Full-fuel payload for the M600 is 645 lb (293 kg) compared to 550 lb (250 kg) for the M500. Fit and Finish. Increasing an airplanes efficiency and useful load is probably a federal offense. Are you interested in scheduling a demonstration flight in an Evolution aircraft? 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 interior alone will sell the Matrix to a lot of non-flying spouses. 100/100 lbs. Simplifying an American vehicle is not acceptable. To the extent market history exists for such a decision, its lousy. At FL200, it will true about 195 knots at normal cruise or 150 knots at economy cruise. The Malibu Matrix PA-46R-350T produced by Piper. 4100 lbs. Performance Parameters and Weights: Cruises FL120 with 185KTAS using 18GAL/h 1000nm IFR range plus reserve or 1100nm range VFR. Work on the PA-46 began in the late 1970s, with a pro­to­type (the PA-46-300T) first fly­ing on No­vem­ber 30, 1979. 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. With all 720 pounds of fuel in the tanks, 567 pounds of people and stuff can go into the cabin. The boards make that practical without reducing the engine to a cylinder-chilling idle. Make: Piper, Model: Malibu / Mirage / Matrix, Year built: 2008, Registration No. 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. As with the Mirage and Malibu, maximum approved altitude is 25,000 feet. Even at max cruise, where the burn rate is on the order of 20 GPH, full fuel. It takes into account runway size, wind, time, fuel 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. Pitch feels relatively heavy for a single, but aggressive trim keeps it from being objectionable, in our view. To the extent market history exists for such a decision, its lousy. Closer inspection reveals the absence of a forward pressure bulkhead and a 13 cubic foot nose baggage area limited to 100 pounds. Piper unveils its take on a turbocharged, four-place single—with two extra seats. 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. For the model we flew, that works out to 516 pounds of tanks-full payload or just three people and no baggage. LANDING WEIGHT 4100 lbs. However, we did hit our head on the ceiling enough to wish for more headroom. The rules clearly state that automobiles and airplanes are to get bigger, heavier, more complicated and less efficient as the production years pass. Visibility over the nose is good and the airplane climbs at 700 FPM. ): 669: Wingspan (ft.): 43: Overall length: 28 ft. 11 in. 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. Fill out the form below and the Evolution team will get back to you. Takeoff is with flaps either up or at 10 degrees-20 degrees for short field. My fuel flow doesn’t change, but my airspeed does. Piper Malibu Matrix. 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. Cabin, FlightThe Matrix comes into its own as a luxury liner immediately on ingress. 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. • Std. 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. Wing area (sq. On takeoff, the airplane holds the centerline like it’s on rails and at 80 indicated, a healthy tug pulls it off. Theres more than adequate rudder authority on the takeoff roll and tracking is smooth. Piper Matrix: The Pressure Is Off. 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.) We believe this hamstrings Piper; the company is clearly sophisticated enough to recognize the value of lean-of-peak operations. 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). 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 Go look it up. 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. Piper took a risk in creating a simplified, unpressurized version of its decades-old Malibu/Mirage. 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. Beech Bonanza vs. Piper Matrix. The Piper PA-46 Malibu and Matrix are a family of American light aircraft manufactured by Piper Aircraft of Vero Beach, Florida. 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. Engine • Turbocharged Lycoming TIO -540-AE2A • 350 HP • 6 Cylinder Propeller • Hartzell 3-Blade • Composite • Constant Speed Fuel Capacity • Usable: 120 Gals. High-performance aircraft are typically hobbled by low gear and flap speeds. • 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. The rules clearly state that automobiles and airplanes are to get bigger, heavier, more complicated and less efficient as the production years pass. Not the best solution, in our view, but at least they’re placed forward enough to be easily readable. 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. 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 288 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. And without the weight of cabin plumbing, it has slightly better payload. As has been our experience with current production Pipers, speed was exactly on the book while fuel flow was one GPH higher than book. We observed the climb rate to stabilize at just over 1100 FPM and the airplane to fly hands off. Thats enough fuel for a two-hour VFR trip at long-range cruise. What we mistakenly discounted was the large price Delta between the two models. glide path and considers weather conditions en route to the nearest safe runway. If a buyer could afford an expensive cabin-class single, who would opt for a non-pressurized version over one with pressurization? There are two baggage areas: a large one in the nose and a smaller one aft of the rear seats. Payload, Range. The airstair is wide and easy to enter and the two rear seats are easily accessible. Piper took an existing design and adapted it for their non-pressurized version. The long wings make for stable, predictable slow flight, but also some breakout inertia that increases perceived roll force. Piper has adhered to the secret of general aviation marketing: Find a niche and fill it before someone else does. Overall height: 11 ft. 4 in. Getting into the cockpit is a squeeze, especially for tall pilots or those large of girth. 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. The first notch of flaps can go out at 165 knots, too. "The PiperJet Altaire is a powerful and stylish blend of efficiency, cabin volume, range, payload and speed," Berger says. The lower price is one, but the Matrix delivers equivalent performance to the Mirage, without the complexity of pressurization. Why anyone would operate the airplane at reduced power eludes us. 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. What’s the appeal? Piper doesnt give percentage power settings, but rather “high-speed, normal, economy and long-range” cruise power settings. 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. Piper Malibu Mirage Performance and Specifications . 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. The airplane flies off at 80 to 85 KIAS. 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. In southern climates, this is almost a must-have because unlike other singles, you can’t open a door to drink in the prop blast. Westbound in the winter in a 260-knot turbine is just painful,” Jones says. At 16,500 feet, we observed 196 KTAS on 21 GPH. Piper hit on a winning formula when it yanked the pressurization out of the Mirage. With four seats filled and 100 pounds of bags, the airplane has payload left for 76 gallons of fuel. Early Malibus were all piston-engined, but a turboprop version, introduc Maximum range was expected to be 1,300 nautical miles (2,407.6 km), with a full-fuel payload of 800 pounds. Useful Load – 1421 lbs. 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. It has a single PFD and MFD, supported by dual Garmin GNS430Ws, with XM weatherlink and an S-TEC 55X autopilot. 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). The long nose made picking a precise pitch attitude easier than in most airplanes, so maneuvering proved enjoyable, especially with the crisp roll rate. This is a small step down from the Mirage, but gives up no significant functionality. The only complaint we had about the cabin is the lack of head and legroom for the pilot. To create the Matrix, Piper cut both weight and price. 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. The landing gear is hydraulic, with free fall backup. It continues to be a brisker seller, even in a soft market. Normal climb is with full power (which is also maximum continuous power) and 125 KIAS for cooling and visibility over the nose. 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. We found the cabin load versus fuel tradeoff to require less compromise in the Matrix than in many other piston airplanes. Write CSS OR LESS and hit save. 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. • Usable Fuel – 120 gals./720 lbs. 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. This website contains many older reviews. It’s now about $150,000—still less money, but less of a no-brainer decision against the Mirage. including metal bars over the starter and mag switches. I think I’ve got more flexibility than a turbine. Ten degrees of flap on downwind and about 120 knots allowed smoothly fitting in with traffic. The Piper Matrix is un-American. 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. While there isnt a potty, there is a relief tube. Cars outgrow garages and airplanes lose useful load. It takes longer and requires more fuel to climb to any altitude at reduced power. Like the Cen­tu­rion, the Mal­ibu was to fea­ture cabin pres­sur­iza­tion (5.5 psi), a fea­ture not in­cluded on the pro­to­type. 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. Despite the current economic downturn, it appears the decision was a winner. Nor do we understand the continued use of yokes instead of side sticks, again, for safety reasons. 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. If you’re current on the G1000, fine. But once the muscle memory is ingrained, it’s doable. Piper also spent money on market surveys to assess demand for the proposed airplane as well as the right price point. There is a zero fuel weight- the maximum load that can go in the cabin-of 4123 pounds. He lives in Denver. 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. The Matrix/Mirage cockpit has come a long way in 28 years. While the original Matrix was almost $400,000 less than the Mirage, that price difference has melted away, according to dealers we spoke to. The POH doesn’t publish any lean-of-peak settings, but recommends lean to peak against a 1760 TIT limit. 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. Its such a well-thought-out system that we would be surprised if a pilot is ever unable to lower the gear. Even at max cruise, where the burn rate is on the order of 20 GPH, full fuel . 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. If not, bring someone who is. 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. ft.): 175: Wing loading (lbs./sq. We continue to be baffled by Lycomings resistance to this well-established trend. Piper selected Williams International to supply its FJ44-3AP turbofan engine for the PiperJet. (The reviewing pilot is 6-feet-4 inches tall.). Along with the G1000 comes a GFC700 autopilot, the AP of choice these days. • Payload (w/full … Go look it up. PAYLOAD 356 lbs. 598 lbs. Early Malibus were all piston-engined, … That makes it a definite head-down to use, but its functions can be duplicated with knobs and keys on the main screens. © Belvoir Media Group, LLC. 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. During climb, we found the S-TEC autopilot accurately held selected rates of climb, which were easily programmed through the integrated Avidyne system. 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. Its maximum payload is 1,200 pounds, and full fuel is 1,768 pounds. Max gross weight is 4358 pounds for a useful load of 1236 pounds. : N194ED, TTAF: 700 h The international marketplace for new and used airplanes and aircraft Home The Matrix is essentially identical to the Mirage. 04 Feb 2010, 14:28. “If I need to stay low because of the wind, I can do that. From a crashworthiness standpoint, all seats have three-point harnesses and the fuel tanks are well out in the wings. Before you can fly a Matrix, you have to taxi it. 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. We were surprised not to find some positive lockout from the left to the off position, making an inadvertent fuel shutoff possible. 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. As a result, it has a great air conditioner that cools the cabin quickly. Ever since club seating was first offered on the Cherokee 6, Piper has made passenger-friendly cabins and continues the tradition here. The air conditioning in the airplane we flew was welcome on a hot Florida day in August. 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. CTRL + SPACE for auto-complete. Simplifying an American vehicle is not acceptable. 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. 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. Max ramp weight 1976kg/4358Ibs MTOW 1968kg/4340Ibs EW 1393kg/3072Ibs Maximum useful load 583kg/1285Ibs Maximum usable fuel 453l/120GAL Payload with full fuel 257kg/566Ibs Perhaps it will do just that with the new TEO-540-A described on page 24 of this issue. Fuel capacity: 120 GAL. lean-of-peak operational data in the POH because Lycoming wont authorize it. 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. All four of the club seating chairs recline and the rear seats individually fold forward to reach the rear baggage area. In 2008, the introductory year, the Matrix outsold the Mirage five to one because, dealers say, it had a substantially lower price. 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. Not the Matrix. Piper Matrix: Strong Performer, Good Value, 200-Knot Buzzkill: MX, Insurance Realities. Ownership costs ... Find and Compare PIPER PA-46 for sale Also Consider. 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. Internal baggage capac… CHTs stabilized with the hottest at 380 degrees, which we consider to be the maximum acceptable for cruise for any piston airplane. It was an unpressurized light aircraft with an all-metal structure, single-piston engine, low wings, and tricycle undercarriage. Empty Weight – 2937 lbs. 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. fuel (lbs. All rights reserved. Pilot qualification and insurance may determine which way the deal goes. 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. The aircraft is powered by a single engine and has the capacity for one pilot and five passengers. Cirrus owners stepping up—depending on the model—aren’t getting much of a speed bump in the Matrix. 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. This website contains many older reviews. We climbed to 12,000 feet and found the airplane cruised a bit above book on a warmer than standard day: about 187 knots and 19 GPH. Still, Piper managed to move 33 airplanes in 2009 and another 23 in the blackest recent year, 2010. BAGGAGE CAPACITY 30/100 lbs. The lines in the graphs should be longer to make them usable. 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. 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. Performance Parameters and Weights: Cruises FL120 with 185KTAS using 18GAL/h 1000nm IFR range plus reserve or 1100nm range VFR. Were impressed. Insurance is also cheaper, especially for low-time pilots. Rick Durden is an Aviation Consumer contributing editor. At economy settings, fuel consumption drops to as little as 11 GPH, for a 40-knot give-up in speed. To mount them there G1000 has a single engine and has the capacity for one and... 24.8: power loading ( lbs./hp ): 669: Wingspan ( ). With XM weatherlink and an S-TEC 55X autopilot werent so sure when Piper first announced their,... 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