light! 
                                    
                                    
                                    Because of MEA 
                                    requirements, ATC step-climbed me to 11,000 
                                    as we approached Tucson.  Still, the 
                                    Ovation clicked-off 178 knot TAS numbers 
                                    even though the power was down around 60%.  
                                    As we crossed the mountains east of Tucson, 
                                    still at 11, I could see the beacon at 
                                    Marana at 12 o’clock and only 30 NM ahead.  
                                    Time to start down and here’s where those 
                                    standard speed brakes really come in handy.  
                                    Power back to 20”/2500 RPM, roll the nose 
                                    down to peg the airspeed at the top of the 
                                    Green Arc (174 KIAS) and with the brakes 
                                    out, the VSI settles on 1000 FPM down.  
                                    This helps keep the engine temperatures 
                                    comfortably in the Green (I did watch the 
                                    JPI – it will show rate of cooling) and very 
                                    soon we were on the downwind.  As the 
                                    autopilot levels off, power continues back 
                                    to about 16" and at 140 the gear comes down.  
                                    With another slight reduction in power, we 
                                    are soon at 110 which is flap speed, and 
                                    once the gear and flaps (takeoff position) 
                                    are set, we can again reduce the power 
                                    slightly and begin to descend toward the 
                                    blackness that surrounds Marana.  One 
                                    of my least favorite things to do at night, 
                                    especially in mountainous terrain, is to 
                                    land at a strange airport.  Thank 
                                    goodness for all the lights Mooney puts on 
                                    the Ovation.  With a landing light on 
                                    each wing, a taxi light on each wing, white 
                                    recognition lights on each wing, we light up 
                                    the sky like a Boeing. 
                                    
                                    
                                    Normally, I 
                                    like to fly between 90 and 100 on base while 
                                    descending at 500 FPM, and then turn final 
                                    and put the rest of the landing flaps (the 
                                    Ovation has flap preselect set at TO = 
                                    10-degrees and LDG = 33-degrees) down.  
                                    Then slowing to a normal landing Vref of 1.3 
                                    VSO or about 75 KIAS on short 
                                    final, I will cross the fence at 1.2 Vref 
                                    before entering the flare.  Trimming 
                                    with the standard electric trim, and I make 
                                    a smooth touchdown.  How come my best 
                                    landings come when I’m alone?
                                    
                                    
                                     
                                    
                                    No 
                                    cowl flaps needed
                                    
                                    
                                    When we talk 
                                    about landings in the Ovation or any of the 
                                    new generation long body Mooneys (M20M, M20R 
                                    or M20S) we must talk about the landing 
                                    attitude.  As I mentioned earlier, the 
                                    long bodies sit with about a positive 4.5 
                                    degrees pitch attitude on the ground.  
                                    Pilots moving into the newer aircraft from 
                                    one of the shorter length Mooneys (M20K or 
                                    earlier) will immediately notice this 
                                    difference when they first sit in the 
                                    cockpit.  Now thinking about sight 
                                    picture and pitch attitude during the flare 
                                    for landing, most aircraft will need about + 
                                    5-degrees during the round out to keep the 
                                    nose wheel off the runway until the mains 
                                    are on.  This works quite well for all 
                                    the Mooneys except the Ovation, Eagle or 
                                    Bravo.  With an almost 5-degree nose up 
                                    attitude sitting level, the pitch attitude 
                                    is going to need to be higher during landing 
                                    in order to land on the main wheels before 
                                    the nose.  One of the biggest 
                                    transition problems I have found for pilots 
                                    moving into these long Mooneys is the 
                                    landing – more specifically, landing on the 
                                    nose first or all three simultaneously.  
                                    Either action can quickly lead to a porpoise 
                                    and the outcome of this isn't very pretty.  
                                    Pilot must develop a different sight picture 
                                    when landing these new Mooneys.  Where 
                                    5-degrees worked before, 8-degrees is 
                                    necessary now.  This just takes 
                                    practice and the help of a competent 
                                    instructor familiar with long-body Mooneys.
                                    
                                    
                                     As with all 
                                    Mooneys, airspeed control during the final 
                                    approach is key.  Fly too fast and the 
                                    airplane will float on a cushion of air 
                                    forever.  
                                    
                                    
                                    Fly the correct 
                                    approach speed (1.3 V Stall for the weight 
                                    and flap configuration) on short final, have 
                                    the airplane configured for landing and 
                                    trimmed and the touchdown is normal.  
                                    If we use a target altitude of 50 feet above 
                                    the runway to achieve this, then the last 50 
                                    feet is very easy.  If we are still 
                                    chasing the airspeed or trim at 50 feet AGL, 
                                    then a go around might be advised in order 
                                    to set it up again.  Seldom do good 
                                    landings come from bad approaches!
                                    
                                    
                                    
                                    El Paso 
                                    slides under the nose
                                    
                                    
                                    Also, since these longer Mooneys have larger 
                                    (and heavier) engines up front, I recommend 
                                    liberal use of the electric trim to relieve 
                                    the control wheel force during the flare.  
                                    With just two people in these airplanes, the 
                                    CG during landing is well to the front of 
                                    the envelop and the rotational forces are 
                                    quite high (it’s an inertia issue not 
                                    control effectiveness).  I’ve noticed 
                                    the after my best landings, the elevator 
                                    trim is almost completely nose-up under 
                                    these situations.  One area that seems 
                                    to be a concern to some when they think 
                                    about landing a Mooney with full flaps (the 
                                    recommended configuration) and a bunch of 
                                    nose-up trim is the go around.  This is 
                                    just not an issue.  The go around 
                                    procedure in the Ovation (as well as all 
                                    other Mooneys) is: 
                                    
                                    1.     
                                    
                                    
                                    Pitch to 8-degrees nose up while 
                                    simultaneously smoothly applying full 
                                    takeoff power to climb at VX.
                                    
                                    2.     
                                    
                                    
                                    Retract the flaps to the takeoff position 
                                    (if they are full down).
                                    
                                    3.     
                                    
                                    
                                    Verify on the VSI and Altimeter that there 
                                    is a positive rate of climb.
                                    
                                    4.     
                                    
                                    
                                    Retract the landing gear.
                                    
                                    5.     
                                    
                                    
                                    Retract the remaining flaps.
                                    
                                    6.     
                                    
                                    
                                    Target VY if clear of obstacles.
                                    
                                    7.     
                                    
                                    
                                    Throughout this procedure, use electric and 
                                    manual trim as necessary to reduce the 
                                    pressure on the control wheel. 
                                    
                                    
                                    This is easily accomplished even without 
                                    electric trim, and during the process, the 
                                    control forces needed to fly the correct 
                                    pitch attitude or airspeed are well within 
                                    those even the smallest and lightest pilots 
                                    posses. 
                                    
                                    
                                    Three hours and fifty minutes after 
                                    departing Kerrville, N1051K had arrived at 
                                    it’s new home and the proud owner was 
                                    carefully putting her to bed in her new 
                                    hanger…what an airplane! 
                                    
                                    
                                    Four days later, after accomplishing more 
                                    than 12 trouble-free hours of flight 
                                    training, I am once again in 51K ready to 
                                    depart back to Kerrville to return the 
                                    airplane to the factory for it’s first oil 
                                    change.  During the almost 16 hours of 
                                    cross-country and rugged flight training, we 
                                    only used 1 ½ quarts of oil, so the rings 
                                    should be seating correctly. 
                                    
                                    On 
                                    the return (Marana to San Antonio – 678 NM - 
                                    3 hours, 25 minutes, 49 gallons of fuel) I 
                                    did get the chance to do some speed runs at 
                                    11,000 feet to check the true airspeed.