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Piper PA-46 Malibu and Mirage Engine Conversion

Piper PA-46 Meridian · Supplemental Type Certificate

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Overview

This document discusses the conversion of the Piper PA-46 Malibu to a more powerful engine, specifically the Continental TSIO-550C. It details the performance characteristics of the conversion compared to the original engine, the TSIO-520-BE, and highlights the benefits and drawbacks of the upgrade. The document is aimed at pilots and aviation enthusiasts interested in the technical aspects of the PA-46 series and the implications of engine modifications. It provides insights into the operational performance, fuel consumption, and handling characteristics of the modified aircraft, as well as the installation process and costs associated with the conversion.

  • The Piper PA-46 Malibu can be converted to a TSIO-550C engine for enhanced performance.
  • The conversion maintains a maximum power output of 310 hp at 35.5 inches of manifold pressure.
  • Fuel consumption increases by about 24% compared to the original TSIO-520-BE engine.
  • Climb performance is improved, with a rate of climb of 1,000 fpm at 125 KIAS.
  • The conversion cost is approximately $57,000.

Document

Source

Originally published by aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Supplemental Type Certificate
Year
1994
Pages
6
File size
5.6 MB
Publisher
aeroresourcesinc.com
Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the Piper PA-46 Meridian.

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In this document

Engine Conversion Overview

The document outlines the conversion of the Piper PA-46 Malibu from the 310-hp Continental TSIO-520-BE engine to the 350-hp Lycoming TIO-540-AE2A engine, which has been rebranded as the Mirage. The conversion aims to enhance performance while maintaining similar weight and balance characteristics.

Performance Comparison

The TSIO-550C engine is limited to 310 hp for the conversion, achieving this at 35.5 inches of manifold pressure and 2,600 rpm. This engine provides more usable horsepower at lower power settings compared to the original 520 engine, which operates at 100% power at the same output.

Fuel Consumption and Efficiency

The TSIO-550C engine consumes approximately 24% more fuel than the TSIO-520-BE at equivalent power settings. However, it can be operated at lower power settings to match the fuel efficiency of the original engine, thus preserving range and endurance.

Climb Performance

Recommended climb power setting for the modified Malibu is 33.5 inches and 2,500 rpm, with a fuel consumption of 32 gallons per hour. The rate of climb is approximately 1,000 feet per minute at 125 KIAS up to 10,000 feet.

Cost of Conversion

The cost for the engine conversion is approximately $57,000, which includes a factory-new engine, new mounts, and the supplemental type certificate. This is compared to a factory-overhauled TSIO-520-BE engine priced at $42,256.

Safety notes

  • Monitor throttle to avoid exceeding the 35.5-inch manifold pressure limit during takeoff.

Full document text

92 • APRIL 1994 PHOTOGRAPHY BY ALTON K. MARSH AND BARRY GROSS and some of those were very lean pro- duction years-Piper Aircraft's PA-46 Malibu already has undergone one significant round of factory modifica- tions. This was when Piper switched from a 310-horsepower Continental TSlO-520-BE engine to a 350-hp Lycoming TIO-540-AE2A, cleaned up the instrument panel, and freshened the interior design. The re-engined Malibu was renamed the Mirage. The Mirage is faster but at the expense of higher fuel consumption and greater empty weight. Now the aftermarket is eying the pre-Mirage Malibu. Not surprisingly, power and speed are the focus-tur- bine power (Piper tried it), liquid- cooled power (RAM wants to do it), and just plain more power. Henry Van Kesteren, a longtime fixed-base operator who now has a modification shop at Albert Whitted Municipal Air- port in St. Petersburg, Florida, has opted for the latter approach. His Continental TSIO-550C-powered Malibu conversion has been approved by the Federal Aviation Administration under a supplemental type certificate, and he has sold and delivered the first example, the air- plane you see pictured here. Van Kesteren has taken a middle- of-the-road approach with his con- version, achieving something that has the performance characteristics of both the Malibu and the Mirage. The twin-turbocharged, twin-inter- cooled 550C engine is rated at 350 hp, but in Van Kesteren's Malibu conver- sion, it is manifold pressure limited to 310 hp, the same as the 520-BE engine it replaces. Maximum power in a standard 520-powered Malibu is achieved at 38 inches manifold pres- sure and 2,600 rpm. The 550 delivers the same 310 hp at 35.5 inches and 2,600 rpm. If the larger engine is limited to the same maximum power output as the one it replaces, what then is the advantage of the conversion? The answer lies in the percentages. The 550 achieves its 310 hp at about 88.6 percent of maximum rated power. At 310 hp, the 520 is delivering every- thing it's got-100 percent. Reduce power to 75 percent for cruise, and with a 520, you'll have 232 horses pulling for you. The 550 delivers 262 hp at 75-percent power. The bottom line: Even with the 310-hp limitation, there's more usable horsepower available from the 550. Because there is no such thing as a free power lunch, the bill for the 550's extra punch is in fuel consumption. It takes fuel to produce power and more fuel to produce more power. At the same percentage of power, the 550 consumes about 24 percent more fuel than the 520. That affects endurance and range. Of course, with the 550 you have the option of reducing power to achieve the same horsepower and fuel flow as a 520, thereby preserving orig- inal endurance and range perfor- mance. In fact, it's likely that the 550 is a bit more efficient than the 520 given its "volumetric efficiency" and other esoteric features understood only by people gifted with internal combustion insight. But why buy more power if you're not going to use it? The 550 Malibu likely will be flown the same as a Mirage: Bump up the •Even with the 310-hp limitation, there's more usable horsepower available from the 550. throttle to a go-fast setting on shorter trips when endurance or range are not concerns, and go for lower power settings and lower fuel consumption on those continent-crossing trips. The differences between the 550 and 520 are all internal. The 550 has a longer piston stroke and thus a differ- ent crankshaft and piston skirts, and it uses a single-stage engine-driven fuel pump rather than the more expensive two-stage pump on the 520. Like the 520, the 550 has dual alternators and vacuum pumps and a 2,000-hour time between overhauls. The 5.5-psi pressurization differential is unchanged with the conversion. Engine dimensions, weight, and con- figuration (where the accessories are mounted) are the same, so it's a rela- tively easy conversion to perform. No changes are required to the cowling, and weight and balance is unaffected. The manifold pressure gauge is altered to reflect the lower maximum limit of 35.5 inches. Van Kesteren's first 550 conversion is a 1985 Malibu. The previous owner, AOPA PILOT • 93 94 • APRIL 1994 Larry Lee, flew it in the 1992 around- the-world air race and also installed some new interior appointments developed by his company, Plastek, including attractive Mirage-style pull- down window shades. Van Kesteren bought the airplane after it was involved in a minor land- ing accident. He repaired the damage (a collapsed gear), performed the engine conversion, and installed Spoilers, Incorporated's hydraulically actuated spoilers in the wings. The air- plane has been sold to Lyle Kallis, a contractor in Red Deer, Alberta, Cana- da, near Calgary. Kallis and a friend, along with Van Kesteren, stopped by AOPA in Frederick, Maryland, on their way back to Canada to give us an opportunity to fly the airplane. No question, a Malibu is beautiful in almost every respect. It stands higher and wider than any other sin- gle on the ramp and many twins, as well. Its big-airplane character is accentuated by the airstair door and the fact that you pass through the passenger cabin-albeit hunched over-to get to the cockpit. The Malibu's attributes-cruise performance, pressurization, the long and wide cabin, and its commanding presence-are responsible for its resurgence in the used airplane mar- ket. After the rash of Malibu/Mirage in-flight structural failures between May 1989 and March 1991 and the National Transportation Safety Board / FAA investigation that fol- lowed, used Malibus dropped as much as $50,000 each in value. How- ever, the federal investigation did not find fault with the airplane's struc- ture, and today, prices for used Mal- ibus are back almost to normal levels.

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One dealer quoted current prices ranging from $260,000 to $350,000 for low-time Malibus built between 1985 and 1988 (the last year for the 31O-hp version; the Mirage appeared in 1989). Asking price for a new Mirage is about $658,000. Van Kesteren repainted his Mal- ibu and, at Kallis' request, installed a Shadin fuel totalizer-a worth- while addition given the nonstan- dard fuel flows. The Malibu holds 120 gallons of usable fuel and has a maximum take- off weight of 4,100 pounds. When the Malibu Van Kesteren converted was first registered in 1985, it weighed 2,777 pounds empty, and it has only gained 58.8 pounds since. With full fuel, the airplane can handle 544 pounds in the cabin. For our flight, the tanks and seats were half-full, so we were about 410 pounds shy of maximum takeoff weight. The takeoff is more work intensive than in a standard Malibu because the throttle has to be monitored to avoid exceeding the 35.5-inch mani- fold pressure limit. On the plus side, there is no turbo lag as you add power; they spool up instantly. We spent the first part of the flight at low altitude, droning around in circles for air-to-air photos. When that was over, we bade the photo platform ship, a Piper Saratoga, farewell and set climb power. Air traffic control cleared us in steps to 25,000 feet, the Malibu's maximum operating altitude. Recommended climb power set- ting is 33.5 inches and 2,500 rpm. With the mixture at full rich, the engine took in 32 gallons of gas per •Where the 550 conversion has a distinct edge... lSln englne temperatures. hour. Rate of climb at 125 KIAS ranged from 1,000 feet per minute passing through 10,000 feet to about 500 fpm as we approached our target altitude. This may represent some- what better performance than a stan- dard Malibu, but differences in pilot technique, instrument indications, ambient conditions, and the unique characteristics every airplane ex- hibits make it difficult to make accu- rate comparisons. Where the 550 conversion has a distinct edge is in engine temperatures. The standard Malibu's 520 engine has suffered heat problems since the airplane's inception. Proper setup of the fuel and induction systems can mitigate the problem, but the 550 seems to run far cooler. On our ascent to Flight Level 250, cylinder head tem- peratures (CHTs) hovered around 300 degrees. When we leveled off for cruise and leaned, CHTs rose about 50 degrees. Van Kesteren believes the 550 Mal- AOPA PILOT • 95 If a 550 engine doesn't excite you, try a SSO-sllp PT6. Van Kesteren bought Piper's Malibu prototype and stllck a King Air 890 engine in it. Not available in mass qualltities. and still descend at nearly 2,000 fpm. Van Kesteren's 550 conversion for the Malibu sells for $57,000. That is the installed price for a factory-new engine (provided the 520 engine it replaces is sent to Continental in exchange), new Lord mounts, and the supplemental type certificate. The standard two- blade Hartzell Malibu propeller can be used on the 550. That compares to a list price of $42,256 for a factory over- hauled 520-BE (including exchange). Van Kesteren's conversions are done at his shop in Florida (contact VKLeasing, Incorporated, One Beach Drive, Box 2, S1. Petersburg, Florida 33701; tele- phone 813/898-1921; fax 813/823- 5484), but he said he is willing to con- sider field installations done by experi- enced Malibu service centers. Is the 550 conversion a Malibu or is it a Mirage? The answer is either or both. It weighs no more than a Malibu and can be operated like one using " equivalent horsepower and fuel flows. Or it can be flown like a Mirage: high- er horsepower, higher fuel flow, and the payoff, more speed. It's an inter- esting choice. 0 tings, the 550-powered Malibu will have about an hour's less endurance compared to the standard airplane. The flight manual supplement does not include revised performance, range, and endurance tables, only this cryptic note, "Performance will be equal to or better than a standard Malibu," and the caution that range and endurance are adversely affected if fuel flows are increased over that of a standard Malibu. The spoilers enabled us to descend from the flight levels with ease. Descents from high altitudes in a clean airplane like the Malibu are dif- ficult at best and, to avoid gross power reductions, involve use of flaps and at times even extending the land- ing gear. The spoilers eliminate the worry and the work. With the boards extended, we were able to keep the power and engine temperatures up •Revised performance, range, and endurance tables are not provided. om mend retarding the mixture to achieve a turbine inlet temperature (TIT) that is 50 degrees lean of peak, as Piper and Continental do with the 520. Leaning past peak TIT is neces- sary on the 520 to reduce engine tem- peratures and to avoid exceeding 75- percent power-above which leaning is not permitted, but it has proven to be a controversial procedure. Owners report excessive wear on the exhaust valves, pipes, and exhaust gas temper- ature probes. At high-speed cruise power set- ibu to be the fastest in the PA-46 fleet, and the numbers bear him out. We set the power at 75 percent-31 inches, 2,500 rpm, and about 21 gallons per hour and watched the airspeed needle settle on 149 knots indicated, 230 knots true airspeed. A reduction to 65-percent power resulted in 220 KTASand fuel flow of 17.7 gph. At 16,500 feet, a high-speed cruise power setting resulted in 210 KTAS at 22.4 gph. Van Kesteren takes a conservative approach to leaning. He does not rec- 96 • APRIL 1994 - --------.---- _. --'--------- --- ._---- _._~