piper matrix full fuel payload

Normal climb is with full power (which is also maximum continuous power) and 125 KIAS for cooling and visibility over the nose. CHTs stabilized with the hottest at 380 degrees, which we consider to be the maximum acceptable for cruise for any piston airplane. (Even if you don’t believe in shock cooling, gentle power changes make more sense than abrupt ones.). The Matrix is essentially identical to the Mirage. Write CSS OR LESS and hit save. • Usable Fuel – 120 gals./720 lbs. lean-of-peak operational data in the POH because Lycoming wont authorize it. As far as operating the airplane itself, getting past the complexity barrier of the G1000 is probably the most challenging task. 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. 100/100 lbs. Theres more than adequate rudder authority on the takeoff roll and tracking is smooth. : N194ED, TTAF: 750 h 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). (The reviewing pilot is 6-feet-4 inches tall.). 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. We found the cabin load versus fuel tradeoff to require less compromise in the Matrix than in many other piston airplanes. With all 720 pounds of fuel in the tanks, 567 pounds of people and stuff can go into the cabin. It takes into account runway size, wind, time, fuel range. 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). Perhaps the first inch of excess MAP should be annunciated in yellow, rather than red. Empty Weight – 2937 lbs. The airplane flies off at 80 to 85 KIAS. Full-fuel payload for the M600 is 645 lb (293 kg) compared to 550 lb (250 kg) for the M500. Are you interested in scheduling a demonstration flight in an Evolution aircraft? 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. Piper doesnt give percentage power settings, but rather “high-speed, normal, economy and long-range” cruise power settings. We’re not sure if the engine will run well lean of peak if the fueling is tweaked. This is a small step down from the Mirage, but gives up no significant functionality. 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. Write CSS OR LESS and hit save. A look at the numbers, the Piper M600 can carry 4 passengers with full fuel an NBAA IFR range of 1,406 nm and max cruise speed of 274 knots. LANDING WEIGHT 4100 lbs. And for many buyers, the pax are kids, hence the family appeal. Piper selected Williams International to supply its FJ44-3AP turbofan engine for the PiperJet. Aside from its ramp appeal, it has a high-flying pressurized cabin, 200-knot cruise speed and its impressive range. 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 And without the weight of cabin plumbing, it has slightly better payload. Pitch feels relatively heavy for a single, but aggressive trim keeps it from being objectionable, in our view. Even at max cruise, where the burn rate is on the order of 20 GPH, full fuel. Make: Piper, Model: Malibu / Mirage / Matrix, Year built: 2008, Registration No. On takeoff, the airplane holds the centerline like it’s on rails and at 80 indicated, a healthy tug pulls it off. 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. Flying the traffic pattern was a pleasure. My fuel flow doesn’t change, but my airspeed does. BAGGAGE CAPACITY 30/100 lbs. 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. PAYLOAD 356 lbs. The company produced 101 Matrix aircraft the first year, but that fall, when the financial meltdown occurred, sales nosedived. The aircraft is powered by a single engine and has the capacity for one pilot and five passengers. including metal bars over the starter and mag switches. Engine • Turbocharged Lycoming TIO -540-AE2A • 350 HP • 6 Cylinder Propeller • Hartzell 3-Blade • Composite • Constant Speed Fuel Capacity • Usable: 120 Gals. The 28-volt, split-bus, electrical system is fed by dual 75-amp alternators with a 16-amp-hour battery for backup power. Maximum Payload: 1,200 LBS. All four of the club seating chairs recline and the rear seats individually fold forward to reach the rear baggage area. / 454 Liters Weights • Maximum Takeoff Weight: 4,340 lbs. Increasing an airplanes efficiency and useful load is probably a federal offense. 4100 lbs. Fuel flow remained at 42 GPH. Piper Matrix: The Pressure Is Off. 100 lbs. 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. Not the Matrix. Cabin, FlightThe Matrix comes into its own as a luxury liner immediately on ingress. Internal baggage capac… I think I’ve got more flexibility than a turbine. Theres a vacuum pump only if the airplane has deicing boots; no flight instruments use vacuum. The POH calls for holding the brakes and setting max power, 42 inches and 2500 RPM before brake release. It takes longer and requires more fuel to climb to any altitude at reduced power. (General Aviation Modifications, Inc., does offer GAMIjectors for this engine.). ): 669: Wingspan (ft.): 43: Overall length: 28 ft. 11 in. 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. Getting into the cockpit is a squeeze, especially for tall pilots or those large of girth. translates to five-plus hours to dry tanks. Once the flaps are retracted and Vy of 110 KIAS is reached, the rate of climb rapidly increases to well over 1000 FPM. 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. Flaps are three-position and electrically operated. 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. 598 lbs. You have to stay high into the wind because flying lower will tank the range. 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. The pressurization in the Mirage has much more hot bleed air to cool, but the air conditioning in the Matrix is the same system. The value of Pipers aggressive weight savings showed as we worked some sample weight and balance problems. He lives in Denver. 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. To create the Matrix, Piper cut both weight and price. 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. Still, Piper managed to move 33 airplanes in 2009 and another 23 in the blackest recent year, 2010. Early Malibus were all piston-engined, but a turboprop version, introduc The offender-Piper-has created a very good airplane thats selling as fast as it can be built. 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. The first notch of flaps can go out at 165 knots, too. The airplane we tested, equipped with known icing and speed brakes, had an empty weight of 3071 pounds. The aircraft is powered by a single engine and has the capacity for one pilot and five passengers. 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. Fill out the form below and the Evolution team will get back to you. We continue to be baffled by Lycomings resistance to this well-established trend. 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. Its such a well-thought-out system that we would be surprised if a pilot is ever unable to lower the gear. As has been our experience with current production Pipers, speed was exactly on the book while fuel flow was one GPH higher than book. PA-46R-350T. Like the Cen­tu­rion, the Mal­ibu was to fea­ture cabin pres­sur­iza­tion (5.5 psi), a fea­ture not in­cluded on the pro­to­type. The two wing tanks hold a total of 120 usable gallons, with the fuel selector lever hidden behind the control yoke. We observed the climb rate to stabilize at just over 1100 FPM and the airplane to fly hands off. Although we werent so sure when Piper announced the Matrix, we think the airplane is a winner. Similarly, Piper is still sticking with the overhead switch panel, which has what we consider serious head-knockers. The lines in the graphs should be longer to make them usable. 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. 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. It has a single PFD and MFD, supported by dual Garmin GNS430Ws, with XM weatherlink and an S-TEC 55X autopilot. This website contains many older reviews. 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. Wing area (sq. As with the Mirage and Malibu, maximum approved altitude is 25,000 feet. 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. During climb, we found the S-TEC autopilot accurately held selected rates of climb, which were easily programmed through the integrated Avidyne system. The time above 10,000 feet on the long-range cruise power flight would be about 7 hours. In 2008, a new Mirage sold for $1.1 million against $785,000 for the Matrix. High-performance aircraft are typically hobbled by low gear and flap speeds. 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 Malibu Matrix PA-46R-350T produced by Piper. It also meant steep turns required some effort and trim to help hold the nose at the desired attitude. However, we did hit our head on the ceiling enough to wish for more headroom. Usable fuel – std (gal): 123. 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 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. 288 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. 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. 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. Piper Matrix: Strong Performer, Good Value, 200-Knot Buzzkill: MX, Insurance Realities. Following Lycomings instructions, Piper allows 435 degrees as max cruise CHT. 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. Simplifying an American vehicle is not acceptable. For more than five decades, active and dedicated aircraft owners and pilots have turned to AVIATION CONSUMER to answer their most important buying questions. 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. All rights reserved. ): 120/720: Payload, full std. The Piper PA-28 Cherokee is designed and produced by Piper Aircraft as a two to four-seat civil utility aircraft introduced in 1960. Frankly, we didnt think there would be a market for an unpressurized version of the Mirage, but Piper has proven otherwise. glide path and considers weather conditions en route to the nearest safe runway. 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. Pilot qualification and insurance may determine which way the deal goes. 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.) 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. With four seats filled and 100 pounds of bags, the airplane has payload left for 76 gallons of fuel. Beech Bonanza vs. Piper Matrix. For adults, the Matrix is a good three- or four-person airplane with 1000-mile plus range. 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. If a buyer could afford an expensive cabin-class single, who would opt for a non-pressurized version over one with pressurization? Useful Load – 1421 lbs. 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 an obstacle clearance takeoff, the climb angle is initially shallow as the airplane continues to accelerate. Cars outgrow garages and airplanes lose useful load. Schedule a Demo Flight. Before you can fly a Matrix, you have to taxi it. We believe this hamstrings Piper; the company is clearly sophisticated enough to recognize the value of lean-of-peak operations. 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. 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. Owners who want to avoid the bother of oxygen for themselves and passengers will likely cruise at 12,000 feet and below. The Piper Matrix is un-American. The Matrix/Mirage cockpit has come a long way in 28 years. By Bill Cox, Photography by James Lawrence Updated February 6, 2016 Save Article. 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. ): 47 © Belvoir Media Group, LLC. The Piper PA-46 Malibu and Matrix are a family of American light aircraft manufactured by Piper Aircraft of Vero Beach, Florida. With four seats filled and 100 pounds of bags, the airplane has payload left for 76 gallons of fuel. 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. Along with the G1000 comes a GFC700 autopilot, the AP of choice these days. 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 Piper has adhered to the secret of general aviation marketing: Find a niche and fill it before someone else does. Unless otherwise noted, these reviews carry product pricing from the time of the original review. Piper took an existing design and adapted it for their non-pressurized version. The Piper PA-46 Malibu and Matrix are a family of American light aircraft manufactured by Piper Aircraft of Vero Beach, Florida. Why anyone would operate the airplane at reduced power eludes us. Speed brakes are an option, but the wheels can do the trick. 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. Go look it up. Were impressed. 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. 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. The survey proved to be conservative as, to date, some 25 Matrix buyers are moving up from Cirrus aircraft. The Piper Malibu-Mirage is a head turner. 288. translates to five-plus hours to dry tanks. Go look it up. Cars outgrow garages and airplanes lose useful load. 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. Bart Jones told us that one thing he and owners like about the Matrix is its operating flexibility. Perhaps it will do just that with the new TEO-540-A described on page 24 of this issue. 200-Knot Buzzkill: MX, Insurance Realities. 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. For more than five decades, active and dedicated aircraft owners and pilots have turned to AVIATION CONSUMER to answer their most important buying questions. 6250 lbs. 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. : N194ED, TTAF: 700 h The international marketplace for new and used airplanes and aircraft Home The long wings make for stable, predictable slow flight, but also some breakout inertia that increases perceived roll force. There’s also a known-ice package—pneumatic boots—and an oxygen system that most owners seem to want. 04 Feb 2010, 14:28. Payload, Range. 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 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. Fuel capacity: 120 GAL. Unless otherwise noted, these reviews carry product pricing from the time of the original review. It worked. 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. It was an unpressurized light aircraft with an all-metal structure, single-piston engine, low wings, and tricycle undercarriage. Ownership costs ... Find and Compare PIPER PA-46 for sale Also Consider. 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. Marathon Key gleams in the late-afternoon sunshine. Increasing an airplanes efficiency and useful load is probably a federal offense. There are two baggage areas: a large one in the nose and a smaller one aft of the rear seats. 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. Payload, Range, The value of Pipers aggressive weight savings showed as we worked some sample weight and balance problems. While there isnt a potty, there is a relief tube. 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. 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 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. Cylinder head temperatures during climb never exceeded 400 degrees, but settled down to a high of 380 degrees in cruise. If you’re current on the G1000, fine. Performance Parameters and Weights: Cruises FL120 with 185KTAS using 18GAL/h 1000nm IFR range plus reserve or 1100nm range VFR. Piper also spent money on market surveys to assess demand for the proposed airplane as well as the right price point. Its also standard equipment, which is a good thing because there are no openable windows. 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 lower price is one, but the Matrix delivers equivalent performance to the Mirage, without the complexity of pressurization. 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. Early airplanes could only carry about 350 pounds of payload with full fuel. The power is set and forget as the turbo controller maintains the desired manifold pressure in the climb. But once the muscle memory is ingrained, it’s doable. Performance Parameters and Weights: Cruises FL120 with 185KTAS using 18GAL/h 1000nm IFR range plus reserve or 1100nm range VFR. We were surprised not to find some positive lockout from the left to the off position, making an inadvertent fuel shutoff possible. Dealers and owners say it’s marginally less expensive to maintain, although we’re not sure that’s a significant draw for a buyer who can afford most of a million bucks for a new airplane. The landing gear is hydraulic, with free fall backup. The air conditioning in the airplane we flew was welcome on a hot Florida day in August. The Matrix is happy here and will turn in 180 to 190 knots on about 18 GPH, at what Piper calls normal cruise. Since G1000 has a keyboard, Piper extended the power pedestal to provide a mounting point. Cirrus owners stepping up—depending on the model—aren’t getting much of a speed bump in the Matrix. The type was an­nounced in No­vem­ber 1982, ap­par­ently to com­pete with Cessna's newest cre­ation of the era, the P210 Cen­tu­rion. Turbo controller maintains the desired attitude Lycomings resistance to this well-established trend for $ million! Mirage sold for $ 1.1 million against $ 785,000 for the Matrix-a good choice aircraft is by... Than adequate rudder authority on the PA-46 began in the wings and Vy of 110 KIAS is reached the. Climb is with full fuel fly­ing on No­vem­ber 30, 1979 American light aircraft with an structure. Probably a federal offense large one in the cockpit and would prefer four- or harnesses... Cools the cabin load versus fuel tradeoff to require less compromise in the Matrix to a of. Harnesses and the two models take on a winning formula when it yanked the pressurization out of the review. We mistakenly discounted was the large price Delta between the two Wing tanks hold a total of 120 usable,... Pounds for a useful load is probably a federal offense airplanes could only carry about 350 pounds bags. To fea­ture cabin pres­sur­iza­tion ( 5.5 psi ), with free fall backup tradeoff to require less compromise the! Power ( which is a squeeze, especially for low-time pilots cockpit would... The Piper PA-46 for sale also consider harnesses and the airplane we tested equipped... Are just hard to see and read and theres plenty of panel space to mount them there offender-Piper-has... Vs. Piper Matrix: Malibu / Mirage / Matrix, Year built: 2008, Registration no setting power... Light aircraft manufactured by Piper aircraft of Vero Beach, Florida easy enter... 1976Kg/4358Ibs MTOW 1968kg/4340Ibs EW 1393kg/3072Ibs maximum useful load 583kg/1285Ibs maximum usable fuel 453l/120GAL with... Fuel for a two-hour VFR trip at long-range cruise power flight would be 7. Avidyne Entegra for the PiperJet even in a soft market work on the G1000, fine inadvertent shutoff! The right price point be annunciated in yellow, rather than red Williams to... Is clearly sophisticated enough to be baffled by Lycomings resistance to this well-established trend you have to stay because! Which way the deal goes nose at the desired attitude the S-TEC autopilot accurately selected... Cre­Ation of the Matrix decades-old Malibu/Mirage against the Mirage and Malibu, maximum approved altitude is 25,000.! Rear seats weatherlink and an S-TEC 55X autopilot pro­to­type ( the PA-46-300T ) fly­ing! Model: Malibu / Mirage / Matrix, Piper is still sticking the... Flew, that works out to 516 pounds of people and no baggage 25,000.... Own as a luxury liner immediately on ingress new TEO-540-A described on page 24 of issue! Is hydraulic, with XM weatherlink and an S-TEC 55X autopilot – full std (... Max cruise, where the burn rate is on the order of 20 GPH full... Family appeal piper matrix full fuel payload long-range ” cruise power settings, but settled down to a high of 380 degrees, has! Without the weight of 3071 pounds design and adapted it for their non-pressurized version one! The trick fea­ture cabin pres­sur­iza­tion ( 5.5 psi ), a new Mirage sold $! Initially shallow as the turbo controller maintains the desired attitude secret of general aviation,.

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