1 - 19 We use cookies to help you get the best experience when using our website. In order for the cabin to withstand an internal pressure greater than that of the outside air, the fuselage must be beefed up, thereby adding extra weight to the basic airframe and reducing useful load. If flown at the same 25,000-foot altitude, the 340’s 4.2-pound differential would allow a cabin height of just more than 11,000 feet. Pressurization exacts a considerable cost, not only in dollars, but in performance and payload. Aside from its ramp appeal, it has a high-flying pressurized cabin, 200-knot cruise speed and its impressive range. https://www.facebook.com/PiperOwnerSociety?fref=ts. Please send us your experiences on your aircraft. However, that didn’t stop Cessna from selling almost 900 of the little devils over the model’s nine-year life. The Piper Malibu is a single turbocharged engine, non-pressurized, produced by Piper from 1984 until 1988. The lower cabin altitude is an excellent idea, considering that many people (especially smokers) experience some hypoxia above 8000 feet. The test airplane had a full-fuel payload of more than 650 pounds. It was, after all, the first all-new general-aviation airplane in at least a decade. Without pressurization or oxygen in my Turbo Mooney, I could have headed east to Albuquerque at 13,500 feet VFR and had an easy 5000 feet of terrain clearance most of the way. Piper Malibu Matrix Aircraft Information. The Piper PA-46 Malibu and Matrix are a family of American light aircraft manufactured by Piper Aircraft of Vero Beach, Florida.The aircraft is powered by a single engine and has the capacity for one pilot and five passengers. Specifications & Performance – 1984 Piper Malibu, Used Price: $220,000, Engine make/model: Cont TSIA-520BE, TBO – hours: 2000, Fuel type: 100LL, Propeller: 3-blade, CS, Landing gear type: Tri/Retr, Gross weight (lbs): 4100, Useful load – std. Empty Weight: 2460 lbs. 1. Another advantage of choosing the LGB-ABQ hop to test the Malibu’s flexibility was that I could load the airplane with six people and still have plenty of fuel reserve. Running the pressurization system drains power from the engine and results in less torque at the prop, meaning lower thrust and slightly reduced performance. • Maximum Ramp Weight: 4,358 lbs. On my flight eastbound, I also benefitted from prevailing winds. This aircraft is listed for $298,310, the average historical price for aircraft like this is $1,199,073. Singles also have a natural advantage over twins when it comes to range. Since my load of people totaled about 850 pounds, I knew I’d have to leave 200 pounds of fuel behind. Then too, I would have had to settle for probably 30 knots less speed at the lower altitude with less turbo advantage and calmer winds. 2.0 He has authored more than 2,200 magazine articles and was the on-camera host of the 1980s TV series “ ABC’s Wide World of Flying.” Bill is currently rated Commercial/Multi/Instrument/Seaplane/Glider/Helicopter. Rather than try to adapt an existing airframe to compete with the P210, the Vero Beach-based company elected to build a new airplane from the ground up. If a pilot wasn’t a smoker and was in good shape, he could climb on up to 23,000 feet to grab a tailwind or top Mt. The cruise speed is 196 knots (226 mph, 363 km/h), stall speed is 58 knots (67 mph, 108 km/h), and maximum speed … Our mission is to empower the end-users, the aircraft owners and pilots. Passionate about aviation. Pumping the cabin up to 5.5 psi allows the Malibu to maintain a sea-level cabin at 12,000 feet, after which the cabin will gradually climb to 8000 feet as the airplane ascends to 25,000. (18.0 gallons/hr @ $5.40/gal), Misc: landing, parking, supplies,catering, etc, Typical Price: $288,516.00 Wing span: 43 ft Length: 28 ft 4 in Height: 11 ft 3 in Avionics. You start to feel your age a little when you can clearly remember the introduction of an airplane that’s now 21 years old. Often considered the ultimate creature comfort for aviators, a properly functioning pressurization system eliminates the need for oxygen masks above 12,500 feet, allowing a pilot to fly nearly as high as he wishes in relative comfort, while breathing low-altitude air. Like most six-place singles, especially pressurized ones, the Malibu won’t carry full tanks and full seats. While it’s true they’d still be there for the trip home, I had the option of selecting a lower altitude to minimize the speed loss. ( (Several years ago, NBAA surveyed its members and found to its surprise that the average trip length was only 360 nm.). Fuel burn was only 41.2 gallons. Night and peripheral vision are particularly susceptible to oxygen deprivation, so much so that the ultra-conservative feds suggest pilots and passengers alike breathe supplemental O2 at night above 5000 feet. 0 As the entry-level pressurized twin, it has a deserved strong following among business fliers. While the “Crowded Skies” phenomenon is a myth over perhaps 90 percent of the United States, there’s little question that the deserted middle altitudes between 15,000 and 25,000 feet are a nice place to visit. Range: 1261 nm. This listing was posted on Jun 03, 2020. Asking Ted's question one more time, are there any PA46-350s (aka Malibu Mirage and came from Piper with a Lyc TSIO540) that have been converted to TCM IO550 power? Yet Piper prospered with the Malibu because of its unique capabilities and unusual luxury. 9 9-64 Revised Supplement number (cont.) He can be contacted via email at flybillcox@aol.com. ) At the maximum operating altitude of 23,000 feet, cabin altitude was typically at (or slightly above) the 12,500-foot height at which FAA recommends supplemental oxygen. When the winds were good, the airplane could fly 1780 nm nonstop across the Atlantic from Gander, Newfoundland, to Shannon, Ireland.). It has a maximum payload of 660 kg and a fuel capacity of 120 gallons. Date: 20-AUG-1984: Time: 14:00: Type: Piper PA-46-310P Malibu: Owner/operator: Piper Aircraft Corporation: Registration: N4371Y: C/n / msn: 46-8408082: Fatalities: Cruise Speed: 187 kts. As mentioned, “normal” 75-percent cruise consumes exactly 16 gallons, and 65 percent results in 14 gph, so a setting of 70 percent would burn 15gph. What needs to be done? - Send us pictures of your plane. 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