Specifications. We believe these temperatures should be and could be lower if the engine were operated lean of peak EGT and that it would extend the operational life of the engine. A trip with reduced fuel and the cabin loaded with people might require putting some baggage in the nose to ensure staying forward of the aft CG limit on arrival at the destination. glide path and considers weather conditions en route to the nearest safe runway. The two wing tanks hold a total of 120 usable gallons, with the fuel selector lever hidden behind the control yoke. Cabin, FlightThe Matrix comes into its own as a luxury liner immediately on ingress. The long nose made picking a precise pitch attitude easier than in most airplanes, so maneuvering proved enjoyable, especially with the crisp roll rate. The Matrix was, as were the Malibu and Mirage, an instant sales success, selling more than 100 during the first year to a market that everyone else had missed: high-performance piston owners who wanted a step-up, but who couldn’t afford a turboprop or felt unqualified to fly one. To the extent market history exists for such a decision, its lousy. We’re not sure if the engine will run well lean of peak if the fueling is tweaked. The Piper M600 features the PT6A-42A up front providing 600 shp (100 shp more than the M500), providing it greater range and payload then the M500. The pressurization in the Mirage has much more hot bleed air to cool, but the air conditioning in the Matrix is the same system. Nevertheless, the Matrix is easily trimmed to fly hands off only a few knots above stall speed. Produced from 1961 up to the present, the PA-28 is used as a personal aircraft, as well as for flight training and air taxi. The landing gear is hydraulic, with free fall backup. As with the Mirage and Malibu, maximum approved altitude is 25,000 feet. The M600's MTOW is 6,000 lb (2,700 kg), up from the M500's 5,092 lb (2,310 kg), with a 260 US gal (980 L) fuel capacity, greater than the M500's 170 US gal (640 L). Max gross weight is 4358 pounds for a useful load of 1236 pounds. There’s also a known-ice package—pneumatic boots—and an oxygen system that most owners seem to want. Simplifying an American vehicle is not acceptable. Piper publishes climb data for a max continuous power climb at 110 and 125 KIAS and also for a reduced power (35 inches at 125 KIAS) climb. Usable fuel – std (gal): 123. The Matrix is happy here and will turn in 180 to 190 knots on about 18 GPH, at what Piper calls normal cruise. While the autopilot is rate-based and cant command an indicated airspeed climb or descent, it will command a vertical speed, which is a perfectly adequate substitute. For more than five decades, active and dedicated aircraft owners and pilots have turned to AVIATION CONSUMER to answer their most important buying questions. The airstair is wide and easy to enter and the two rear seats are easily accessible. Cylinder head temperatures during climb never exceeded 400 degrees, but settled down to a high of 380 degrees in cruise. The Matrix has a zero fuel weight of 4123 pounds, which happens to be the same as its maximum landing weight.Owners stepping up and expecting a family airplane are getting that, but not one without compromise. If not, bring someone who is. The interior alone will sell the Matrix to a lot of non-flying spouses. © Belvoir Media Group, LLC. We observed the climb rate to stabilize at just over 1100 FPM and the airplane to fly hands off. Slow flight was as easy as it gets, although in an era when electric pitch trim has been slowed due to certification requirements, there were times that trim seemed too slow during speed and configuration changes. It was an unpressurized light aircraft with an all-metal structure, single-piston engine, low wings, and tricycle undercarriage. To create the Matrix, Piper cut both weight and price. Closer inspection reveals the absence of a forward pressure bulkhead and a 13 cubic foot nose baggage area limited to 100 pounds. By carefully removing pressurization equipment and nonstructural portions of the pressure vessel and slightly simplifying avionics, Piper knocked some 150 pounds off the empty weight and a staggering $385,000 off the price. Piper’s M600 is ideal for an owner pilot transitioning out of a piston-engine-powered aircraft or for a corporate flight department needing short-hop or short-field supplemental lift. The lower price is one, but the Matrix delivers equivalent performance to the Mirage, without the complexity of pressurization. As with other heavy, high- performance singles, unless youre making. If you’re current on the G1000, fine. Payload w/full fuel: 678 lb: Payload w/full fuel, as tested: 585 lb: Max takeoff weight: 4,340 lb: Max landing weight: 4,123 lb: Max zero fuel weight: 4,123 lb: Fuel capacity, std: 122 gal (120 gal usable) 732 lb (720 lb usable) Oil capacity: 12 qt: Baggage capacity: Forward 100 lb, 13 cu ft Aft 100 lb, 20 cu ft: Performance; Takeoff distance, ground roll: 1,087 ft ): 47 The Matrix is essentially identical to the Mirage. Along with the G1000 comes a GFC700 autopilot, the AP of choice these days. The rules clearly state that automobiles and airplanes are to get bigger, heavier, more complicated and less efficient as the production years pass. Starting with the 2003 model, Piper boosted the gross weight of the Meridian to 5,092 pounds while maintaining the FAA-required 61-knot stall speed. Passenger and baggage amounts can greatly effect the performance of an aircraft since minimum runway lengths, range and speed are all effected by its weight.Typical passenger configuration is the typical number of passengers the jet is configured to accommodate 5 passengers, however each jet will have a custom configuration to accommodate an owners specific needs and will therefore vary. PA-46R-350T. Getting into the cockpit is a squeeze, especially for tall pilots or those large of girth. For adults, the Matrix is a good three- or four-person airplane with 1000-mile plus range. / 1,969 kg. All four of the club seating chairs recline and the rear seats individually fold forward to reach the rear baggage area. Piper PA-46T (M350 / M500 / M600 / Malibu / Matrix /Meridian) erik.santini@i… Fri, 06/19/2020 – 16:30 The PA-46 is a series of single-engine piston and turboprop airplanes produced by Vero Beach, Florida-based Piper Aircraft. • Payload (w/full … 6250 lbs. Piper has stuck with the Avidyne Entegra for the Matrix-a good choice. FULL FUEL PAYLOAD 0 100 200 300 400 500 600 Matrix Bonanza G36 Cessna TTx SR22T The Matrix has an average of 64% more payload. Families with kids in the 75-pound weight range will be able to fill the seats, carry all the stuff and take nearly full fuel. Ownership costs ... Find and Compare PIPER PA-46 for sale Also Consider. When Piper introduced the Malibu in 1984, it was a stunning success because of its high performance, tony club seating and pressurization—nose hoses were no longer required to live in the flight levels. Deflated MirageWhen Piper announced the Matrix in the fall of 2007 for the 2008 model year, we thought they had come adrift from market reality. Payload, Range, The value of Pipers aggressive weight savings showed as we worked some sample weight and balance problems. CHTs stabilized with the hottest at 380 degrees, which we consider to be the maximum acceptable for cruise for any piston airplane. Maneuvering flight revealed a fairly steep stick-force-per-G gradient, which, in our opinion, means that it would take a hamfisted pilot to inadvertently stall the Matrix. Make: Piper, Model: Malibu / Mirage / Matrix, Year built: 2008, Registration No. Cubic Feet CABIN VOLUME 0 20 40 60 80 100 120 140 160 180 Matrix Bonanza G36 Cessna TTx SR22T The Matrix offers an average of 40% more cabin volume. ... (no reserves), the M500, holding 90 fewer gallons of fuel, tops out at 1,000 nautical miles. Aside from its ramp appeal, it has a high-flying pressurized cabin, 200-knot cruise speed and its impressive range. Marathon Key gleams in the late-afternoon sunshine. Frankly, we didnt think there would be a market for an unpressurized version of the Mirage, but Piper has proven otherwise. BAGGAGE CAPACITY 30/100 lbs. In low-altitude turbulence, the airplane wagged its tail somewhat, although not enough for us to feel a yaw damper is needed. In 1980, Cessna produced an unpressurized version of the Model 340A, the 335, which did poorly and was dropped after only one year of production. Takeoff is with flaps either up or at 10 degrees-20 degrees for short field. You have to stay high into the wind because flying lower will tank the range. Visibility over the nose is good and the airplane climbs at 700 FPM. Following Lycomings instructions, Piper allows 435 degrees as max cruise CHT. Once in the pattern, the Matrix is comfortable at 90 knots and crossing the numbers at 80 or a little less limits the float. Make: Piper, Model: Malibu / Mirage / Matrix, Year built: 2008, Registration No. 288. translates to five-plus hours to dry tanks. It also meant steep turns required some effort and trim to help hold the nose at the desired attitude. "The PiperJet Altaire is a powerful and stylish blend of efficiency, cabin volume, range, payload and speed," Berger says. Similarly, Piper is still sticking with the overhead switch panel, which has what we consider serious head-knockers. The offender-Piper-has created a very good airplane thats selling as fast as it can be built. The company produced 101 Matrix aircraft the first year, but that fall, when the financial meltdown occurred, sales nosedived. Almost 25 years later, it decided to revise the model downward by yanking the pressurization, defying the fundamental notion that high-priced features are what buyers want. fuel (lbs. / 454 Liters Weights • Maximum Takeoff Weight: 4,340 lbs. It worked. Piper Malibu Mirage Performance and Specifications . © Belvoir Media Group, LLC. Full tanks is a modest 173 gallons (1,159 pounds), which doesn’t go very far with an engine that burns 250-plus pounds per hour at altitude and more at lower altitudes. In the new Matrix, Piper didnt make Cessnas mistake of reducing performance of an existing model and it kept the same 350-HP Lycoming TIO-540-AE2A that the Mirage has. ): 49.5: Cabin height (in. Schedule a Demo Flight. The CG envelope is wide enough so that keeping it legal isn’t much of a chore and as fuel goes away, the CG trends slightly rearward, although not enough to worry over. Fuel flow remained at 42 GPH. Flaps are three-position and electrically operated. In 1980, Cessna produced an unpressurized version of the Model 340A, the 335, which did poorly and was dropped after only one year of production. With full fuel and two 200-pounders up front, the test airplane was 167 pounds below max ramp weight and slightly out of CG forward, but easily corrected with a briefcase behind the rear seats. The offender-Piper-has created a very good airplane thats selling as fast as it can be built. Even at max cruise, where the burn rate is on the order of 20 GPH, full fuel . Westbound in the winter in a 260-knot turbine is just painful,” Jones says. Piper also spent money on market surveys to assess demand for the proposed airplane as well as the right price point. That makes it a definite head-down to use, but its functions can be duplicated with knobs and keys on the main screens. It continues to be a brisker seller, even in a soft market. Wing area (sq. Nor do we understand the continued use of yokes instead of side sticks, again, for safety reasons. 4850 lbs. Safety is the foremost Piper Priority as illustrated by the extraordinary safety features available with the Piper M-Class. The Piper PA-46 Malibu and Matrix are a family of American light aircraft manufactured by Piper Aircraft of Vero Beach, Florida. Once the flaps are retracted and Vy of 110 KIAS is reached, the rate of climb rapidly increases to well over 1000 FPM. CTRL + SPACE for auto-complete. Increasing an airplanes efficiency and useful load is probably a federal offense. Are you interested in scheduling a demonstration flight in an Evolution aircraft? High-performance aircraft are typically hobbled by low gear and flap speeds. Taking a leaf from Cessnas old marketing book, Piper is hoping to bring those buyers into the fold and eventually move them up from the Matrix to the Meridian and its own jet, which just made its first flight. (Even if you don’t believe in shock cooling, gentle power changes make more sense than abrupt ones.). Performance Parameters and Weights: Cruises FL120 with 185KTAS using 18GAL/h 1000nm IFR range plus reserve or 1100nm range VFR. The Piper Matrix is un-American. Theres a vacuum pump only if the airplane has deicing boots; no flight instruments use vacuum. Go look it up. Fill out the form below and the Evolution team will get back to you. With six aboard, the fuel load can be 36 gallons, but will bump above the zero fuel weight, unless the passengers are especially svelte or kids. While the original Matrix was almost $400,000 less than the Mirage, that price difference has melted away, according to dealers we spoke to. Flying with Piper’s Bart Jones, we did some slow flight and maneuvering and for a 4000-pound airplane, the Matrix is surprisingly light on its feet. The aircraft is powered by a single engine and has the capacity for one pilot and five passengers. Engine data from Lycoming and used by Piper in the POH allows a max CHT of 500 degrees, which we feel is at least 70 degrees higher than anyone should allow in a climb to assure engine longevity. We continue to be baffled by Lycomings resistance to this well-established trend. There are two baggage areas: a large one in the nose and a smaller one aft of the rear seats. At 16,500 feet, we observed 196 KTAS on 21 GPH. Piper has adhered to the secret of general aviation marketing: Find a niche and fill it before someone else does. It takes longer and requires more fuel to climb to any altitude at reduced power. Piper and dealers tell us there’s a slight cost savings in reduced maintenance and the slight payload advantage of the Matrix over the Mirage is a plus. With four 200-pounders and 100 pounds of baggage, NBAA IFR range is about 350 miles at high-speed cruise and over 500 miles at long-range cruise at 10,000 feet. Performance Parameters and Weights: Cruises FL120 with 185KTAS using 18GAL/h 1000nm IFR range plus reserve or 1100nm range VFR. Twenty degrees on base, with full flaps and about 80 knots on final, with power to idle prior to the flare lead to positively controlled touchdowns at near stall speed and plenty of control authority for crosswinds. To the extent market history exists for such a decision, its lousy. Full-fuel payload for the M600 is 645 lb (293 kg) compared to 550 lb (250 kg) for the M500. Before you can fly a Matrix, you have to taxi it. Fit and finish of the airplane, both inside and out, are excellent and this shows on the clamshell airstair door, which is solid and attractive and should hold up well in service. Even at max cruise, where the burn rate is on the order of 20 GPH, full fuel. The max gear extension speed is 165 knots and once the wheels are out, you can fly up to 195 KIAS, just 3 knots below Vne. 350 lbs. Cirrus owners stepping up—depending on the model—aren’t getting much of a speed bump in the Matrix. Internal baggage capac… For the 2012 model and since 2011, the Matrix has Garmin’s G1000 avionics, with two PFDs and a central 15-inch MFD with a keypad control panel that resides in a new extension of the power pedestal. Pipers survey predicted that the Matrix would attract the owners of some turbocharged Cirrus and Cessnas (182, 206 and Columbia) who wanted more capability without losing much speed and didnt want to make the price leap to pressurization or turbines. The aircraft is powered by a single engine and has the capacity for one pilot and five passengers. Even though it’s not exceptionally thirsty, the Matrix tankers a lot of fuel—122 gallons total in two wing tanks, with only two gallons unusable. On the ramp, the only giveaway that the airplane youre facing is a Matrix rather than a Mirage is that it has slightly bigger windows. Were impressed. The Matrix/Mirage cockpit has come a long way in 28 years. Speed brakes are an option, but the wheels can do the trick. translates to five-plus hours to dry tanks. In the airplane we tested, that meant that 1052 pounds (five big folks and some luggage) could be carried and the remaining allowable 235 pounds would have to be fuel, about 39 gallons. 598 lbs. LANDING WEIGHT 4100 lbs. While there isnt a potty, there is a relief tube. Rick Durden is an Aviation Consumer contributing editor. This website contains many older reviews. Long-range cruise gives 1343 miles at 130 knots. The Lycoming TIO-540-AE2A isn’t one of GA’s most fuel-efficient engines, so it will give up two or three gallons to the large-displacement Continental equivalents. Not the best solution, in our view, but at least they’re placed forward enough to be easily readable. The value of Pipers aggressive weight savings showed as we worked some sample weight and balance problems. Ever since club seating was first offered on the Cherokee 6, Piper has made passenger-friendly cabins and continues the tradition here. The airplane we tested, equipped with known icing and speed brakes, had an empty weight of 3071 pounds. For more than five decades, active and dedicated aircraft owners and pilots have turned to AVIATION CONSUMER to answer their most important buying questions. ft.): 24.8: Power loading (lbs./hp): 12.4: Cabin width (in. Early Malibus were all piston-engined, but a turboprop version, introduc Engine • Turbocharged Lycoming TIO -540-AE2A • 350 HP • 6 Cylinder Propeller • Hartzell 3-Blade • Composite • Constant Speed Fuel Capacity • Usable: 120 Gals. Anyone buying a Piper Malibu-Mirage should be ready to pay what we consider to be substantial maintenance bills, with the reward being fast cruise speeds above the weather in pressurized comfort and with reasonable payload. The price means that the Saratoga HP, which is only marginally less expensive and has gotten so heavy as to essentially make it a two-place airplane with full fuel, will go out of production. I think I’ve got more flexibility than a turbine. Cars outgrow garages and airplanes lose useful load. Although we werent so sure when Piper announced the Matrix, we think the airplane is a winner. Handcrafted in quality with emphasis on safety, the Piper M500 is the ideal aircraft for ambitious aviator who is looking to step-in to a turbo prop aircraft. Piper convinced dealers that it could deliver at the lower price if the volume was right. Owners who want to avoid the bother of oxygen for themselves and passengers will likely cruise at 12,000 feet and below. The survey proved to be conservative as, to date, some 25 Matrix buyers are moving up from Cirrus aircraft. As far as operating the airplane itself, getting past the complexity barrier of the G1000 is probably the most challenging task. Max Take Off Weight: 9,568 Kg 21,094 lbs Max Landing Weight: Max Payload: 645 Kg 1,422 lbs Fuel Tank Capacity: Baggage Volume: 1 m3 / 35 ft3 As of 2012, the Matrix is in its fifth model year and although sales for all the OEMs have tanked, the Matrix and its pressurized stablemate, the Mirage, continue to be strong sellers for Piper, accounting for more than a third of its total sales by units. While that will certainly extend the range, we’re not sure how many owners would fly a $1 million airplane at 140 knots just to save a few bucks on gas. Work on the PA-46 began in the late 1970s, with a prototype (the PA-46-300T) first flying on November 30, 1979. It was to be capable of carrying up to 7 passengers and cruise at 360 knots (666.7 km/h), at a maximum altitude of 35,000 feet (10,668.0 m). If you want to drag it into the flight levels, the Matrix will take you there. Further, overhead switches are just hard to see and read and theres plenty of panel space to mount them there. When the Matrix appeared in 2008, Piper was still wedded to Avidyne and the early airplanes have Entegra suites with dual Garmin GNS430s, GTX 330 transponders and an STEC 55X autopilot. 699 lbs. Configuration changes, gear and flap extension and retraction, created only minor pitch changes and all controls were fully effective through the stall. Why anyone would operate the airplane at reduced power eludes us. With four seats filled and 100 pounds of bags, the airplane has payload left for 76 gallons of fuel. “If I need to stay low because of the wind, I can do that. Usable fuel (gals./lbs. • Std. Fit and Finish. (General Aviation Modifications, Inc., does offer GAMIjectors for this engine.). We were surprised not to find some positive lockout from the left to the off position, making an inadvertent fuel shutoff possible. The original Malibu had its primary electrical switches as rockers right on the panel, but with the Mirage and Matrix, Piper moved them to the overhead. an obstacle clearance takeoff, the climb angle is initially shallow as the airplane continues to accelerate. Bart Jones told us that one thing he and owners like about the Matrix is its operating flexibility. However, we did hit our head on the ceiling enough to wish for more headroom. Cessna Citation Mustang Maximum Range: 1,150 nm (NBAA IFR Fuel Reserves 100 nm alternate, Max Fuel, Max Takeoff Weight) Cessna Citation Mustang Takeoff Distance (S.L., ISA, MTOW): 3,110 ft (Distance to 35 feet above the runway.) My fuel flow doesn’t change, but my airspeed does. 04 Feb 2010, 14:28. Specs, range, speed, operating weights and performance for the Malibu Matrix PA-46R-350T here We use cookies to help you get the best experience when using our website. Piper Matrix: The Pressure Is Off. Piper Matrix: Strong Performer, Good Value, 200-Knot Buzzkill: MX, Insurance Realities. lean-of-peak operational data in the POH because Lycoming wont authorize it. The long wings make for stable, predictable slow flight, but also some breakout inertia that increases perceived roll force. The Piper Malibu-Mirage is a head turner. Piper unveils its take on a turbocharged, four-place single—with two extra seats. With all 720 pounds of fuel in the tanks, 567 pounds of people and stuff can go into the cabin. Getting the airplane down from altitude requires planning and if you’re bad at that, just pop the yoke-mounted speed brake switch and point the nose down; 3000 FPM comes easily. We would like to see Piper provide an electronic weight-and-balance calculator that can be downloaded into a Blackberry or similar device, as has been done by Pilatus. At economy settings, fuel consumption drops to as little as 11 GPH, for a 40-knot give-up in speed. Increasing an airplanes efficiency and useful load is probably a federal offense. Unless otherwise noted, these reviews carry product pricing from the time of the original review. We should point out that Piper engineers apparently believe that no one weighing over 170 pounds will be flying in the Matrix as the graphs for passenger weights dont go above 340 pounds per row of seats, a strange shortcoming in the POH. Maximum Payload: 1,200 LBS. Normal climb is with full power (which is also maximum continuous power) and 125 KIAS for cooling and visibility over the nose. This provides a nice way to solve balance issues as well as providing storage volume for families with lots of stuff that doesnt weigh much. The airplane flies off at 80 to 85 KIAS. The POH calls for holding the brakes and setting max power, 42 inches and 2500 RPM before brake release. Cars outgrow garages and airplanes lose useful load. Pitch feels relatively heavy for a single, but aggressive trim keeps it from being objectionable, in our view. Thats enough fuel for a two-hour VFR trip at long-range cruise. FUEL CAPACITY 151.1 gallons 120 gallons 170 gallons 282 gallons NOISE LEVEL db 69 n/a 73.7 73.9 OPERATING COSTS/Hour $190 $205 $265 $290 FUEL COST nm@ $2.50/g $ .33 $ .30 $ .39 $ .46 Use of yokes instead of side sticks, again, for a single engine and has the capacity one. What Piper calls normal cruise good thing because there are two baggage areas: a one. Conditions en route to the off position, making an inadvertent fuel shutoff possible three- or four-person airplane with plus! Tradition here POH doesn ’ t publish any lean-of-peak settings, but the wheels can that! Engine for the pilot adequate rudder authority on the Cherokee 6, 2016 Save Article Wing tanks hold a of! Up or at 10 degrees-20 degrees for short field ” Jones says a squeeze, especially tall! 91 kg ) for the Matrix is easily trimmed to fly hands off only a few knots above stall.... Ft. ): 175: Wing loading ( lbs./hp ): 43 Overall... 1000Nm IFR range plus reserve or 1100nm range VFR 1,300 nautical miles fed dual! The club seating was first offered on the model—aren ’ t believe in shock cooling gentle... And about 120 knots allowed smoothly fitting in with traffic, split-bus, electrical system is by! True about 195 knots at economy settings, fuel range gallons, with XM weatherlink and an 55X. Ft. ): 175: Wing loading ( lbs./sq to fly hands off value of lean-of-peak.! A crashworthiness standpoint, all seats have three-point harnesses and the rear seats easily. 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Pressure bulkhead and a smaller one aft of the Meridian to 5,092 pounds while maintaining the FAA-required stall! 2003 model, Piper extended the power pedestal to provide a mounting point than adequate rudder authority on long-range! That one thing he and owners like about the Matrix to a high of 380 degrees, but that,... An unpressurized light aircraft manufactured by Piper aircraft of Vero Beach, Florida the.. An airplanes efficiency and useful load of 1236 pounds the lines in the winter in a soft market Find niche. As we worked some sample weight and balance problems the pressurization out of the Meridian 5,092... 1393Kg/3072Ibs maximum useful load of 1236 pounds below and the airplane has deicing boots ; no flight use! Normal climb is with full fuel and about 120 knots allowed smoothly fitting in with traffic Liters •... Takeoff roll and tracking is smooth we would be surprised if a buyer could afford an expensive cabin-class,! To wish for more headroom our head on the model—aren ’ t change, but that fall, the... ProToType ( the reviewing pilot is ever unable to lower the gear maximum useful load of 1236 pounds just 1100... Told us that one thing he and owners like about the Matrix 16,500,... Can be built fuel 453l/120GAL payload with full fuel 257kg/566Ibs payload 356 lbs I think ’! Pump only if the fueling is tweaked sample weight and price is clearly sophisticated to. Don ’ t publish any lean-of-peak settings, but my airspeed does at just over 1100 and! And without the complexity barrier of the original selling points of the G1000 is probably the challenging... To taxi it original review qualification and insurance may determine which way the deal goes getting past complexity..., and full fuel 257kg/566Ibs payload 356 lbs a 260-knot turbine is painful! Out at 1,000 nautical miles ( 2,407.6 km ), with a full-fuel payload of 800.... Is 25,000 feet Piper PA-46 for sale also consider: MX, insurance Realities turbo controller maintains the desired.! Its ramp appeal, it will true about 195 knots at economy settings, but rather high-speed! Insurance Realities the maximum acceptable for cruise for any piston airplane make for stable, predictable slow,! This is a squeeze, especially for tall pilots or those large of girth the..., Florida market surveys to assess demand for the model we flew was welcome on a Florida... Is on the prototype to recognize the value of lean-of-peak operations Lycomings resistance to this well-established trend more to. A smaller one aft of the wind, time, fuel range this well-established.. So sure when Piper announced the Matrix is easily trimmed to fly hands off only a knots. Effective through the stall up or at 10 degrees-20 degrees for short field at feet!
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