Before you can fly a Matrix, you have to taxi it. As an OEM, Piper cant publish. 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. CTRL + SPACE for auto-complete. The Matrix is happy here and will turn in 180 to 190 knots on about 18 GPH, at what Piper calls normal cruise. Unless otherwise noted, these reviews carry product pricing from the time of the original review. The Piper PA-46 Malibu and Matrix are a family of American light aircraft manufactured by Piper Aircraft of Vero Beach, Florida. He lives in Denver. Since G1000 has a keyboard, Piper extended the power pedestal to provide a mounting point. / 454 Liters Weights • Maximum Takeoff Weight: 4,340 lbs. Flying the traffic pattern was a pleasure. We dont much like the lack of flail space in the cockpit and would prefer four- or five-point harnesses up front. 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. Ownership costs ... Find and Compare PIPER PA-46 for sale Also Consider. 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. We were surprised not to find some positive lockout from the left to the off position, making an inadvertent fuel shutoff possible. 200-Knot Buzzkill: MX, Insurance Realities. Owners who want to avoid the bother of oxygen for themselves and passengers will likely cruise at 12,000 feet and below. 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. It takes longer and requires more fuel to climb to any altitude at reduced power. Simplifying an American vehicle is not acceptable. Like the Cen­tu­rion, the Mal­ibu was to fea­ture cabin pres­sur­iza­tion (5.5 psi), a fea­ture not in­cluded on the pro­to­type. Piper unveils its take on a turbocharged, four-place single—with two extra seats. Go look it up. The offender-Piper-has created a very good airplane thats selling as fast as it can be built. 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. Unless otherwise noted, these reviews carry product pricing from the time of the original review. "The PiperJet Altaire is a powerful and stylish blend of efficiency, cabin volume, range, payload and speed," Berger says. Bart Jones told us that one thing he and owners like about the Matrix is its operating flexibility. 100/100 lbs. The air conditioning in the airplane we flew was welcome on a hot Florida day in August. 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. 100 lbs. 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. ): 120/720: Payload, full std. an obstacle clearance takeoff, the climb angle is initially shallow as the airplane continues to accelerate. Simplifying an American vehicle is not acceptable. Its maximum payload is 1,200 pounds, and full fuel is 1,768 pounds. Increasing an airplanes efficiency and useful load is probably a federal offense. 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. While going high gives impressive speed and IFR range, the limiting factor is the 50-cubic-foot internal oxygen system, which has only 3.1 hours for three people at FL200. The time above 10,000 feet on the long-range cruise power flight would be about 7 hours. This website contains many older reviews. Pilot qualification and insurance may determine which way the deal goes. Rick Durden is an Aviation Consumer contributing editor. ConclusionAlthough the reduced price difference between the Matrix and the Mirage makes it less of a value than it once was, we think it’s still an impressive performer for step-up owners who don’t want to fool with pressurization and/or who aren’t customers for a single-engine turboprop. On takeoff, the airplane holds the centerline like it’s on rails and at 80 indicated, a healthy tug pulls it off. 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. Once in the pattern, the Matrix is comfortable at 90 knots and crossing the numbers at 80 or a little less limits the float. As far as operating the airplane itself, getting past the complexity barrier of the G1000 is probably the most challenging task. In low-altitude turbulence, the airplane wagged its tail somewhat, although not enough for us to feel a yaw damper is needed. Fill out the form below and the Evolution team will get back to you. 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. Go look it up. The offender-Piper-has created a very good airplane thats selling as fast as it can be built. The airplane we tested, equipped with known icing and speed brakes, had an empty weight of 3071 pounds. • Engine - Textron Lycoming TIO-540-AE2A • Horsepower – 350 • TBO – 2000 hours • Fuel Type – 100/100LL • Propeller – 3-Blade Hartzell • Landing Gear – Tricycle/Retractable • Max Ramp Weight – 4358 lbs. 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. 699 lbs. 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. 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. The interior is identical as well. 4100 lbs. Payload – full std fuel (lbs): 648. At FL200, it will true about 195 knots at normal cruise or 150 knots at economy cruise. Getting into the cockpit is a squeeze, especially for tall pilots or those large of girth. PA-46R-350T. 288 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. 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. If you want to drag it into the flight levels, the Matrix will take you there. The company produced 101 Matrix aircraft the first year, but that fall, when the financial meltdown occurred, sales nosedived. However, and inexplicably, it would mean running the tanks dry before landing as the max landing weight is precisely the same as the zero fuel weight, making the real-world zero fuel weight something less if one wants to touch down with the engine running. The Garmin G1000 NXi Next Generation Integrated Flight Deck, 500 shp Pratt & Whitney Pt6A-42A engine, 260 ktas max … With four seats filled and 100 pounds of bags, the airplane has payload left for 76 gallons of fuel. The airplane we tested, equipped with known icing and speed brakes, had an empty weight of 3071 pounds. It worked. Max ramp weight is 4358 pounds, giving the tested airplane a useful load of 1287 pounds, or 134 pounds less than in Pipers advertising literature. Once the flaps are retracted and Vy of 110 KIAS is reached, the rate of climb rapidly increases to well over 1000 FPM. BAGGAGE CAPACITY 30/100 lbs. The interior alone will sell the Matrix to a lot of non-flying spouses. 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 © Belvoir Media Group, LLC. Avoiding oxygen use by flying at 10,000 feet, full-fuel VFR range at high-speed cruise, with reserve, is 960 miles while at 185 KTAS. Maximum range was expected to be 1,300 nautical miles (2,407.6 km), with a full-fuel payload of 800 pounds. including metal bars over the starter and mag switches. All four of the club seating chairs recline and the rear seats individually fold forward to reach the rear baggage area. © Belvoir Media Group, LLC. Its also standard equipment, which is a good thing because there are no openable windows. Despite the current economic downturn, it appears the decision was a winner. The aircraft is powered by a single engine and has the capacity for one pilot and five passengers. Its such a well-thought-out system that we would be surprised if a pilot is ever unable to lower the gear. The value of Pipers aggressive weight savings showed as we worked some sample weight and balance problems. The Matrix/Mirage cockpit has come a long way in 28 years. 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. Ever since club seating was first offered on the Cherokee 6, Piper has made passenger-friendly cabins and continues the tradition here. 288. translates to five-plus hours to dry tanks. The original Matrix we flew in 2008 had an empty weight of 3071 pounds against 3121 for the 2012 model, which was equipped with air conditioning. What we mistakenly discounted was the large price Delta between the two models. Piper Matrix: The Pressure Is Off. To the extent market history exists for such a decision, its lousy. The rules clearly state that automobiles and airplanes are to get bigger, heavier, more complicated and less efficient as the production years pass. The two wing tanks hold a total of 120 usable gallons, with the fuel selector lever hidden behind the control yoke. Specifications. It’s not hard, but the wingspan is 43 feet, so you need to pay attention on the ramp and taxiways to avoid catching a wing or a snowdrift. For adults, the Matrix is a good three- or four-person airplane with 1000-mile plus range. During our climb the hottest CHT was 404 degrees, an indication that without having to pump up a cabin , the engine wasnt working as hard. Similarly, Piper is still sticking with the overhead switch panel, which has what we consider serious head-knockers. 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. Piper convinced dealers that it could deliver at the lower price if the volume was right. Useful Load – 1421 lbs. Piper also spent money on market surveys to assess demand for the proposed airplane as well as the right price point. High-performance aircraft are typically hobbled by low gear and flap speeds. Configuration changes, gear and flap extension and retraction, created only minor pitch changes and all controls were fully effective through the stall. Empty Weight – 2937 lbs. Extra PoundsOne of the original selling points of the Matrix was Mirage-level performance at equivalent fuel economy with about 50 more pounds of payload. To create the Matrix, Piper cut both weight and price. 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. The sight picture gives the impression of the prop being a long way forward—it is—and with the baggage between you and the engine, the cabin is quiet. A typically equipped Matrix invoices for about $757,000, with the only big ticket option being known icing approval, which costs $55,000 and knocks 4 knots off the cruise speed. The 28-volt, split-bus, electrical system is fed by dual 75-amp alternators with a 16-amp-hour battery for backup power. “If I need to stay low because of the wind, I can do that. 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. 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 Matrix is essentially identical to the Mirage. • Payload (w/full … This website contains many older reviews. The first notch of flaps can go out at 165 knots, too. 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. The landing gear is hydraulic, with free fall backup. Westbound in the winter in a 260-knot turbine is just painful,” Jones says. 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. Insurance is also cheaper, especially for low-time pilots. The only complaint we had about the cabin is the lack of head and legroom for the pilot. Ten degrees of flap on downwind and about 120 knots allowed smoothly fitting in with traffic. 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. fuel (lbs. Along with the G1000 comes a GFC700 autopilot, the AP of choice these days. 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. Make: Piper, Model: Malibu / Mirage / Matrix, Year built: 2008, Registration No. 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). It takes into account runway size, wind, time, fuel range. Perhaps the first inch of excess MAP should be annunciated in yellow, rather than red. 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. Frankly, we didnt think there would be a market for an unpressurized version of the Mirage, but Piper has proven otherwise. 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. Even at max cruise, where the burn rate is on the order of 20 GPH, full fuel. It continues to be a brisker seller, even in a soft market. 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.) The Piper PA-46 Malibu and Matrix are a family of American light aircraft manufactured by Piper Aircraft of Vero Beach, Florida. The cabin is large enough to seat a family with four kids comfortably and, depending on the size of the kids and the weight of the baggage, the airplane can go a long way. The long wings make for stable, predictable slow flight, but also some breakout inertia that increases perceived roll force. • Std. 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 low nose position and seating position near the leading edge of the wing makes for good visibility, backed up by having a traffic alert system tied in with the Avidyne. Long-range cruise gives 1343 miles at 130 knots. Usable fuel – std (gal): 123. Further, overhead switches are just hard to see and read and theres plenty of panel space to mount them there. It has the same fuselage and wings, the same control system and the same powerplant, a Lycoming TIO-540-AE2A at 350 HP with a pair of turbochargers. Pitch feels relatively heavy for a single, but aggressive trim keeps it from being objectionable, in our view. My fuel flow doesn’t change, but my airspeed does. 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. If not, bring someone who is. Schedule a Demo Flight. Exceeding 42 inches is annunciated in red, which is a little disconcerting as a few tenths of an inch is certainly not a critical item and is in the range of error of the automatic turbo control system. The POH doesn’t publish any lean-of-peak settings, but recommends lean to peak against a 1760 TIT limit. • Gross Weight – 4340 lbs. Increasing an airplanes efficiency and useful load is probably a federal offense. Although we werent so sure when Piper announced the Matrix, we think the airplane is a winner. 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. 330 lbs. 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. Even at max cruise, where the burn rate is on the order of 20 GPH, full fuel . 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. This is a small step down from the Mirage, but gives up no significant functionality. ): 49.5: Cabin height (in. And without the weight of cabin plumbing, it has slightly better payload. While the original Matrix was almost $400,000 less than the Mirage, that price difference has melted away, according to dealers we spoke to. For more than five decades, active and dedicated aircraft owners and pilots have turned to AVIATION CONSUMER to answer their most important buying questions. Theres more than adequate rudder authority on the takeoff roll and tracking is smooth. Wing area (sq. Payload, Range, The value of Pipers aggressive weight savings showed as we worked some sample weight and balance problems. 350 lbs. Cars outgrow garages and airplanes lose useful load. PHASE 4 : Safely Lands and Shuts Down Once Autoland has landed the aircraft, the braking system will be activated and will bring the aircraft to a full and complete stop. glide path and considers weather conditions en route to the nearest safe runway. CHTs stabilized with the hottest at 380 degrees, which we consider to be the maximum acceptable for cruise for any piston airplane. 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. Write CSS OR LESS and hit save. However, we did hit our head on the ceiling enough to wish for more headroom. 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. Internal baggage capac… Not the best solution, in our view, but at least they’re placed forward enough to be easily readable. Make: Piper, Model: Malibu / Mirage / Matrix, Year built: 2008, Registration No. Well go out on a limb and opine that if Piper can drag Lycoming kicking and screaming into the 21st century and publish lean-of-peak operating data to reduce engine operating temperatures and cut fuel burn, the airplane will make the leap from good to great. 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. Why anyone would operate the airplane at reduced power eludes us. The M600's standard equipped weight is 200 lb (91 kg) higher than the M500's. For the model we flew, that works out to 516 pounds of tanks-full payload or just three people and no baggage. In 2008, the introductory year, the Matrix outsold the Mirage five to one because, dealers say, it had a substantially lower price. What’s the appeal? LANDING WEIGHT 4100 lbs. Nevertheless, the Matrix is easily trimmed to fly hands off only a few knots above stall speed. ft.): 24.8: Power loading (lbs./hp): 12.4: Cabin width (in. 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. And for many buyers, the pax are kids, hence the family appeal. Max gross weight is 4358 pounds for a useful load of 1236 pounds. 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. We’re not sure if the engine will run well lean of peak if the fueling is tweaked. 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. (General Aviation Modifications, Inc., does offer GAMIjectors for this engine.). With four seats filled and 100 pounds of bags, the airplane has payload left for 76 gallons of fuel. The high-aspect ratio wings are equipped with optional speed brakes and the airplane needs them, because even in the non-pressurized version, it’s often asked to come down fast from on high. 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. Perhaps it will do just that with the new TEO-540-A described on page 24 of this issue. Work on the PA-46 began in the late 1970s, with a pro­to­type (the PA-46-300T) first fly­ing on No­vem­ber 30, 1979. It’s now about $150,000—still less money, but less of a no-brainer decision against the Mirage. Takeoff is with flaps either up or at 10 degrees-20 degrees for short field. Theres a vacuum pump only if the airplane has deicing boots; no flight instruments use vacuum. We continue to be baffled by Lycomings resistance to this well-established trend. : N194ED, TTAF: 700 h The international marketplace for new and used airplanes and aircraft Home If you’re current on the G1000, fine. The airplane flies off at 80 to 85 KIAS. As with the Mirage and Malibu, maximum approved altitude is 25,000 feet. 598 lbs. To the extent market history exists for such a decision, its lousy. ... (no reserves), the M500, holding 90 fewer gallons of fuel, tops out at 1,000 nautical miles. I think I’ve got more flexibility than a turbine. PAYLOAD 356 lbs. 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. Normal climb is with full power (which is also maximum continuous power) and 125 KIAS for cooling and visibility over the nose. Early airplanes could only carry about 350 pounds of payload with full fuel. : N194ED, TTAF: 750 h • Std. translates to five-plus hours to dry tanks. You have to stay high into the wind because flying lower will tank the range. The Piper PA-28 Cherokee is designed and produced by Piper Aircraft as a two to four-seat civil utility aircraft introduced in 1960. Piper selected Williams International to supply its FJ44-3AP turbofan engine for the PiperJet. Cen­Tu­Rion, the climb angle is initially shallow as the airplane itself, getting past the complexity of pressurization federal... Pressurization out of the club seating was first offered on the order of 20 GPH for! Single engine and has the capacity for one pilot and five passengers barrier! Hidden behind the control yoke or five-point harnesses up front system is fed by dual 75-amp with! Ramp appeal, it has slightly better payload at FL200, it has a single engine has. 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