For the 1956 model year, the company applied the nosewheel concept to its tailwheel 180 and smaller sibling 170, creating the 182 and 172. Thus began a sales tour de force that continues to this day. Where the 172 became the most popular general aviation airplane in history, the more powerful and capable 182 became the big-engine, reliable, go-almost-anywhere, powerful climbing, carry-almost-anything, good-handling, comfortable old boot that could be found nearly anywhere on the planet where there was space into which to shoehorn an airplane.

In the first decade of manufacture, Cessna fine-tuned the 182 with a wider and deeper fuselage that made the cabin truly comfortable for four, added a panoramic rear window, as well as beginning steady gross weight increases so that what was soon named the Skylane became the utility infielder of the GA world.

• READ MORE: We Fly: Embraer Phenom 300E

The original design was eventually stretched to become the models 205, 206, 207, and, with retractable landing gear, the 210 and retractable 182.

In 1962, Cessna became the first to successfully bring a form of turbocharging to general aviation with its model 320 twin. A turbocharger is an air compressor that pumps more air into an engine, allowing it to develop greater power at higher altitudes than a normally aspirated engine as intake pressure drops with altitude. A turbocharger uses exhaust gas to turn a turbine, to compress and boost intake pressure. When there’s more air entering the engine, more fuel can be added to the fuel/air mixture resulting in greater power.

Turbochargers have been around since World War I, but their complexities and fiery operating environment prevented their widespread use in GA until the Cessna 320 debuted with a system that was reliable and didn’t require a degree in engineering for pilots to operate safely. The 320 sold like mad, so Cessna expanded its turbo offerings.

For the 1981 model year, Cessna turbocharged the Skylane, but with a relatively primitive, fixed-wastegate system that involved significant pilot workload. Nevertheless, it proved popular, outselling the normally aspirated 182 until Cessna’s hiatus on piston-engine production in 1986.

When that production began once more in 1996, the 182 was reintroduced in its normally aspirated form. In 2001, to start out the new century, a new turbocharged 182—the T182—was offered with important updates, including aggressive corrosion-proofing and aerodynamic tweaks to the airframe. Motive force now came from a Lycoming engine with slightly more power, the 235 hp TIO-540-AK1A with 2,000-hour TBO. Most significantly, the turbocharging system was a sophisticated set-and-forget type.

A sloped controller in the system sensed manifold pressure and modulated the wastegate to keep the correct amount of exhaust gas going through the turbine section of the turbocharger to maintain the desired manifold pressure. The wastegate is a valve that adjusts to direct exhaust gas through the turbine section of the turbo until the system decides the amount is appropriate, and then it directs any excess into the overboard exhaust pipe.

There was one more pause in Turbo Skylane production—in 2013—when Cessna explored replacing it with a diesel version. I’ve heard various reasons that the diesel didn’t work out but don’t know if any are true. Cessna, wisely, in my opinion, reintroduced the T182T with deliveries starting in 2023. The newest version included the latest Garmin G1000 NXi avionics suite, a heated prop, and upgraded interior amenities. Max operating altitude is 20,000 feet. Base price is currently $760,000.

As an aside, the first “T” in T182T refers to the Cessna’s way of saying that the flying machine is turbocharged. The second letter designates the specific model (as type certificated) of 182. The first model 182 had no alphabetical suffix—it is called the “no letter.” Each subsequent model change received a new letter, although some letters were skipped. The current normally aspirated 182 is the 182T.

The Basics

The T182T I flew was the first off of the assembly line in the 2023 production restart. It was flown as a demonstrator for 240 hours before being purchased by Phil Preston of Poplar Grove, Illinois. The airplane came with most available options including electric air conditioning, oxygen, and a striking interior.

The T182T’s Lycoming engine is a “max continuous power” engine—it develops its full-rated 235 hp continuously at 32 inches of manifold pressure, 24 gallons per hour (gph) fuel flow, and a quiet 2400 rpm all the way to 20,000 feet. There is no time limit on full-power operation.

• READ MORE: We Fly: Cirrus SR G7

Empty weight of the airplane I flew is 2,191.5 pounds. With a maximum ramp weight of 3,112 pounds (max takeoff weight is 3,100 pounds), it has a useful load of 920.5 pounds. (Cessna’s advertising claims a 998-pound useful load.) Max landing weight is 2,950 pounds, so 192 pounds of fuel (27 gallons) must be burned off following a max-weight departure. Fuel capacity is 92 gallons in the integral wing tanks, of which 87 is usable.

With full fuel—522 pounds—398.5 pounds can be loaded into the cabin. At first blush that doesn’t seem like much for a legendary load hauler like the 182, but the huge fuel tanks make the airplane a camel. At 15 gph, full tanks give well over five hours endurance.

Still, with all the options, this airplane is heavy. Putting four 200-pounders in the cabin means the airplane is over its maximum landing weight without any fuel aboard, so juggling fuel and passengers is required. Assuming having 10 gallons of fuel on board when landing at maximum landing weight after burning off 27 gallons following a gross weight takeoff, the maximum possible cabin load for the airplane we flew is 698.5 pounds, or three large adults and baggage. Maximum baggage is 200 pounds—split between three baggage areas.

Cessna singles have a reputation for some of the longest center-of-gravity (CG) ranges in the industry. The T182T lives up to its reputation. I ran several weight-and-balance scenarios and found that in none of the occupant and baggage combinations I tried was the airplane out of the forward or aft CG limit. That’s impressive.

The fuel system is simple. Two tanks and a fuel selector that offers left, right, and both and off positions. Leaving it on the “both” position means getting all the available fuel and minimizes the risk of selecting a tank that doesn’t have fuel in it. To avoid inadvertently shutting off the fuel, the selector valve must be pushed down before it can be rotated to the “off” position. I was impressed by the accuracy of the fuel gauging system, something important when launching with partial fuel may be routine.

The electrical system is straightforward—dual bus, 28-volt DC, powered by a 95-amp alternator with primary and standby batteries. The standby battery will power the equipment on the essential bus for about 45 minutes.

Walking around this new T182T revealed excellent fit and finish, a beautifully applied paint job and some of the aerodynamic touches made over recent years to maximize speed, such as smaller steps, low-drag wheel fairings, and a low-profile beacon.

The Cabin

Opening one of the large cabin doors, you notice little touches, such as their solid feel and the easy step into the cabin itself. Preston has owned several airplanes, high-wing, low-wing, and biplane. He told us that he chose the 182 because of the ease of entry: “I don’t like climbing up onto a wing to get in and out of the airplane.” He also likes the high wing because he’s loaded and unloaded airplanes in the rain many times and prefers to be able to stay dry.

The seats are delightfully comfortable and adjust far more easily than older 182s to fit a wide variety of pilot sizes and shapes. Cessna has been a leader in GA crashworthiness going back to 1946 when it began offering shoulder harnesses as optional equipment for all seats in its singles, continuing through the 1960s when it did full-scale crash testing and later when it donated some 172s to NASA for its crash research. Where it shows in this new T182T is with the best occupant restraint systems available in general aviation—AmSafe airbag seat belts for all four seats.

• READ MORE: We Fly: Diamond DA62

The clean panel is dominated by the Garmin NXi two-screen display with all controls, switches, and knobs easily accessible to the left-seat pilot.

Flying It

Start-up is not simple. The process, including system checks, takes nearly a minute before the starter switch is engaged. On my flight the engine started easily on the first try, even though it was hot. Preston told me that he has not had any problem with hot starts.

Once the avionics were on, Preston showed how easy it was to load a route into the Garmin NXi system. He said that he appreciated its wireless database and flight plan loading capability.

Taxiing out, I was impressed at how easily the airplane rolled and the lightness of the nosewheel steering—there’s no sense of a heavy engine pressing down on it as there is in older Skylanes. On the hot morning of our flight, I came to quickly appreciate the electric air conditioning. It cooled the cabin rapidly.

I used Cessna’s recommended 10 degrees of flap for takeoff. Lined up, and throttle forward, I monitored the manifold pressure to make sure that it stopped at the 32-inch redline. While the turbocharger control is automatic, if the engine oil is cold, the control can be sluggish, and it’s possible to overboost the engine slightly. If 32 inches is reached before the throttle is fully open, just stop pushing it forward until the control system catches up. Acceleration is rapid, and right rudder is most definitely required, especially once the nosewheel leaves the ground.

The aggressive takeoff performance of the turbo Skylane reminded me that the T182T meets the U.S. Department of Defense’s definition of STOL aircraft right out of the factory—no mods required. At sea level, it will take off or land over a 50-foot obstacle in less than 1,500 feet. Few production airplanes are that capable. For a short field takeoff, 20 degrees of flaps are used.

Cleaned up and holding V_Y, 84 kias, loaded about 200 pounds below gross on a warmer than standard day, the rate of climb approached 1,000 feet per minute (fpm)—book is 1,015 fpm on a standard day. When I pulled the power back to what Cessna calls for in a “normal” climb—25 inches of manifold pressure and 16 gph fuel flow, while maintaining the full 2,400 rpm—the rate of climb sagged off by nearly half. At the suggested 95-knot airspeed, it was only 550 fpm.

Frankly, in my opinion, making a power reduction for climb in an airplane with a max continuous power engine makes no sense. It greatly increases the time to altitude and burns slightly more fuel—according to the POH—than a climb at full power. In addition, in case of an engine failure after takeoff, the higher it happens, the better the radius of action for a forced landing. Using full power and climbing at V_Y, the time to 20,000 feet per the POH is only 23 minutes from sea level and burns 9.2 gallons.

For a “normal” climb, it takes 24 minutes just to get to 12,000 feet and burns 6.3 gallons. Comparatively, at full power and V_Y, it takes 13 minutes and 5.1 gallons of fuel to get to 12,000 feet.

As with all but the oldest Skylanes, control forces on the Turbo Skylane are not light.

However, if sufficient pressure is applied to deflect them, the airplane is quite responsive with a most satisfying roll rate. Pitch forces are heavy, mostly due to the downspring in the elevator system that allows the long CG range. The first rule of thumb when flying a Skylane is to use the trim when any change is made in power or speed. With trim, the Skylane is a pure pussycat to fly—one of the reasons it has been so popular for so long. With trim, steep turns are a piece of cake. The solid stability of a Skylane in slow flight could set the standard for GA aircraft—the T182T proved no exception.

The Garmin Electronic Stability and Protection system kicked in while I was maneuvering (it can be disabled). It is a safeguard to protect the pilot while hand flying. Once the aircraft is rolled beyond a selected angle of bank or gets faster or slower than set speeds, it applies control forces to roll the airplane toward wings level or pitch up or down to control speed. Given that in-flight loss of control is well up there when it comes to risk of fatal accidents, I like this system a lot.

Stalls—hey, what do you want? It’s a Cessna. Power on, power off, full flaps, or clean, it’s a nuthin’ muffin. With the ball centered, it breaks straight ahead. A little pitch reduction, and it’s flying. Adding power (right rudder, remember!) turns any descent into a climb forthwith.

Preston and I then looked at cruise power versus airspeed. As much as I despise the overused phrase “power packed,” that describes this Lycoming engine. For pilots used to maximum cruise at 75 percent power, this engine gets one’s attention because it can be run, and leaned, at as much as 87 percent power—204 hp on a 235 hp engine. At 10,000 feet, the POH quotes a cruise speed on a standard day of 155 knots and 17.8 gph at 87 percent—that’s moving in a 182. At 20,000 feet on a standard day, 82 percent generates 165 knots while burning 16.3 gph.

Some time ago, I was told that Cessna does its cruise speed testing by launching above gross weight so that the airplane is at gross at altitude—and therefore the book speeds will be conservative. For over 40 years I’ve cross-checked book versus actual speeds on new Cessnas, and that’s always been the case.

Descending to 10,000 feet and setting up 75 percent power, at 15 degrees above standard temperature, the book called for 144 ktas. Preston and I saw 145, however, our fuel burn was 13.8 gph versus the book’s 13.6. Want to save some fuel but still move along nicely at 10,000 feet? Pull the power back to 60 percent and get a quiet decent 131 knots at 11 gph. Want to go far? According to Cessna, max range is 971 nm at best economy power.

Leaning leads to an issue that is troubling for an airplane of this sophistication and a useful load that is, let’s face it, not exactly great. Lycoming’s recommended lean mixture setting is 50 degrees rich of peak turbine inlet temperature (TIT). (Lycoming certificated the engine, so Cessna must follow Lycoming protocols.) With what we know now from published data from sophisticated general aviation engine test facilities, 50 degrees rich of peak is not at all good for an engine.

It is the power setting for the highest combination of heat, internal cylinder pressure, and minimum detonation protection—and may necessitate cylinder replacement prior to engine overhaul. For best power, Lycoming calls for 125 degrees rich of peak TIT—which is better for detonation protection. Per the POH, best economy is at peak TIT. That setting is not wonderful because it is still in the range of maximum heat and internal cylinder pressure as well as lower detonation protection.

Lean of peak (LOP) operation is not “approved.” As far as I can tell, it’s not a limitation, so it is a recommendation. Still, it makes no sense to me. Lycoming engines have a reputation for excellent mixture distribution between cylinders and have been run LOP for decades. LOP reduces fuel burn 2 to 3 gallons per hour and dramatically reduces CHTs as well as internal cylinder pressures.

In an airplane that is heavy to start with, having to burn 2 or 3 gph more than necessary isn’t a stellar idea. It means having to carry extra fuel instead of payload. For a trip of several hundred miles, that can mean an extra hour of endurance wasted. To make a good airplane even more capable by reducing fuel consumption, extending engine life and increasing payload, one wonders why Cessna hasn’t leaned on Lycoming to come into this century with engine operating guidelines.

As we flew, I purely enjoyed working with the Garmin automation in the Turbo Skylane. Preston demonstrated that not only did the autopilot engage smoothly, programming it to do what we wanted was easy.

Millions of words have been written about Garmin automation, so I won’t add more here, other than to say it was intuitive, easy, worked well, and seamlessly integrated into the T182T.

Approaching our towered airport, I was asked to keep the speed up until short final. Those are magic words to a Skylane pilot. The T182T smoked down a long final at 150 kias until 3 miles out—then I took advantage of the high flap speeds. The first 10 degrees of flaps can come out at a blistering 140 kias, 20 degrees at 120 kias, and all of them at 100 kias. The airplane slowed so quickly that it was a piece of cake to be stabilized at 60 kias while still several hundred feet up.

I’ve heard pilots complain that 182s are nose heavy. They aren’t. The reality is that with just two aboard, the airplane is near the forward CG limit, so a lot of nose-up elevator is necessary to flare. Plus, if the airplane isn’t trimmed, it’s going to take a lot of effort to heave the yoke aft because of the downspring in the system and the airframe’s attempt to nose down to maintain its trim speed.

The POH says that the demonstrated crosswind level is 15 knots. With the effective flight controls of the T182T, I suspect that number is conservative.

Conclusion

The Cessna 182 became the four-place airplane everyone wanted because it does almost everything well—it’s the SUV of the general aviation world. With turbocharging the T182T takes that utility and performance to new heights and new capabilities, giving a pilot more options and more ability to deal with weather and winds.

Spec Sheet: Cessna T182T Skylane

2024 Base Price: $760,000

Engine: Lycoming TIO-540-AK1A

Propeller: (Manufacturer, metal or composite, number of blades) McCauley, metal, three blade

Horsepower: 235

Length: 29 feet

Height: 9 feet, 4 inches

Wingspan: 36 feet

Wing Area: 174 square feet

Wing Loading: 17.8 pounds per square feet @mtow

Power Loading: 13.19 pounds/hp

Cabin Width: 42 inches

Cabin Height: 49 inches

Max Takeoff Weight: 3,100 pounds

Max Zero Fuel Weight: N/A

Standard Empty Weight: 2,114 pounds

Max Baggage: 200 pounds

Useful load: 998 pounds, depending on options

Max usable fuel: 87 gallons

Service Ceiling: 20,000 feet

Max Rate of Climb, MTOW, ISA, SL: 1,040 fpm

Max Cruise Speed at 82% Power at 20,000 Feet: 165 ktas

Max Range: 971 nm [45-minute reserve]

Fuel Consumption at 82% Power: 16.3 gph

Takeoff Over 50 Ft. Obs: 1,385 feet [ISA, sea level]

Landing Over 50 Ft. Obs: 1,335 feet [ISA, sea level]

This feature first appeared in the Summer 2024 Ultimate Issue print edition.

The post Ultimate Issue: We Fly the Cessna T182T Skylane appeared first on FLYING Magazine.

As Butch asked Sundance in the 1969 movie, “Who are those guys?” To which I add: Why the Phenom 300E? And, what makes that jet so popular?

I’ll answer the second question first. It’s a combination of being the fastest single-pilot jet in the sky, the fastest light jet with the highest payload and the ability to use runways less than 4,000-feet long and climb directly to FL 450. It offers stunningly attractive and comfortable interiors as well as solid human factors engineering (HFE) that keeps the workload for a single pilot manageable in challenging conditions.

For the first question, those men and women are Embraer, a Brazilian manufacturer that for more than 50 years has been designing and building turboprops and jets for the airlines, general aviation, and military. We’ve heard it said that Embraer is channeling the disruptive aeronautical design philosophies of countryman Alberto Santos-Dumont, whose aviation firsts from 1901 through 1909 made him a household name throughout much of the world.

After visiting Embraer’s Melbourne, Florida, campus—built as the U.S. space program there was slowing down to take advantage of a highly trained workforce—with its 192,000-square-foot production facility, engineering and technology center, two paint facilities, delivery center with design studio, and flying the Phenom 300E—I came away with the feeling that the manufacturer is on the cutting edge of bizjet design, performance, and customer service (75 centers worldwide).

• READ MORE: We Fly: Cirrus SR G7

I’ll be the first to admit that the definition of light jet is a bit amorphous, although, in general, it can carry six to eight passengers on flights of two to three hours and access relatively small airports.

The Phenom 300E can be configured for as many as 10 passengers on board. A 25-degree wing sweep helps generate a maximum speed of Mach 0.8 and a high-speed cruise of 464 knots, yet its sophisticated flaps mean it can operate from 4,000-foot-long runways at sea level, needing 3,209 feet for takeoff at its 18,551-pound maximum gross weight. Fully fueled, its NBAA range is 2,010 nm, which includes the ability to divert to an alternate airport 100 nm away. With eight occupants, its NBAA range is 1,178 nm. Max operating altitude is FL 450 (45,000 feet), and the 300E can climb directly there in 22 minutes.

The Basics

The Phenom 300 debuted in 2009. In 2013 it received an avionics upgrade to the Garmin G3000 Prodigy Touch Flight Deck. A major interior redesign came in 2017. A power bump in 2020 gave it its current impressive cruise speed. That’s when it became known as the 300E—the “E” standing for Enhanced. Power is supplied by a pair of FADEC-controlled Pratt & Whitney PW525E1 engines putting out 3,478 pounds of thrust each. TBO is 5,000 hours.

Recent Developments

Enhancements keep coming for the 300E.

• Autothrottles: They tie in with the autopilot for normal operations as well as overspeed and underspeed protection. Servos move the power levers, giving the pilot a tactile indication of the power setting in addition to the display on the gauges.

• Emergency Descent Mode (EDM): With the autopilot engaged, should the cabin pressure climb above 25,000 feet, the system turns the jet 90 degrees left and commands a descent to 15,000 feet while setting the transponder to 7700. For those aircraft equipped with autothrottles, power is reduced for the descent and increased then the aircraft reaches 15,000 feet.

• Runway Overrun Awareness and Alerting System (ROAAS): It engages at 1,000 feet agl and monitors altitude and speed for the runway in use and the runway conditions. Between 500 and 100 feet agl, if approach parameters are exceeded—generally too high and/or too fast—the system cautions that unless the pilot gets the jet back into appropriate approach parameters, it won’t be able to stop on the runway—“Caution, overrun.” If things are not corrected by 100 feet agl, an aural warning, “Overrun, go around,” sounds. If the airplane floats on landing, the system will give another caution, “Long flare.” ROAAS keeps working through rollout. If the jet isn’t decelerating appropriately, it issues another warning, “Overrun, brakes.”

• GWX75 radar: It has been upgraded with automatic vertical scanning and predictive hail capabilities, which predicts hail and presents it visually on the weather display.

• READ MORE: We Fly: Diamond DA62

The airplane flown had a basic empty weight (BEW) of 11,739 pounds. With full fuel—5,353 pounds—the payload was 1,459 pounds, or six 200-pound passengers and a lot of baggage. What is usually more important is how flexible the aircraft is when it comes to fuel versus cabin load. The zero-fuel weight for the 300E is 14,263 pounds, so when loading the airplane, anything over that weight has to be fuel. That means in the airplane we flew up to 2,524 pounds could go into the cabin—a whopping load. Bringing the airplane up to gross weight with 4,288 pounds of fuel still means the jet can fly well over 1,300 nm with reserves and go fast doing it.

With Embraer demo pilots Marisha Mohler and James Crawford, some sample weight-and-balance problems using the Prodigy Touch were run. Bottom line: It was nearly impossible to load the 300E out of CG, something of major importance because it minimizes the risk that a loading error will create an uncontrollable flying machine.

The Walk-Around 

Walking around the jet, I was impressed by the size of the left-side-accessed, heated-aft baggage compartment—84 cubic feet—with room for skis and golf clubs.

I was advised that the Phenom 300 was originally designed for high usage in the fractional and charter world—with a life of 35,000 hours or 28,000 cycles—so Embraer borrowed from its experience in the constant operation airline world for longevity and robustness. I noticed such features as all exterior panels, including the windshield, use a single screw head design. If necessary, the windshield can be replaced in four hours. The lavatory is serviced externally. Single-point fueling is available, and the large airstair door is beefed up to withstand long-term use but is designed for one-handed operation.

For speed, the skins are flush-riveted, the area rule of the rear fuselage is particularly notable inboard of the engines, and there are gap seals between all control surfaces. The auxiliary power unit (APU) plug is angled, so it will pull out, rather than rip out, should a pilot taxi away with it connected. The right engine can be run in a ground power mode, functioning as an APU.

Systems are conventional, but almost all are set and forget, with automation taking care of routine tasks and abnormalities and using the large screen presentation of the Prodigy Touch to display irregularities so that the crew can determine what actions, if any, are necessary. I saw numerous examples of HFE designed to reduce pilot workload and maximize situational awareness. One example is the spoilers. When deployed in-flight, they stow automatically when certain conditions are met. They deploy automatically on landing.

• READ MORE: We Fly: Cessna TTx

Braking is via a brake-by-wire system with an electronic, rather than mechanical, anti-skid system in the same box that turns pilot brake input into electrical impulses to the brake hydraulics. The brakes are carbon, maximizing effectiveness as they heat up. Wing, tail, and engine inlet deicing is via bleed air. The windshields are electrically heated.

The electrical system is a 28-volt, eight-bus system powered by two 390-amp generators.

The Cabin

When talking about a purchase price on the order of $13 million, the reality is that an owner-flown, fractional, or charter jet exists to carry people of means who want to get to a destination fast and in comfort. I think that is true especially for the owner-flown jet family. After all, there’s a hoary aviation axiom: If the nonflying spouse ain’t happy, ain’t nobody happy, and the jet better have a comfortable potty.

After spending time in the cabin, I think Embraer nailed it. First, the cabin never gets too high—the 9.4 max pressure differential means that at the FL 450 maximum operating altitude, the cabin is at 6,600 feet. The cabin shape is a modified vertical oval, allowing the seats to be mounted low to maximize headroom. Standing 6-foot-4, I’ve been uncomfortably crowded in a lot of aircraft cabins—that was not the case here. The comfy seats recline, swivel, and track horizontally away from the bulkheads.

Everything on the ceiling is flush, including the air vents. Finally, there’s a design that gets rid of the ball-shaped head-knockers we’re used to. What is called a tech panel is on the ceiling, containing motion sensors. Moving a hand near the veneer lights up buttons to control the various entertainment systems, video displays, and cabin lighting.

The lavatory is the real thing—complete with a sink—and with solid, sliding doors for privacy. It has a window that is the same size as those in the rest of the cabin, so there’s no feeling of retreating into a black hole, especially as the lav seat can be belted and used as a passenger seat.

My takeaway from our time in the cabin and Embrarer’s Melbourne design center is that there is serious commitment to not only comfort but an elevated level of style and panache. But, then again, that’s what we expect from the country that gave us the elegance of the samba.

The Front Office

Moving forward to where the magic happens, the first thing that I observe is the sheer size of the Garmin G3000 Prodigy Touch displays and the well laid-out nature of the panel. Once seated, I found the seats to be among the easiest to adjust and the most comfortable I’ve experienced on any bizjet.

While I may have to turn in our jaded journalist accreditation, I kept running into things that were at the high end of our experience. I’ve used rudder pedals that adjust fore and aft, but never as easily as these. At my height, I’m used to being uncomfortable on a flight deck—it wasn’t the case in the 300E. To my amazement, when Captain Mohler—who is well over a foot shorter than I—got into the right seat, the seat and rudder pedals adjusted to fit her physique easily. I’m not used to that range of adjustment in flight deck seating.

I then looked at an issue I feel critical to design—crashworthiness for those at the point of the arrow. The most common bizjet accident is a runway overrun or loss-of-control event that involves impact at under stall speed, where good crashworthy design means keeping the crew alive. I generally liked what I saw. The restraint system is five-point, and there is flail space in front of the crew and no head-gouging overhead switches.

The more I learned about the flight deck and systems, the more I realized the significant thought that went into setting up the 300E for single-pilot operation and felt that it is a most reasonable step up for pilots flying single-pilot turboprops and smaller jets.

The Garmin G3000 Prodigy Touch Flight Deck avionics blend well with the aircraft, presenting what the pilot needs to know, when needed, and the shallow menu allows accessing information required with a minimum of screen inputs. Garmin’s intuitive design is well known, so I won’t go into detail here. Its incorporation in the 300E came across as nearly seamless.

While Prodigy Touch requires intense, focused training, I think that its design is pilot-friendly and intuitive. Once it is understood, a pilot can program the automation easily—thus freeing them to do the important stuff, such as think and maintain situational awareness. That’s especially important when dealing with weather or high-density airport arrivals in a single-pilot jet that goes as high and fast as this one.

Flying It

Starting a Phenom 300E is so easy that I can’t help but wonder whether it’s illegal in some states. You turn the appropriate rotary switch at the base of the power quadrant from “stop,” past “run” to “start.” Wait two, count ’em, two, seconds and then turn the switch back to run. FADEC takes care of monitoring engine rpm, applying fuel and ignition at the appropriate time and monitoring temps as the engine spools up—stopping the start automatically should something be amiss.

Yes, you monitor and are prepared to move the switch to stop, but there’s little to do. Taxiing is via the rudder pedals and carbon brakes. Once running, the jet will roll away from the chocks at idle power, meaning that braking is needed.

Takeoff preparation is easy—the checklist is short and consists generally of setting flaps, confirming that the departure procedure and initial altitude are loaded in the Garmin. I liked that there is nothing extra to do—or forget—after takeoff clearance is received. There’s a takeoff configuration button to push that checks the critical stuff and confirms that the jet is configured for takeoff. Switchology at that point is that every switch should be in the 12 o’clock position and all lights off. “12:00 and dark,” is the call. It’s simple, straightforward, and crew-friendly.

Loaded about 2,000 pounds below gross for this launch, V₁ was 105 knots, with V_R at 106. Acceleration was as to be expected for a bizjet, exhilarating and addictive.

Rotation immediately generated a positive rate of climb, once the gear was up and flaps retracted, we watched the rate of climb slide into the 3,000 fpm range as we accelerated.

We alternated hand-flying and having the automation handle things as we were slowly cleared to a 16,000-18,000-foot block altitude east of Melbourne. There, we hand-flew the 300E through steep turns and found that the jet is just plain fun to fly. The controls are heavy but responsive and the aircraft stays where you put it. Stick-force-per-G is linear and gets heavy quickly, so it’s unlikely someone will inadvertently load up the airframe when maneuvering.

With the autopilot back on, we pushed the power levers from max cruise to the climb mark and reached FL 450 so quickly that we were still negotiating with ATC for a route where we could have 10 minutes of level flight for a speed check. Once at altitude, we left the power in the climb setting and accelerated to Mach 0.8 , where at ISA minus-7 degrees Celsius we were burning at a total of 910 pph.

Pulling the power back to max cruise, the speed slowly backed off from Mach 0.8 to about 0.78 before it was time to start a descent. Heading down, we explored an emergency descent with power at idle (no effect on pressurization) and spoilers deployed and saw 10,000 fpm on the gauges.

I was impressed by the ease of programming the Prodigy Touch system as Captain Mohler did so while we were being vectored through busy Florida airspace and set up for the RNAV approach into Runway 9R at Melbourne. What would otherwise have been a workload-intensive event was something, in my opinion, easily handled by a single pilot comfortable with the automation and maintaining situational awareness.

Once established on glideslope, Captain Mohler suggested trying the coupled go-around feature. Pushing one of the TOGA (takeoff-go-around) buttons on the power levers caused the flight director to command an appropriate pitch up with the autopilot following the command. With autothrottles installed, the power would have come up simultaneously.

We then disabled the autopilot and rejoined the glideslope to set up a demonstration of ROAAS.

I’ve seen far too many bizjet runway overshoot accidents—and they almost invariably arise from being high and/or fast on final with a pilot determined to complete the landing and certain they can pull things together, only to discover the laws of physics can’t be broken. I think ROAAS will go a long way in reducing one of the remaining bugaboos of bizjet operations.

After sampling the automatic go-around and ROAAS features, landing the jet in gusty conditions proved to be a nonevent. I found it easy to maintain VREF. Captain Mohler called for pulling the power levers to idle at 50 feet and making a minimal flare. We managed to develop a sink rate at the last moment and touched down embarrassingly firmly. However, in performing its design duties, the trailing beam landing gear soaked things up and made us look good.

In the gusting crosswind we appreciated the automatic spoiler deployment. I could pay full attention to keeping the airplane tracking where we wanted with the main gear firmly on the ground. Applying gentle pressure initially to the brake pedals provided feedback that all was well, so I applied significant pressure as we wanted to make a nearby taxiway. I never felt the anti-skid cycle, but the jet slowed as if someone had tossed out an anchor.

In Conclusion

I came away from our time with the Phenom 300E impressed in many ways.

I like the robustness of the airframe. I appreciated the thought that went into a design focused on the needs of pilots so that either as a crew or single pilot, they can concentrate their time and energy on what is important, situational awareness, and handle whatever weather, ATC, or equipment failures throw at them without descending into the high-stress, tunnel-vision world where mistakes are made.

Spec Sheet: Embraer Phenom 300E

Price (as tested, estimated): $13 million

High Cruise Speed: 464 ktas

Max Mach Number: 0.80 MMO

NBAA IFR range (5 passengers): 2,010 nm

Takeoff Distance, 1,000 nm/NBAA IFR: 3,209 ft. at max gross weight

Landing Distance, Unfactored/NBAA IFR: 2,212 ft.

Max Operating Altitude: 45,000 ft.

Length: 51 ft., 4 in.

Wingspan: 52 ft., 2 in.

Height: 16 ft., 9 in.

Cabin Length: 17 ft., 2 in.

Cabin Width: 5 ft., 1 in.

Cabin Height: 4 ft., 11 in.

Maximum Payload: 2,524 lbs.

Payload, Full Fuel: 1,459 lbs.

Pressurized Stowage: 10 cubic ft. in the cabin

Aft Cargo Stowage: 84 cubic ft.

Cockpit at a Glance: Embraer Phenom 300E

A. The Embraer Phenom E00E’s pair of displays can be laid out in many ways. The primary flight display features a familiar Garmin interface, with airspeed and altitude tapes plus attitude information.

B. The multifunction display hosts the power and propulsion system schematic in this view.

C. A Garmin GTC-style touchscreen controller also follows the similar control unit found in many new piston and turboprop airplanes.

D. The power levers on the right side of the pilot’s seat are set as required for the necessary engine power output.

E. The flight control yoke is used to control pitch and roll.

This feature first appeared in the May 2024/Issue 948 of FLYING’s print edition.

The post We Fly: Embraer Phenom 300E appeared first on FLYING Magazine.

The complexity of the instrument panel has served either to intrigue or intimidate potential pilots. Having been the former kind, I’ve had trouble putting myself in the latter’s point of view.

But with ever-advancing avionics and capabilities, I admit it can be tough even for the seasoned ones among us to keep up. That’s why the fresh approach Cirrus took to its next model in the SR series makes a lot of sense.

And for new pilots—and this pilot who flies Cirrus aircraft sporadically—as opposed to a seasoned owner or dedicated Cirrus instructor, the barrier to entry and re-entry has fallen significantly.

Though it’s not as overtly revolutionary as the Cirrus Airframe Parachute System (CAPS) or Safe Return enabled by Garmin Autoland on Cirrus’ SF50 Vision Jet, the reimagined flight deck in the new SR G7 and other improvements make a more immediate impact—because pilots benefit from them on every flight, from the moment you press the start button.

Wait—what??? There’s a start button?

What’s new here takes us way beyond the panel.

A Beginner’s Mind

When you must approach something from a fresh perspective, it helps to go into a beginner’s mindset.

But how to do so when you’ve known the airplane since its early development years, as I have? In a similar fashion, the engineering and product dev teams at Cirrus had to work to place themselves in that beginner’s mindset.

My first look at the G7 started with a long cross-country. And the fact that I hadn’t flown an SR for a year assisted me in taking in the new generation with as close to a newbie’s view as possible. I met up with Cirrus SR product director Ivy McIver in stealth mode at the Hagerstown Regional Airport (KHGR) in Maryland.

She warned me ahead of time that the airplane wouldn’t appear different from the outside but to expect something truly different inside. So I fired up the GoPro and prepared for her to open the door.

First Approach

From the walk-up you might notice a new paint scheme, new colors—but it’s true you won’t really register a change until you open the pilot’s door.

In fact, McIver had been flying the G7 around in broad daylight, with only a series of foiled sunshades to hide the nature of what awaited inside. This obviously kept the ruse going, and according to McIver, I was officially the first person outside of Cirrus to demo the new model, a real privilege.

• READ MORE: We Fly: Diamond DA62

After giving me a quick preview on the ground, we needed to see the G7 in action to begin to appreciate all that had been accomplished with the redesign. We flew in pursuit of good weather and photo backdrops not browned by the seasons, and headed south—nearly straight south—from Maryland to Florida by way of Hilton Head, South Carolina.

It honestly took the five-plus hours en route (and a fuel stop) to get a sense of it all.

Engine Start

Push the button. Hold it in, monitor a gauge, release. After setting things up, that’s typically all you have to do in a jet. The mag switch has been relocated, made larger to the palm, and incorporates a button to start. It’s an elegant way to make the process similar to the SF50, while still preserving the ability to isolate mags, whether in a before-takeoff check or in-flight issue. There’s no key to insert—just like with today’s automobiles. The logic is, if you can enter the airplane with the key fob, you can start the engine.

Fuel selection has also benefited from “Vision Jet-ification, ” with an automatic fuel switching protocol that alternates tanks by physically moving the fuel selector knob with every 5 gallons burned. You can override the system to manual by lifting a sliding door, but it was honestly completely forgotten within the first half hour of our flight demo. It’s very similar to that found in many single-engine turboprops as well.

Taxiing out reveals more fascinating tools. While we have experienced SafeTaxi and SurfaceWatch from Garmin before, the G7 takes it a step further with automated slewing to the proper PFD perspective during ground operations versus in flight. The functionality is smart, in that it zooms in and out, adding and subtracting info from the display based on your speed and location relative to a runway—whether you are holding in the ramp area or taxiing onto the active for takeoff, for examples.

Cross-Country Lines

The faster an airplane cuts through the air, the more of the country you can string together at one go.

But the engineering behind the G7 didn’t wring a few more knots from the carbon fiber airframe by tweaking fairings or FIKI panels. The team accomplished the most recent speed mods in the last G6 version we flew (“We Fly: Cirrus SR22T 8000,” March 2021).

Instead, the G7 begins saving the pilot time on the ground—during pre-startup, taxi, and before takeoff checks—streamlining what had at times been belt-and-suspenders checklists into the key items retained in a logical flow. A new scroll wheel fell nicely to hand as I ran through the commensurate checks during each stage of preflight, in-flight, and postflight procedures. The checklists come linked to the CAS as well, so that the appropriate ones come to the fore when an alert pops up.

• READ MORE: We Fly: Cessna TTx

Some elements are just left on. Like the nav lights. With long-life LEDs, when would you choose to leave them off? Therefore, not only do the nav lights come on when BATT 1 is turned on—the same goes for the avionics—but the nav light switch has been removed from the electrical system subpanel in front of the PFD as well.

Streamlining has targeted what’s in the PFD too. Menus have popped out of their nesting, leaving layers behind that previous pilots had to wade through. The G1000 gained complexity over the years—expanding in parallel into the G2000, G3000, and Perspective. When you can strip away those unnecessary complications, you save time in normal operations but also during abnormal and emergency procedures.

Where the pilot retains control—such as in setting the power and mixture—Cirrus incorporated aids to make standard adjustments easier. Since the engine monitoring system knows the aircraft altitude, outside air temperature, and internal temps in the Continental IO-550-N (in the case of the normally aspirated SR22 we flew for the report), it updates the green arcs on the power setting and fuel flow gauges on the display. The pilot puts the power setting at the percent power desired then sets the mixture to the top of the green arc for best power. Further leaning for LOP settings—or rich of peak settings—can utilize lean assist.

While these tools have been available in various forms in Garmin-integrated flight deck installations, the protocols underwent refining with the latest edition of the Perspective Touch+ in the SR G7.

In-Flight Maneuvering

So if the shell of the SR22 has remained the same, along with its planform, control surfaces, and powerplant, why would I take the time to fly through a full series of maneuvers—after spending five-plus hours speeding down to Florida and two more as a safety pilot in our photo mission for what you see on the cover and in these pages?

Because one more thing has changed in the G7—and it may not mean much to most pilots who fly the new model, but it impressed me enough to need to take it through its paces. That’s the updated flight control stick. The SR series’ flight control mechanism had iterated only slightly from its origins as a somewhat utilitarian-feeling half-yoke managed by trim on a hat button in the first production SR20 in the late 1990s. The upgrade in ergonomics with the G7 makes a real difference to this size-5-glove wearer.

• READ MORE: We Fly: Garmin Autoland for the Beechcraft King Air 200

Another new jet-like inclusion? A stick shaker. This I definitely had to see in anger, so as part of the standard test profile I conducted, we looked at both power-on (departure) and power-off (approach) stalls. Holding down the autopilot disconnect button allows you to maneuver past the ESP (electronic stability protection), and in this case, pitch up to a deck angle needed to induce preliminary stall buffeting. However, before any break, the stick shaker activated—as if the “danger Will Robinson” graphics on the PFD could be ignored—compelling the release of whatever back pressure I was holding in to induce the stall condition.

Flap overspeed protection makes for one more improvement, preventing the pilot from deploying the flaps above the programmed indicated airspeed relevant to the flap setting selected. It also prevents you from retracting the flaps when airspeed is too low.

Behind the Systems

Cirrus also calls out an intelligent new battery to support the electrical system. How can a battery demonstrate intelligence? Maybe that’s a bit of affectation—but we’re seeing certain levels of system monitoring and responsiveness in electric and hybrid aircraft, and this may be an instance where there is carryover from these innovations in battery management systems that make them seem, well, intelligent, as they optimize cells purportedly for improved performance.

Systems pages on the MFD present the details from the pilot’s operating handbook in a color-coded manner, easing quick interpretation and assessment of status for electrical, ice protection, fuel, and environmental control systems. When used in combination with the checklists, the need to pull out the pilot’s operating handbook in flight goes down—saving more time in tense situations.

The built-in oxygen system comes as an option—I suppose you can save the money and 18 pounds of added weight if you don’t plan to fly high. But at $13,900 to me it’s cheap insurance to have O2 locked and loaded so that you can access it quickly and with less fuss than a portable system. And you don’t need to be flying the turbo model up in the teens to gain from its use—most of us perform better in the airplane if you turn on the juice as low as 7,000 or 10,000 feet, especially at night.

Stacking Up the Options

The specific serial number we flew was an SR22 GTS version of the G7, equipped with air conditioning, Cirrus Global Connect, built-in oxygen, and the Hartzell lightweight three-blade composite propeller upgrade. The blend prices out at $1,136,500 and takes the weight from the standard GTS basic empty weight of 2,359 pounds to 2,419 pounds—the Hartzell prop takes off 12 pounds, while the AC adds 55 and Global Connect 6.

The standard interior has taken a turn to anything but a commonplace look and feel. Not only have the seat designs seen a visual update, but the ergonomics have improved as well. Better placement of the USB-C ports and more robust cup holders—seriously, this is an issue when they are flimsy in a million-dollar-plus aerial conveyance—round out the updates. As with the G6, the baggage door is unlocked with proximity to the key fob, and it opens with the touch of a button to assist when your hands are full. And you can see if it’s left open by CAS message and on the appropriate systems page.

Connectivity includes Garmin’s Flight Stream 510 that the avionics OEM rolled out in 2016, automating the data exchange between the aircraft, pilot, and manufacturer. Jeppesen ChartView, SiriusXM weather and audio, and Garmin Pilot come along for the ride too. The GTS package adds Cirrus Executive (yaw damper, enhanced vision system), Cirrus Awareness (active traffic, eTAWS), Cirrus Advantage (14-inch screens, taxiway routing, Surface Watch), certified flight into known ice (FIKI) protection, the Premium appearance options and GTS badging to identify the series.

For a low-end reference on the evolved series, pricing begins at $634,900 for a base model G7 SR20. All versions come standard with a three-year, 1,000-hour spinner-to-tail warranty that rivals other new piston singles. For $21,900 to $25,900, you can add two years and 1,000 more flight hours to create five-year coverage for the SR G7, depending on the model.

And we can’t help but mention the new colors, in and out, that add to the wide-ranging palette of head-turning options. While you can choose a more restrained look, Cirrus offers more to appeal to those who don’t mind drawing attention on the ramp. New exterior colors include the striking blue on N433CA, while several customer favorites remain, such as the gray on N616SP, which I flew for this piece. And the interior continues the conversation piece, with leather, bolstered seats, and satin silver vents and lights. Pilots can choose from five leather colors and two cabin interiors. The seats can be appointed with black Alcantara inserts or an all-leather design.

The Grand Total

Wrapping it up in a complete package and taking a step back, what has Cirrus Aircraft achieved here? In my estimation, the company had to have felt challenged to build on its success—with the 500th Vision Jet overall delivering in the third week of December and 389 2023 SR models flying out the door by the end of the third quarter of 2023.

Simplifying things is hard, particularly when selling at an ever-increasing price. It’s easy to chase the marketing pundits chorusing “more, more,” adding to the feature set to justify the value.

But to the Cirrus customer, who has typically been sold on the lifestyle offered and enabled by the airplane, the most elusive commodity is time. Other OEMs have thought through time-saving elements—think of the Gulfstream G700, that, when certificated, will allow the pilots to go from opening the door to engine start in less than five minutes. So this is what Cirrus really achieves with the streamlining of the flight experience made possible by the G7.

The G7 hits the mark, giving a pilot for whom technology resonates—but doesn’t wish to piddle around the airplane, tinkering on weekends, and getting things just so—the ability to walk up to the airplane, start up, and go with a streamlined approach, knowing the technology in the background has your back.

Spec Sheet: 2024 Cirrus SR G7

Price, as tested: $1,136,500

Engine: Continental IO-550-N, 310 hp

Propeller: Hartzell lightweight, composite, three-blade

Seats: 5

Length: 26 ft.

Height: 8 ft., 11 in.

Wingspan: 38 ft., 4 in.

Wing Area: 145.16 sq. ft.

Wing Loading: 24.8 lbs./sq. ft.

Power Loading: 11.61 lbs./hp

Cabin Width: 4 ft., 1 in

Cabin Height: 4 ft., 2 in.

Max Takeoff Weight: 3,600 lbs.

Max Zero Fuel Weight: 3,400 lbs.

Standard Empty Weight: 2,272 lbs., base 2024 SR22

Max Baggage: 130 lbs.

Useful Load: 1,328 lbs., base 2024 SR22

Max Usable Fuel: 92 gal.

Service Ceiling: 17,500 ft.

Max Rate of Climb: MTOW, ISA, SL: 1,310 fpm at 50% flaps (takeoff); 1,268 at 0% flaps (en route)

Max Cruise Speed: 186 ktas

Cruise Speed at 75% Power, 8,000 ft. pressure altitude, 3,400 lbs., ISA: 180 ktas

Max Range at 55% Power, 14,000 ft., ISA: 1,169 nm; 11.3 gph

Stall Speed, Flaps Up: 73 kcas

Stall Speed, Full Flaps: 61 kcas (most forward CG)

Takeoff Over 50 Ft. Obs: 1,868 ft. (ISA, sea level)

Landing Over 50 Ft. Obs: 2,535 ft. (ISA, sea level, flaps 100%)

Cockpit at a Glance: 2024 Cirrus SR G7

A. Mimicking the Vision Jet, the SR G7 features a push-button start—though mags and mixture must be properly set for ignition to take place.

B. The new Cirrus Perspective Touch+ by Garmin includes twin 12-inch displays that come standard, with 14-inch PFD and MFD an option. All feature split-screen capability.

C. The two Garmin GTC touchscreen controllers carry over from the jet as well and offer redundancy of functions.

D. The digital, dual-channel automated flight control system (AFCS) incorporates “smart servo”

technology and includes an optional yaw damper that automatically disconnects at 200 feet agl.

E. Updated synoptic pages and streamlined checklists aid in the monitoring of both systems and procedures throughout all phases of flight.

F. The Cirrus IQ app gives the pilot remote viewing and control. Optional Cirrus Global Connect delivers worldwide texting, telephone service, and weather.

This column first appeared in the January-February 2024/Issue 945 of FLYING’s print edition.

The post We Fly: Cirrus SR G7 appeared first on FLYING Magazine.

Since the first of its kind—the Wright Flyer, if you go back all the way—airplane designers have addressed the tension between power and control in a variety of ways. Some with centerline thrust, such as the Cessna 336 and 337 Skymaster, and others with pilot support, such as the Beechcraft King Air’s latest autothrottles—both under supplemental type certificate and standard in new models—taking flight in the one-engine regime into “easy day” territory.

But Diamond quietly achieved the latter in elegant ways with the DA62, starting with its first flight in April 2012. Now, more than 11 years later, the twin has become a darling of private owners as well as a handful in flight training.

Futuristic Lines

I first contemplated the DA62 in detail as I flew off its wing in Diamond’s newest sister ship, the DA50 RG, for a pilot report last spring (see “We Fly: Diamond DA50 RG” in Issue 938). We followed a course from Friedrichshafen, Germany (EDNY), after the AERO 2023 conference, to Diamond’s home in Wiener Neustadt, Austria, south of Vienna. While at first take the DA62 appears to be a stouter version of the DA42 that preceded it (and which sees most of its time on training flight lines in Europe and North America), upon inspection it appears even more robust—less a Captain Proton design than a Porsche Cayenne with wings and a T-tail.

• READ MORE: We Fly: Cessna TTx

I did my initial multi in 1995 in a pair of Cessna 310s—first a J-model belonging to master Twin Cessna instructor Chuck Clemen, and the second a striking P-model with a jaunty red stripe at Longmont Air Services at what is now KLMO in Colorado. I started an airline transport pilot certificate course in a Piper Seminole at one point—and that’s another story—but was less than impressed with it after enjoying the stately, still-modern ramp presence and performance of the 310. But the lack of single-engine climb rate on takeoff in Colorado even in the 310 sobers you up quickly.

That’s where the DA62 demonstrates its difference. With a single-engine service ceiling of 13,000 feet, you might actually be able to climb to the pattern for a landing following an engine failure after takeoff at mile-high elevations—as opposed to closing both throttles and aiming for the softest spot like you were in a single.

While the DA42 came in a couple of versions, one with Lycoming and one with Austro Engine powerplants, the DA62 entered both EASA and FAA certification with the AE-330s, a bespoke jet-A burner based on a Mercedes-Benz automotive diesel engine. Originally having a 1,000-hour TBO, the bar was raised in 2019 to1,800 hours, with estimated overhaul costs still in flux as of press time. But regardless, it’s great news—saving money for engines making it to the later TBO.

FADEC Baseline

The DA62’s genius lies in the way the designers architected the FADEC-enabled engines to leverage that control into a safety net for the pilot to use in the event of a power loss. But the simplification of operation begins on engine start and carries on throughout the flight.

• READ MORE: We Fly: Garmin Autoland for the Beechcraft King Air 200

The before-takeoff checks illuminate how this works. The dance of checking prop, mixture, and mags—involving six levers in most standard light twins—is replaced with the 20-second-long ECU test that runs its automated magic when you press and hold the button on each engine in sequence. The fuel system also follows the simplicity rule, with two tanks centered between the fore and aft spars and within the stout carbon fiber structure to attain the level of crashworthiness for which Diamond airplanes are known. To crossfeed in the event of single-engine operations, or to balance fuel between the wings, you place the fuel on/off lever into that position for the tank, with the red off position guarded with a sliding, red metal gate.

Flight Test

I took the opportunity to fly with Micke Lang, pilot and delivery manager in flight operations for Diamond Aircraft, out of the European factory location at Wiener Neustadt (LOAN). After watching the previous days’ ballet of aerial photography of the DA62, with its steep turns and quick breaks, I couldn’t wait to get my hands on the stick—yes, a twin with a control stick—and feel those maneuvers for myself.

Lang briefed me on the flight ahead prior to getting on board the airplane. Then he walked me through the engine start, flipping the master switch on and pushing the silver button on the left and then right as we cleared both sides visually. Soon we were calling our position on the 1,067-meter (3,501 feet) runway for a normal takeoff, which in our very light configuration—with half tanks and just the two of us on board—took less than half its length.

We cruise-climbed up at 110 knots indicated (V_Y is 89 kias) to a moderate altitude of 4,500 feet msl from which to begin the high work series, starting off with a power-off stall with flaps and a mild relaxation of pressure around 70 knots on the tape. No bad habits as long as both engines are turning in equal measure. In fact, the aerodynamics compared favorably to the single-engine retract DA50 RG I’d just tested, definitely showing the family resemblance.

Single-Engine Operations

We put the DA62 through a full palette of ops on one engine—with Lang shutting down the left engine with a flip of the switch, upon which time it automatically went into feather, prop stopped. I took the controls, and put in 5 degrees of bank into the good engine, but tooling around on one above the Austrian fields felt only nominally different from two-engine maneuvers, handling wise. The left side is the critical engine, but the low power adjustment needed to maintain level flight at that altitude made it feel decidedly not so critical. It makes sense that V_YSE at 87 kias is so close to V_Y in this twin.

After conducting the demonstration of the loss of power, bringing that side back to life was as simple as maintaining the recommended airspeed, 80 knots (76 knots for a stopped prop), allowing the prop to regain forward thrust as I turned the ECU switch back on.

All along the flight, I felt instantly comfortable with the familiar Garmin G1000 NXi up front with two primary flight displays and a central multifunction display. Within its avionics brain, you find the industry standard ESP (enhanced stability protection), an emergency level mode, weather radar via the GWX8000, and Surface Watch ground alerting system. The most recent Phase III software update introduced split-screen functionality, Bluetooth recording of pilot audio, and coupled go-arounds using the GFC 700 autopilot.

Getting Current?

As we returned to base, Micke demonstrated one unique flight regime for the DA62, the accelerated descent. Putting the airspeed tape at the bottom of the yellow arc—at 162 kias and 1,100 fpm down—we smoothly bled off altitude to transition to the charted visual approach back into LOAN. I gave Lang a moment’s pause when I answered his question: How many landings shall we do? Three, I said half in jest, so I can be current.

Yes, in an EASA-registered airplane not logging instruction, that was not really to be the case, but with the ease of operation—and the straightforward approach and touchdown sight pictures for the DA62—it would have been readily accomplished.

Can It Carry Seven?

The target market for the airplane (see “The Owner Experience” below) lies in the coveted six-seater realm, and the DA62 goes one better over standbys such as the Beechcraft Bonanza G36 by allowing for up to seven passengers. To be fair, the rear seats combined are really only workable for a couple of children perhaps, but with seven belts instead of six, that option remains. And with a useful load of up to 1,548 pounds, that choice is real. Front baggage compartments hold up to 66 pounds on each side—and the third row can have an optional fold-down capability to fit in more stuff by volume.

The owner can choose a range of materials and designs based on whether those kids—hypothetical or not—tend to leave a trail of Goldfish crackers and sippy cups behind, or if they’re grown and ready to go looking at college campuses with the pilot on a whirlwind tour.

And while you can make your own paint scheme a reality, the selection of premium colors runs from ruby red to anthracite black. With the leather interior choices on Diamond’s famous crashworthy seats, owners can opt for a variety of options, from highlight stitching to custom panels and carpets.

Market Penetration

Since the DA62 was first delivered in 2015, with two units, Diamond has kept a steady cadence of between 26 to 33 units each year up through 2021.

However, a jump to 53 out the door in 2022 and 30 in the first half of this year signal an uptick in orders. At press time, Diamond had reported a total of 273, according to figures compiled by the General Aviation Manufacturers Association, in the hands of mostly ecstatic private owner-pilots.

The significant fleet speaks to the sweet spot that the DA62 has found in the market—for a true family luxury SUV of the air.

The Owner Experience

With nearly 275 in the field, the Diamond DA62 is making pilots happy with their choice.

In the 40 years since he became a pilot, and 20 in the aviation business, John Armstrong of LifeStyle Aviation has flown his share of light twins. But the Diamond DA62 is the airplane of choice to fly every week.

“It’s my go-to airplane, and I love it,” Armstrong says, because it requires relatively little effort from the pilot compared to others in the piston-twin segment.

That sentiment echoed through the voices of the four DA62 owners FLYING interviewed for this article. From high time pilots, such as Armstrong and Scott Thompson, to brand-new ones, like Brett Swanson and John Chaffetz, everyone agreed that the DA62 ranked among the lowest in pilot workload and commensurately high in capability and capacity for their respective missions.

Bill Craven purchased serial number 177 in January 2022—and he transitioned from the Cessna T182T and T206 that he had used to fly his family from the Seattle area to a vacation home in central Washington. Craven was attracted by the DA62’s flight into known icing (FIKI) approval to make the oft-wintry trek over the Cascades. With a similar useful load to the 206 but with an extra engine, the DA62 has proven to be a reliable mount.

“It’s easy to fly, but also a pilot’s airplane,” Craven says, referring to the airplane’s control stick and direct feedback.

Chaffetz started flying in a DA40 in the Los Angeles Basin, so the transition to the DA62 felt natural to him. It also appealed to his passengers.

“The stability is the thing,” he says. “It’s a little bit heavier than the DA40 but still fun to fly. It’s just so much more comfortable on longer trips.”

With the ability to seat up to seven people, depending on their size, owners have options. Thompson has a few tips regarding the configuration.

“It’s really a four-adult, two-kid, or five-adult, two-kid, or five-adults-and-a lot-of-bags airplane,” he says.

And it sips jet-A, which several owners reported was an advantage because of its widespread availability. Several we spoke with reported economy cruise burns of around 15 to 20 gph total.

But for all of that capability, the mechanics of flying the twin remain straightforward. For Swanson, more than any other thing, the simplicity of operating the DA62 lends him a degree of confidence that he truly appreciates.

“The pilot workload is just lower,” he says, which allows him to use the airplane to visit store franchise locations around the Southeastern U.S., with either his wife or several colleagues on board.

Plus, it passes the all-important test for passenger and pilot—satisfaction.

“When it sets down on the runway, it sticks—that’s part of the confidence,” Swanson says, noting that although his insurance was pretty expensive during the first year, it was worth it.

Cockpit at a Glance

A. The engine-start sequence is enabled by the control inherent in the Austro AE-330 powerplants, using the ECU switches for each engine.

B. The Garmin G1000 NXi offers ESP, emergency level mode—and in the latest update, split-screen functionality and coupled go-arounds with the GFC 700 autopilot.

C. The single lever for each engine helps to reduce workload, and one-engine-out operations are streamlined so that bringing back the power on the failed engine feathers the prop.

D. The fuel system is also simplified, and it follows Diamond’s standards for safety and crashworthiness, plus the ability to crossfeed with the slide of a switch.

E. The control sticks are unique among twins, giving the airplane an immediate responsiveness.

Spec Sheet: 2024 Diamond DA62

Price, standard equipped: $1,471,950

Engine: 2 x Austro Engine AE-330, diesel

Propeller: 2 x MT-Propeller MTV-6-R-C-F/CF, composite, three blade

Horsepower: 180 hp per side (177 hp max power, 169 hp max continuous power)

Seats: Up to seven

Length: 30 ft., 1 in.

Height: 9 ft., 3 in.

Wingspan: 47 ft., 10 in.

Wing Area: 184.1 sq. ft.

Wing Loading: 27.54 lbs./sq. ft.

Power Loading: 14.32 lbs./hp

Cabin Width: 4 ft., 2.8 in

Cabin Height: 4 ft., 2.4 in.

Max Zero Fuel Weight: 4,850 lbs.

Max Takeoff Weight: 5,071 lbs.

Empty Weight: 3,523 lbs., depending on options

Max Nose Baggage: 132 lbs.

Max Rear Baggage: 265 lbs.

Useful Load: 1,548 lbs., depending on options

Max Usable Fuel: 86.4 gal. (main + aux.)

Max Operating Altitude: 20,000 ft.

Single-Engine Service Ceiling (ISA, MTOW): 11,000 ft.

Max Rate of Climb (MTOW, ISA, SL): 1,028 fpm

Cruise Speed at 85% Power: 185 ktas, ISA, 12,000 ft.

Max Cruise Speed: 192 ktas, ISA, 14,000 feet msl, at 4,407 lbs.; 190 ktas at MTOW

Max Range: 1,288 nm with no reserve

Fuel Consumption at 60% power: 11.8 gph, 12,000 ft.

Stall Speed, Flaps Up: 72 kcas MTOW

Stall Speed, Full Flaps: 68 kcas MTOW

V_MC: 76 kias, flaps up

V_YSE: 89 kias (MTOW)

Takeoff Over 50 Ft. Obs: (ISA, sea level, MTOW) 2,732 ft.

Landing Over 50 Ft. Obs: (ISA, sea level, MLW) 2,559 ft.

This column first appeared in the December 2023/Issue 944 of FLYING’s print edition.

The post We Fly: Diamond DA62 appeared first on FLYING Magazine.

The technology has been around since before World War II in military airplanes (see “How Can It Land Itself?” below) and from the mid-1960s in transport category jets. But if necessity is the mother of invention, then market demand is its directional guidance. When Garmin Aviation unveiled its Autoland emergency landing system in 2019, we saw the intersection of relatively inexpensive and precise GPS navigation, digital autopilots, and the FADEC-enabled turbine and turboprop powerplants capable of responding elegantly to an autothrottle.

Garmin debuted Autoland in the Piper M600/SLS—with an emergency-only autothrottle at first. Daher was first to certify a standalone Garmin autothrottle, in the TBM 940, followed by Cirrus in the SF50 Vision Jet, then the two OEMs added Autoland functionality in sequence in 2020. For the safety breakthrough, Garmin secured the Robert J. Collier Trophy—and FLYING’s 2021 Innovation Award.

In the case of Garmin’s Autoland, the fact that someone has yet to push the big red button spells a certain success. Or does it? Have you read of an accident in which the aircraft’s ability to land itself might have saved the day? And would you use the system if the situation warranted?

The Next Versions of Autoland

No one seems to mind that we haven’t seen Autoland used in anger yet. The applications just keep coming. Adding to new certs in the TBM 960 and Daher retrofits, the recently announced HondaJet Elite II program on its model HA-420, and the inclusion of the system on the upcoming Beechcraft Denali single-engine turboprop, Garmin has been working on its own supplemental type certificate for the Beechcraft King Air 200, to be followed by the 300 series—on an up-to-50-year-old design with many configurations.

For the King Air 200 series STC, you need a 200/B200 model—and several key components, including the Pratt & Whitney PT6A-42, -52, or -61 engines paired with four-blade props. Your King Air also requires hydraulic landing gear for Autoland. You’ll need the latest configuration Garmin G1000 NXi flight deck for either autothrottle alone or paired with Autoland. You can start with an analog panel or the basic G1000—you just have to get the updated NXi first.

• READ MORE: Elliott Aviation Delivers First Garmin Autoland Upgrade in King Air B200

Four years ago, I had a sneak peek of the very first installation at Olathe, Kansas, at New Century AirCenter (KIXD). On August 19, I climbed on board with Eric Sargent, engineer and flight-test pilot, into N60HL, which Piper had delegated to the project just a day before the company had to take it out of market survey for the final push to certification. I didn’t know what to expect—and we flew a slightly modified version of the protocol since the whole project remained under a cloak of secrecy at the time.

Still, I had to draw upon all my years of sitting there in the right seat watching students work out how to land without my touching the yoke, in order to keep my hands from grabbing for the horns as the M600 made a competent—if a bit solid—touchdown.

Going Flying—Hands Off

During that initial dance with Autoland, Jessica Koss, then aviation media relations specialist and now demo pilot for Garmin, led my introduction to the project. So it was only fitting that she would take the left seat in the King Air for the next demo I’d have—this time out of the Appleton Regional Airport (KATW) in Wisconsin during the week of EAA AirVenture in late July. Garmin announced the STC in progress the week prior, so our moves weren’t top secret this time, but it still felt like we would tap into talents on board the twin turboprop that the bigger iron we taxied past—a Falcon 900, a Citation Latitude—could only dream of having in the panel. With two rated pilots up front, midsize to long-range business jets don’t need “George the autopilot” to do any more than it already does, perhaps. But the King Air—so often flown single pilot—does.

This King Air B200—N288KM, Garmin’s workhorse test bed for new toys—had two critical building blocks installed to make the Autoland system work. First, it needed the upgrade to the G1000 NXi, the integrated flight deck now available by STC or as original OEM equipment in a multitude of light singles and twins. That STC for the King Air 200 series debuted in 2011—and across the King Air C90, 200/B200 and 300/350 series, Garmin estimates roughly 841 aircraft have had the STC installed, with 562 already equipped with the upgraded G1000 NXi.

Second, the King Air needed an autothrottle. While another autothrottle option exists for the model—the Innovative Solutions & Support installation, which debuted in 2019 and won FLYING’s Editors Choice Award that year—the Autoland suite requires the Garmin solution. That didn’t exist until recently, and it’s part of the package Garmin introduced at AirVenture. We would get to test both the autothrottle in its stand-alone modes and Autoland with the AT pulling the power levers, literally.

Before we launched, we’d had a briefing on the suite and the procedures. Around the table at the Appleton Flight Center—a hive aswarm with pilots to-ing and fro-ing during the show—Koss, Will Johnson (flight-test engineer), Aaron Newman (flight-test pilot), and Scott Frye (program manager) walked us through the architecture of the system and what to expect.

• WATCH: We Fly Garmin Autoland King Air 200

About That Autothrottle

We followed the plan to go through a takeoff using the autothrottle and climb above the bumps around 5,500 feet msl. The autothrottle itself brings significant safety benefits through its series of modes paired with the phase of flight. One key “pilot surprise” it prevents is throttle rollback when engaged—which has been blamed for several accidents over the course of the twin’s history. It also provides torque adjustment in the case of an over-temperature or overtorque condition.

Takeoff, climb, and descent/approach modes have standard settings or can be user-configurable.

But the phase of flight where the AT shines is if you lose power on one side. Then, it kicks into OEI (one-engine inoperative) mode and supports the pilot, working in parallel with the King Air’s native rudder boost. Autothrottle OEI is separate from rudder boost-triggered OEI ESP, and it is functionally equivalent to normal AT, except it parks the failed side throttle lever in its present position once the failure is detected.

About 20 nm out from KATW, Koss called Appleton Tower and by their prearranged agreement announced the request to initiate the Autoland sequence. As expected, the tower was able to accommodate the demo and told us to expect Runway 21. With the way clear, Koss had me engage the guarded, red-rimmed “Emergency Autoland” button—found in the King Air application on the lower console between the pilot and copilot seats. That keeps it within reach of both cockpit denizens but also the folks in the back.

From there on, Autoland took the reins, and frankly, it got pretty boring—if not still a bit surreal to watch the airplane fly itself. Keep in mind the King Air weighs almost twice as much as any other certificated application thus far—so much needed to be accounted for in the landing portion in terms of ensuring the stabilization of that mass prior to touchdown.

The screens turned to “calm-the-passengers” mode, and a series of gentle maneuvers linked us to the final approach course and a solid touchdown. I joked with Koss that she could surely land better than that—and it’s true. Autoland is not set up to caress the runway with the grace of a skilled—or lucky—pilot. It’s set to land firmly but safely, as if the runway were always slicked with a quarter-inch of rain.

A. The G1000 NXi installation comes first, bringing the latest software into the flight deck if not already installed.     

B. The autothrottle utilizes mechanical linkages as well as electrical components to set power for the phase of flight—or balance power between the engines.

C. Sensors and autopilot servos work behind the scenes to monitor flap and gear positions, and move flight control surfaces in response to Autoland requirements.

D. Garmin’s electronic stability and protection enters a new protocol during engine-out operations.

E. Autoland changes the displays to a passenger-centric presentation that walks the people on board through the steps of the approach and onto the landing.

How it Works

For those who didn’t read FLYING’s complete report in the January/February 2020 issue, or you want a review of what’s going on behind the scenes, here you go. The pieces of Autoland in the King Air B200 emulate those of the original installation—with a few more moving parts (and algorithms inside) to attend to the fact this is a turboprop twin we’re working with and not a single-engine turboprop or jet. In fact, the STC will mark the first certification of a two-engined aircraft, with the initial approval in the twin-engined HondaJet still in the works at press time.

First, there’s Garmin’s electronic stability and protection (ESP). The advanced aircraft recovery functionality has been built into Garmin flight decks since 2010. ESP works in the background when the pilot hand-flies the airplane. It’s independent of the autopilot but is activated using the AP’s servos. If the pilot exceeds a 45-degree bank, and ESP is active, then it will engage and nudge the flight controls to a more level attitude—and encourage the pilot to reduce the bank angle a bit. It works in a similar way with nose-up and nose-down pitch attitudes. If ESP activates for a prolonged period, the autopilot will engage in level mode.

The ESP takes on a new level in OEI management—what old school called “engine-out ops” or “single-engine ops.” Normally, the loss of power on one side triggers a bank excursion unless the pilot captures the change with appropriate rudder and aileron input—remember “dead foot, dead engine” and banking 5 degrees into the good powerplant? Well, upon the power loss, the ESP’s normal limits of 45 degrees change to 10 degrees into the failed engine and 40 degrees into the good engine, and pitch limits tighten from 20 degrees to 10 degrees pitch up and from 17 degrees to just 5 degrees nose down. Low airspeed protection kicks in at V_MCA plus 15 kias.

Second, there’s emergency descent management (EDM). EDM monitors pressurization and, in the event of a pressurization loss, maneuvers the airplane down to 15,000 feet msl or lower, unless the pilot responds.

Third, the autothrottle kicks in. The AT controls power typically by maintaining an airspeed, or a climb or descent rate, as selected by the pilot through the autopilot. In the case of Autoland, the AT continues to manage power during the descent, approach, and landing, based on target speeds, altitudes, and climb or descent rates, as called for by the system. For the King Air application, the autothrottle also balances power between the left and right engines, and monitors both to respond in the event of a power loss.

Fourth, sensors and “smart” autopilot servos work in the background. A barrage of specialized sensors monitor flap and gear positions, as well as braking sensors once the airplane is on the runway. The autopilot also features advanced servos with the functionality to be driven in very fine increments. This allows them to manage the precise vertical/descent rate and touchdown protocol required for a reasonably smooth landing.

Finally, there is a radar altimeter, already installed on the King Air. This advanced altimetry system uses the timing of radio waves to determine the airplane’s height above the ground with pinpoint accuracy. Initial testing of Autoland on previous singles attempted to manage altitude just by reference to the GPS—but the nuances of the roundout managing final feet above the runway required the precision of a radar altimeter to execute the landing properly. Perhaps future iterations of Autoland could use increasingly precise GPS for this component, but we’re not there yet.

So, back to the question posed as we sit here four years into a real, fielded automatic landing system for GA. We probably still need more time flying with the system ready in the background before we’ve contemplated all the ways it might save the day. And future versions are likely to assist us in abnormal situations rather than emergency ones—like using it to fly the airplane (without the ATC warnings) while we care for a sick passenger or upon entering weather we’re not prepared to exit properly.

One thing is for certain: Like a parachute, it’s a tool which, well deployed, can expand our reach as pilots—safely.

What’s it Going to Cost You?

Autothrottle: Starting at $44,995 (plus installation)

Autoland (assuming the G1000 NXi and autothrottle installed): Starting at $32,995 (plus installation)

Upgrading G1000 NXi to Phase II (to support AL/AT): $74,995 when purchased with the AT package

Upgrading the G1000 to the G1000 NXi: $52,995 (plus installation)

Adding G1000 NXi from scratch: $410,000 to $450,000 (depending on facility and options)

Labor estimates:
Autothrottle: 80 to 100 hours

Autoland: 200 to 240 hours

How Can it Land Itself?

With all the tech on the flight deck today, it’s no wonder that a modern airplane can perform a middling-to-decent landing on its own. But if asked when the first automated landing took place, you might be surprised to hear it: August 23, 1937.

That’s when Army Captain Carl Cranetested out his invention—an automatic landing system constructed of airborne receivers installed in a Fokker C-14B paired with a network of five radio beacons surrounding Patterson Field (now KFFO) near Dayton, Ohio.

Crane, director of the Instrument and Navigation Laboratory, and his fellow engineers put their minds to the proposal in 1935. First, in determining the system’s architecture, the group tested the electrical and mechanical components on aircraft in flight—much like a modern autopilot in cruise at first then through approach and landing. From a report filed following the successful attempt and reproduced on Fokker’s website, the process followed a similar structure to modern automatic landings:

First, a Sperry gyro pilot maintained the airplane’s directional control—which had been proven in long-distance flights from Ohio to Texas, New York, and Virginia. Regardless of the airplane’s actual heading when the pilot let go of the controls, the system captured a radio beacon signal from those transmitters that functioned much like marker beacons on an modern ILS.

Using the sensitive altimeter to fix the proper altitude, the airplane tracked inbound to the first of the string of stations, growing ever closer to the field.

For the first complete landing, Crane and engineers George Holloman and Raymond Stout took off from Wright Field (which was KDWF, near Riverside, Ohio, and now closed). As they leveled off and turned on the equipment, the Fokker traversed the roughly 5 sm over to the Patterson landing site.

The Fokker maintained altitude through a throttle “engine”—a rudimentary autothrottle interconnected with the altitude control to adjust the power setting if the minimum altitude was reached prior to Radio Station 1—the closest one to the field. After station passage, the throttle actuated again to set up a power-on glide and descent at a moderate rate until the touchdown was made at Patterson Field. At that point, switches on the landing gear actuated the throttle again, reducing power to idle. The landings were made in winds up to 11 mph and about half in “rough air.”

The C14B had certain advantages in making these trials a success. With a wingspan of 59 feet and a 525 hp Pratt & Whitney R-1690-5 Hornet radial engine, the C14B was relatively powerful when loaded to only half its normal payload—normal max gross weight was 7,341 pounds. Yet it was slow, stable, and ponderous enough in its handling to presume it would land predictably as well, mitigating tendencies to ground loop—which the report excerpt makes no note of, by the way.

Postwar Commercial Autoland

Development on an automatic landing system resumed following World War II, as the Royal Air Force formed its Blind Landing Experimental Unit (BLEU) at two military airfields in Suffolk, England—RAF Martlesham Heath and RAF Woodbridge. Using an increasingly more sophisticated autopilot to track the newly launched ILS for course and vertical guidance, rather than the beacons alone, introduced far more precision into the process. However, though the ILS’ lateral guidance could be used throughout the landing because of the way the transmitter is set up and emits, glideslope guidance ends once the airplane is over the runway threshold, leaving that last 10 feet up in the air, so to speak. Therefore, any autoland system had to begin ignoring the glideslope information once it became unreliable and transition to the radio altimeter.

From this basic truth comes the basis for the Category I instrument approach having a standard minimum altitude of 200 feet agl. Further reductions in those minimums, down to a full “zero-zero” landing, is classified as Category IIIc and requires not only the special onboard equipment and aircraft certification but also pilot training and qualification, and runway certification.

These early systems were tested on the military Vickers Varsity and Avro Vulcan, followed by the first installations on civilian aircraft, the Hawker Siddeley (originally de Havilland) HS.121 Trident, in cooperation with British European Airways. BEA had partnered with the RAF throughout the post-WWII development and made the first automatic landing in commercial revenue service on June 10, 1965, on G-ARPR, from Paris-Le Bourget (LFPB) to London Heathrow (EGLL). From there, the system was installed in the Sud Aviation Caravelle and throughout the turbojet fleets of other airlines.

The U.K. remained pioneers of sorts in utilizing automatic landing systems—driven by the poor weather and persistent low visibility experienced in the British Isles. North American airlines were relatively slow to pick up the new technology. In fact, when BEA went to scrap its Tridents and replace them with the Boeing 757, it was horrified to discover the 757 had no provision for the automatic landing system. While a dozen runways in the U.K. were certified to Cat. IIIc approaches then, only two were in the U.S., and the automatic landing system was deemed unnecessary for operations.

This feature first appeared in the October 2023/Issue 942 of FLYING’s print edition.

The post We Fly: Garmin Autoland for the Beechcraft King Air 200 appeared first on FLYING Magazine.

Back in the mid 1930s, my grandmother took her first joyride in a biplane. For $5 that she split with her best friend, Marion, Isabel Barker defied her father’s explicit instructions not to go up in one of those “newfangled contraptions” and snuck in the secret flight at the county fair in Maquoketa, Iowa. She confessed to him later, being the honest soul she was. But she never forgot that view from the front seat—perhaps a Standard.

But maybe it was a WACO model D.

She’s gone from us 7 years now, and the details remain lost to history. Alex Skiba, former sales and marketing manager for WACO Aircraft, figures many of those pilots who purchase a new WACO YMF-5 in 2023 still do so in order to use it for sightseeing operations. Similar in feel and spirit to those flights from a county fairground, the romantic taste of the sky that an open-cockpit airplane affords hasn’t lost its appeal.

And neither has the WACO.

An Introduction

The WACO takes you back into a beginner’s mind, not only because it evokes the beginnings of aviation’s golden age but also being the first airplane for many cadets facing entry into the U.S. Army Air Corps in World War II. Then, as now, WACO is an acronym, standing for Weaver Aircraft Company in honor of its original co-founder, George “Buck” Weaver, who in 1920 with Elwood “Sam” Junkin, Clayton “Clayt” Bruckner, and Charlie Meyers launched the nascent aircraft builder in Lorain, Ohio (see “The Dream Machines”). You also understand instinctively when approaching it that this flight experience will be completely different from any-thing you’ve had before.

Like preparing for a special first date, I walked through in my mind my previous piloting time in biplanes. A few hours in the stately Stearman, and a quick aerobatic flight in a Christen Eagle—that would be the sum total. My experience is not uncommon among those who choose to purchase new WACOs—like the stunning ed and blue YMF-5 featured in these pages that belongs to Ed Stadelman. As a retired airline pilot—with a 40-year career spanning from Allegheny Airlines to USAir to American, from which he last flew the Boeing 777 out of New York—Stadelman recognized his flight time flying a previously owned Cessna 206 and 310, and a few hours years ago in the Stearman, would not serve as a sufficient precursor to taking on the WACO. It’s not that it’s hard to fly compared to other tailwheel airplanes—it’s just that the sight picture is quite different with the looming cowl blocking most of the forward view from the rear seat, where the airplane is flown from.

Stadelman negotiated a 20-hour training package with the purchase of the YMF-5, and he took a tailwheel refresher course prior to beginning that tutelage—a path he recommends to anyone without significant time in a big-engined biplane.

A. The rear cockpit is laid out with most of the WACO’s instrumentation, according to the owner’s desires. But certain legacy touches, like the teak-handled control stick and flooring, echo back to the original design.

B. The “six pack” on this YMF-5 features two Garmin GI 275 electronic instruments that can be configured for IFR flight.

C. The JPI EDM 930 engine monitoring system gives detailed data from the powerplant and fuel system.

D. The Garmin GTN 750 offers a modern navigation option, even though the owner isn’t likely to file IFR in the open-cockpit biplane.

E. An S-TEC System 55 autopilot is an option, along with a second com radio to round out the IFR package.

You Need a Ladder

Yes, you need a stepladder for most any thorough pre-flight. But this walkaround absolutely requires one. And not just any ladder, but one that will allow you to check the fuel caps on the upper wing—there are at least two, and four if the owner has opted for long-range tanks. The preflight encompasses standard items for any airplane—checking the flight controls, landing gear, fuel and oil levels—but with many nuances special to a biplane with fabric covering and bracing wires.

The aircraft flight manual is 28 pages long. This is notable, as it’s about 20 times shorter than the AFM for a new FAA Part 23 certificated airplane with standard factory-installed avionics. Since everything in the panel—save for the legacy instruments such as airspeed, altimeter, and engine gauges—is an option, those supplements stand alone and are not woven into the manual. There aren’t pages of performance tables for altitudes into the stratosphere, nor are there expanded systems descriptions and pages of warnings for the pilot to wade through and heed gingerly. Maybe that’s because this particular airframe and engine have no airworthiness directives applied to them since the original type certificate was blessed by the CAA in 1934.

The preflight checklist is thorough. It goes from the front and rear cockpits to the left lower wing trailing edge, where in addition to normal checking of the wing and aileron surface and freedom of movement, the slave wire between the upper and lower aileron is addressed. Proper tension of the landing and flying wires, and the security of the interplane strut must be verified as well.

At the nose of the airplane sits the now-standard 300hp Jacobs R755 A2 7-cylinder radial powerplant, with its MT Propeller two-bladed, fixed-pitch prop attached to the hub. There’s an option for an MT-Propeller controllable-pitch version too. The manual advises against flying with less than 3 gallons of oil on board.

As a potential WACO owner, you’ll be pleased to note that those Jakes are still on the market, when it comes time for the 1,400-hour TBO. The R755 A2 can be ex-changed for an overhauled model for $36,950—or you could buy one outright for $43,950—at Radial Engines Ltd., in Guthrie, Oklahoma, for one, at press time.

A Modern Version

Instead of squinting our eyes for flocking aerial competitors around that farmer’s pasture, today’s pilots plying the trade of air tours have ADS-B to call out traffic on a series of optional avionics offered as add-ons to basic VFR and IFR packages.

Stadelman opted for a Garmin GTN 750 WAAS-enabled GPS/nav system and a second com radio, as he flies around the busy New England states from his home base at Falmouth Airpark (5B6) in Massachusetts. He prefers the modern, IFR-capable panel, though he has no plans to fly his prize in the soup. “Even on marginal VFR days, it’s nice to have,” he said. Stadelman also chose the long-range tanks—taking the normal 46-gallon capacity up to 70 gallons—so that he doesn’t need to refuel if going into a grass strip with intermittent or nonexistent services.

Other nice touches in the rear cockpit include backup electronic instruments, additional com radios, and a JPI EDM 930 engine monitoring system. For my flight test, I was paired with N577S, a 10-year-old YMF that WACO keeps for training and demonstration purposes—and virtually identical to Stadelman’s 2022 model in all the ways that mattered, including the modern displays in the rear panel.

Ready to Taxi?

Flying from the back seat actually gives you a little better forward perspective than from the front, where the cowl with its signature bumps looms closer and blocks the view almost completely. I’m up front to start to familiarize myself with the airplane while WACO instructor Bob Danielson learns more about me.

I sit up straight to no avail, then begin wide S-turns to supplement my forward view. I work our way out to the runway at Battle Creek Executive/Kellogg Field (KBTL)for a short flight over to Brooks Field (KRMY), where a vintage hangar and open grass alongside the runway will make our morning photos more historically appropriate. The tailwheel is fully steerable, which improves handling on the ground but preserves the need to lock it prior to landing—lest the airplane trend off quickly from the centerline if the wheel isn’t aligned.

Hands and Feet On Takeoff

You need to be a steady partner with any tailwheel airplane, and the WACO rewards stick-and-rudder competence. The YMF-5 will lift off before you want it to in a three-point attitude unless you firmly place the stick forward as soon as the relative wind over the elevator allows for it. My first takeoff from the front had me working as I figured out the controls, but we managed to come off after about a 1,000-foot ground roll. Liftoff speed hovers just below 60 knots, with V_X at 63 kias and V_Y at 66 kias. We cruised at about 1,000 feet agl for the14 nm hop over to Brooks for my first landing. Danielson coached me through the pattern and landing speed (about 75 kias), and I stayed on it to keep the runway in sight as we came down final. I lost the numbers under that stately cowl several beats before “normal”—and then transitioned to a side view for the touchdown, with Danielson ready on the pedals in case my sense of the rudder pressure required was inaccurate.

• READ MORE: Waco Doubles Production and Plans to Expand Product Line

In the Glorious Open Air

After a trip back to Battle Creek Exec and a lunch break at the WACO Kitchen—I recommend the Wagyu tacos, but then again, I always recommend the tacos—we set off on a true demo flight, with me taking the backseat. The WACO is soloed from the rear cockpit, and as Danielson termed it, “it’s pretty lonely up front” with nothing but airspeed and altimeter, throttle and stick to work with. The front cockpit is built for up to two passengers—and often has the front stick removed lest they get any crazy ideas. So it was truly an act of courage for him to grant me that hallowed rear pit.

I found the YMF was easier to taxi from the rear, and we made it out for an intersection takeoff without too much heartache. But I failed to push forward quite enough on the stick during the takeoff roll, and we lifted off a few knots lower in airspeed than desired. Fortunately, we made up for it in ground effect and carried on up into the blue-and-green patchwork June afternoon.

Under a scattering of fair weather cumulus, I lazed into gentle turns above Gull Lake to the northwest of Battle Creek. Though it felt like breaking the serenity of my brief moments with this considerable companion, I know that many WACO pilots enjoy the highly maneuverable biplane for its grace in basic aerobatics. We hadn’t prepped the cockpits for anything upside down—nor were we sitting on chutes—but I tried out steep turns to 55 degrees of bank and pulled the YMF into a lazy 8 or two, followed by Dutch rolls, to test out its coupling. Perhaps one of those edged into a wingover… Amazingly, for an airplane built when serious adverse aileron drag seemed like it came standard one very model, the YMF didn’t present such vagaries but rewarded even rudder pressure with smooth control.

Landing Home

We circled the lake a few times to allow for anyone on the water to enjoy the sight of a navy blue-and-old-gold biplane against the cloud backdrop. Then I called up Battle Creek Tower, and we headed back in for my first landing attempt from the rear seat. Harkening back to my days flying a Globe Swift, a tail-low wheel landing feels most comfortable to me in taildraggers—and it works well for WACO pilots too, for the most part.

Keeping a few hundred rpm of power in, I targeted 75 knots on the tape and rode down to the long runway at KBTL. I had 10,000 feet to work with, so my aim point was about halfway down the pavement—about where I’d started my takeoff roll. With a gentle lean to compensate for a breath of crosswind, I leveled off and began to feel for the ground, easing out power and taking in a measured inhalation ’til the mains touched.

Was I ready for it? The gods of wind and summer thermals were on my side, and the WACO answered my control pressures honestly. What more could you want from any return to terra firm a than that moment of joy?

Courtesy of the WACO, it can be yours to pursue.

WACO YMF-5

Price, as shown: $658,400; VFR packages start at $590,000

Engine: Jacobs R755 A2, 300 hp

TBO (with current SBs): 1,400 hours

Propeller: MT Propeller MT233R150-6AJ, fixed pitch

Seats: 1+1/2

Wingspan: 30 ft.

Wing Area: 234 sq. ft.

Wing Loading: 12.6 lbs./sq. ft.

Power Loading: 9.83 lbs./hp

Length: 23 ft., 4 in.

Height: 8 ft., 6 in.

Baggage Weight: 75 lbs. aft, 25 lbs. forward

Basic Empty Weight: 2,145 lbs.

Max Gross Weight: 2,950 lbs.

Average Useful Load: 628 lbs. (805 lbs. max)

Fuel: 46 gal. std; 70 gal. with long-range tanks

Max Rate of Climb: 865 fpm

Stall Speed: 51 kias

Maneuvering Speed:120 kias

Load Limits (at 2,950 lbs.): +5.2/-2.1

Cruise Speed: 100 ktas, at sea level

Max Endurance/Range, Max Range Power, Long Range Tanks: 450 nm at 2,500 ft. msl

Takeoff Distance, Sea Level (over a 50 ft. obs.): 1,556 ft.

Landing Distance, Sea Level (over a 50 ft. obs.): 1,650 ft.

This article first appeared in the August 2023/Issue 940 print edition of FLYING. 

The post We Fly: WACO YMF-5 appeared first on FLYING Magazine.

Much like it was during the early days of Popular Aviation—FLYING’s precursor—one of the first aviation magazines in Italy, L’Aquilone, featured plans for building model aircraft used by enthusiasts enamored by the idea of flight. These kit-built machines catalyzed the dreams of Luigi and Giovanni Pascale as they reached their majority in Campania north of Naples.

In league from the beginning, the brothers would nurture and support each other’s imaginations until they could launch their aircraft design and manufacturing efforts in 1948, 75 years ago. The Pascales built their unique airplanes at first incorporated under the marque of Partenavia in 1957—and within the company we know today as Tecnam.

Training Legacy

The latest of Tecnam’s single-engine airplanes to come to fruition, the P-Mentor, joins a legacy of aircraft destined to help aspiring pilots learn to fly. The first true Pascale design to reach production, the original P48 Astore, looks a lot like the Piper Pacer taildragger from which the brothers drew inspiration. The P-Mentor breaks from one tradition, in that it is one of the few of the Pascale designs not named after the year in which it began development—for example, the P48 sprang from the drawing board in 1948, and the P2012 Traveller started in 2012, though it didn’t see European Union Aviation Safety Agency certification until 2019, with FAA certification to follow later that year.

• READ MORE: Tecnam Unveils P-Mentor Training Aircraft

While Tecnam has enjoyed recent success in the U.S. with its modern version of the Astore LSA, and the latest edition of the P92 Echo, the P-Mentor makes a compelling case for a primary trainer that goes beyond the light sport category. The P-Mentor achieved EASA certification under CS 23—equivalent to the FAA Part 23 type certification basis for light aircraft—in 2021. Though the P-Mentor is powered by a version of the same engine found on many LSAs—the Rotax 912iSC3—the airplane’s heft and sophisticated cockpit take it up a notch from the entry-level category to create a platform that will serve to educate new pilots intent on progressing into a career—or just larger, more capable airplanes.

A. The FADEC-equipped Rotax 912iSC3 engine has an easy preflight check sequence.

B. The simulated landing gear switch is also tied to a gear warning horn to help facilitate training in preparation for more complex aircraft.

C. The Garmin G3X Touch displays can be configured in multiple ways, including a base map, engine information system, and the primary flight display. A Garmin GTN650Xi in the RNAV-capable edition enables a complete IFR training program.

D. The control sticks have a shape to them that falls nicely in the hand, and the seats are adjustable, rather than the rudder pedals, for a comfortable fit.

E. An optional Garmin GFC 500 autopilot outfits the P-Mentor for extended cross-country missions and advanced aircraft training.

A Walkaround

My introduction to the P-Mentor began on the ramp at the company’s headquarters in Capua, Italy, following a detailed production-line tour that took in several of the models in various stages of readiness for first flight and eventual delivery. Witnessing how the machines come together always gives insight to how they will perform, so I felt particularly well versed in the P-Mentor’s genesis after hearing Giovanni Pascale—managing director of Tecnam and the latest in the family line to lead the company—walk through each step in that process.

Its low-wing, side-by-side seating evokes similar LSAs I’ve flown recently—such as the BRM Aero Bristell SLSA—yet with an aspect to the way the canopy slopes into the fuselage that recalls its design heritage, as we saw earlier in the tour, from the mid-’50s designs of the firm, but still modern and inspiring confidence as you approach it on the ramp. Tecnam chose to certify the P-Mentor with a maximum gross weight of 1,587pounds, a good 267 pounds higher than the top of the LSA class. Having done so allows for a useful load of up to 628 pounds and the flexibility to have two healthy adults plus full fuel on board.

Walkaround takes in the normal checkpoints with few unique aspects to the process. Tecnam flight test pilot Massimo de Stefano oriented me to a few items, mostly to do with getting in and out of the airplane. Early Pascale designs—and all of its twins—feature a high wing, in part to aid ingress for pilots and passengers. But the low wing has an easy step-up and good handholds for settling yourself into the seats.

De Stefano guided me to the right seat, which was perfect for this review, as it allowed me to assess the P-Mentor as an instructor and see how it would perform and feel flying from that familiar CFI’s perch.

The flight deck features a twin Garmin G3X Touch installation in the complete IFR package—called the “Sport” version—that we flew with in I-PDVF, the company’s demonstrator. Those displays are accompanied by a Garmin GTN 650 Xi nav/com/GPS, a Garmin GAD 29c ARINC data module, and a remote-mounted Garmin GTX 345R transponder with ADS-B In and Out capability. All of that—in addition to the engine management system—is powered by a 14-volt electrical system that utilizes two electrically isolated alternators (A and B) and a main ship’s battery.

Startup and Taxi Out

Starting the Rotax involves a simple process, with a couple of nuances—you first flip a toggle switch to energize the starter in addition to having the master switch on. Then, it’s both FADEC Lane A and B switches on, fuel pump on, and push the red starter button to swing the prop—which caught quickly on the warm engine (from previous flights). There are separate avionics and autopilot masters as well.

Run-up was guided by the engine information display on the right-hand G3X Touch screen, checking both FADEC lanes using the 4-cylinder exhaust gas temperature readouts, along with coolant and manifold temperatures, oil pressure, and volts.

De Stefano took on the task of taxiing out in order to familiarize me with the special procedures at the Capua Airport (LIAU), both of the day—rain showers earlier left the grass runway in varying states of rough—and in general. LIAU has a flight information service staffed by the local fire brigade—and therefore non-English speakers. Unusual, but not wholly unanticipated.

We left our abbreviated flight plan with the FIS and de Stefano guided me through the first takeoff, taking a line that was relatively smooth on the left-hand half of the runway, which measures 1,097 meters, or 3,599 feet.

We took just over one-third of the runway on that takeoff roll, not bad considering the condition of the turf, which appears to be a running source of amusement amongst the Tecnam pilots and their dealers. Test flying is often frustrated by the weather at Capua, with winter rains rendering it unusable for stretches of time.

One clear benefit to the location? I saw the airplane’s performance on a truly soft field. All Tecnam aircraft must pass this test or never reach the skies at all. The local council plans to finally pave the runway sometime in the next year—and we hope that’s on schedule, though the current field has its, well, charm.

In-flight Feel

For our mission, we took off to the northeast from Runway 26 to stay clear of the military field—Grazzanise—on whose control zone perimeter Capua sits, at 64 feet msl. I had the controls through the climbout to 3,000 feet for our high work, and we saw 450 to 700 fpm at the V_X of 70 knots and power set at 28.9 inches and 5,550 rpm.

During steep turns the controls felt solid, and even between aileron and pitch (in the baseline I use, aileron control feel is usually a degree lighter than pitch). However, I found the P-Mentor easy to keep coordinated both in 30- and 45-to-50-degree-bank turns and the proper pitch attitude facile to find in each direction.

Stalls broke mildly—more of a mush in an approach to landing (power off) stall, with a level break in the departure (power on) mode. Recover came swift and sure. I performed a few additional coordination maneuvers, seeking the marriage between aileron and rudder, and with a brisk roll left and right and back to center, again, straightforward to keep the nose on the horizon in its place.

• WATCH: We Fly the Tecnam P-Mentor

I made a power-off glide at 70 knots to test that handling, and the P-Mentor preserved the good gliding characteristics of the P92 Eaglet—precursor to the Echo—that I first flew back in 2006, with a reasonable 9.7:1 glide ratio. No surprises—just honest flying.

In Cruise

Where the P-Mentor trades off its weight for performance shows up in two places—the not-quite-as-short takeoff roll, and in the modest cruise speed of 117 knots. That’s at a power setting of 27 inches MP and 5,480 rpm.

Reducing the power to 24 inches and 5,030 rpm brings us to 100 knots indicated at 2,000 feet msl and13 degrees C—nearly ISA conditions. The panel is setup for cross-country missions in the sport package we tested—and you can do so at the modest fuel burn afforded by the Rotax, which sips 3.7 gph at that economy cruise setting. The company prides itself on the efficiency of its models, which certainly holds true here.

Training to Land

One unique feature of the P-Mentor that places it squarely into the training class is the simulated landing gear lever on the pilot’s subpanel. Though the airplane’s gear remains fixed firmly in place, if you don’t actuate the gear lever to the down position when bringing the throttle to idle, a warning horn sounds—just as it would in a true retract, and it’s tested during the run-up. The idea is to ingrain each of the steps into the thinking process of a new pilot. However, one could argue that because the airplane doesn’t reflect the aerodynamic change of the gear moving and the swinging of the gear doors, it’s a tenuous transfer of learning.

However, Sporty’s sells the same portable type of device in its catalog towards the same purpose, and I suppose it holds merit for building that habit of always checking to see if the gear is down on final.

Short and Soft Techniques

The long-span flaps can be set at the takeoff position (roughly 15 degrees) as high as 106 kias, with full deflection of about 30 degrees—the landing position—at 96 knots, aiding greatly in the ability to slow the airplane.

De Stefano wanted to demonstrate a landing first (and the right line to take on the rutted field), and I was keen to try out the go-around profile of the airplane. A nice, easy approach speed of 70 knots kept us on a smooth path to the touchdown point—and I braced myself for the bounces I figured would be inevitable—but the P-Mentor’s tires handled the uneven turf with aplomb. He pushed the power up for a touch-and-go, and handed the controls back over.

We did a low approach first, and I kept myself purposefully high, and slipped on final to see if the P-Men-tor’s good coupling held true, and it did. During the pass, I flew just off of the deck by about 15 feet, so I could continue to get a sense of things. I pulled up into a nice fly-by for the folks on the Tecnam ramp and entered the pattern again, level at about 750 feet agl—about 800 feet msl.

Remembering to put the “gear” down as I throttled back, it didn’t take long to find the approach speed that seemed to give the best mix of low speed and positive control authority on final. I aimed for the good line in the grass, and I was rewarded with a pleasant touch-down—stick in my lap and a little bit of power in to keep us going as the tufts of turf snatched at the tires.

We readily made the turn off just past midfield to taxi back into the factory—and de Stefano was all smiles as I did—a mark of approval that goes beyond translation. That grin matched my own, as the P-Mentor had been a true pleasure to fly—and would likely be just as much fun to use, yes, mentoring new pilots into the skies.

Tecnam P-Mentor

Price (fully equipped, as tested): $350,750

Engine: Rotax 915iSC3, 100 hp

TBO (or equivalent): 1,200 hours

Propeller: MT V.P. hydraulic with governor, two-blade

Seats: 2

Wingspan: 29.5 ft.

Wing Area: 128.1 sq. ft.

Wing Loading: 12.39 lb./sq. ft.

Power Loading: 15.87 lb./hp

Length: 22.1 ft.

Height: 8.2 ft.

Baggage Weight: 66 lb.

Standard Empty Weight: 959 lb.

Max Takeoff Weight (EASA CS 23): 1,587 lb.

Standard Useful Load (EASA CS 23): 628 lb.

Fuel: 140 liters/37 gal.

Max Rate of Climb: 750 fpm

Max Operating Altitude: 13,000 ft.

Stall Speed (flaps extended): 44 kias

Max Cruise Speed: 117 ktas, at sea level, max continuous power

Max Range @ Max Range Power: 950 nm

Takeoff Distance, Sea Level (over a 50 ft. obs.): 1,706 ft.

Landing Distance, Sea Level (over a 50 ft. obs.): 1,280 ft.

This article first appeared in the July 2023/Issue 933 print edition of FLYING.

The post We Fly: Tecnam P-Mentor appeared first on FLYING Magazine.

Though FAA certification is still pending, the P-Mentor has made it into flight training fleets across Europe, with plans to follow in the U.S. soon. FLYING editor-in-chief Julie Boatman visits the OEM and flies the P-Mentor over the Italian countryside north of Naples (Napoli) in this pilot report.

The post Watch as We Fly the Tecnam P-Mentor appeared first on FLYING Magazine.

The icing on the lebkuchen? I’m with Martin Scherrer, head of flight operations and training for Diamond Aircraft—and we’re climbing away in the new Diamond DA50 RG. We’re speeding towards Diamond’s EU home of Wiener Neustadt, Austria, just south of Vienna, but we have cameras on board the DA62 that’s chasing us. We plan a couple of special stops along the way—those mountains keep soaring up ahead—the German Alps. It would be so wrong not to twirl a couple of turns around a chateau—Neuschwanstein, that inspired a Disney castle, for one. We’ll also tuck into the deep valley that hosts Hallstatt, on the edge of Hallstätter See, often voted the prettiest town in the world for its postcard-envy setting.

But the view from above ranks as the most stunning. As we fly over Salzberg, I can’t help but hum a few bars from the Sound of Music… with a twist: “I am sixteen going on seventeen… time to get my pilot’s license…”

Delivered

While the sweet and swift retract has been type certificated under the European Union Aviation Safety Agency (EASA) since September 2020, FAA validation came nearly to a halt during COVID. The company has delivered 38 into EASA-land while awaiting certification stateside. Diamond anticipates that to come through this summer—and one of the production models departs soon for a U.S. tour in coordination with that milestone.

READ MORE: Diamond Aircraft Receives FAA Type Certification on DA50 RG

No small part of the validation process lies in the ac- ceptance of the new Continental CD-300 jet-A burning diesel engine under the DA50 RG’s complex cowl, which looks as though an engineer blew globes in hot glass—fiberglass—and stuck them in place to shroud the massive powerplant. We’ll see glimpses of that engine during our walkaround, but during our visit to the production line a couple of days later we’ll get to contemplate its intricate architecture as it sits on serial numbers 40 and 41 about to leave the line for flight testing.

The FADEC-controlled CD-300 is the largest Continental diesel in the series to make it to EASA certification—and all 560 pounds of it comprise a substantial percentage of the DA50 RG’s empty weight. It potentially creates a long view down the nose for the pilot—but instead of being in the way, I found it helped me gauge my sight picture both during high work and landings.

WATCH: We Fly the Diamond DA50 RG

For pilots seeing the big CD-300 for the first time, it takes a moment to orient yourself. The CD-300 is liquid-cooled rather than air-cooled. Plus, a diesel engine is self-igniting, meaning there are no magnetos—so the combustion chambers must be heated to a certain temperature and maintain that baseline in order to light off. From the aircraft flight manual: “The bypass cooling circuit (cabin heat exchanger) is always active. The short cooling circuit is active at low cooling temperatures.” This ensures that a cold engine will warm up quickly, and also creates a safety benefit, using coolant rather than exhaust gas. When the coolant temperature reaches 183 degrees Fahrenheit, the external cooling circuit is activated by a valve.

Look at the large intercooler radiators on the nose and follow the orange ducting to that system inside—indicating that the CD-300 features a turbocharging system as well, driven somewhat traditionally by exhaust gas collected from a manifold. Excess gases bypass the turbine via a FADEC-controlled wastegate. A pressure sensor behind the compressor allows FADEC to calculate the correct position of the waste gate’s valve.

Diamond has had a long path to certification on its retract—15 years—because of the issues plaguing early engine partner Thielert Aircraft Engines GmbH, which originally produced the Centurion line from which the CD-300 was derived, generally speaking. Thielert went public in 2005, but by 2008 had declared bankruptcy, with its founder Frank Thielert jailed during the fracas. Centurion Aircraft Engines formed from that basis, and Continental Motors purchased those assets, bringing the 300-hp engine in development under the CD-300 moniker.

And there are interesting times ahead as the CD-300 enters service beyond the EU. The in-family engine OEM Austro Engines has had success in the DA42 and DA62, and we noted a couple of operational distinctions between the AE330s in the DA62 when we flew it.

A. The Garmin G1000 NXi suite features ESP and a blue Level button in the lower center of the instrument panel, which returns the aircraft to straight and level on autopilot, maintaining pitch and roll modes when pressed.

B. The fuel system is unique to the DA50 RG and sup- ports the operations of the CD-300 diesel engine. It draws from the left wing tank through a mechanical feed pump into the injectors, which deliver only a portion of that fuel to the combustion chambers. The unused diesel returns via a common fuel line to the right tank, or as determined by the fuel selector position.

C. The load level is managed by the power lever, which meters fuel required, controls prop pitch and feathering, and adjusts the twin turbochargers in accordance with demand, given the altitude and flight condition.

D. The front seats can recline somewhat, but proper pedal position is adjusted electrically on a long rail that accommodates a wide range of pilot sizes.

E. The optional flight management system keypad tucks into the center armrest console and must be stowed for takeoff and landing.

Fuel System

It takes a dedicated system to deliver fuel to a CD series engine, one that’s plumbed and pumped quite a bit dif- ferently than the standard left-right-both (sometimes) that gasoline engines in light singles use. There’s a tank in each wing, but instead of thinking of them as left and right, they are the main and the aux.

The powerplant draws fuel from the main tank in the left wing through an electrical feed pump to the engine-driven mechanical pump into the injectors, which deliver only a portion of that fuel to the combustion chambers. The unused diesel returns via a common fuel line to the main tank via the aux tank for heat exchange, or as determined by the fuel selector position. Normal on the fuel selector draws from the main; the Emergency position takes fuel directly from the aux tank. The Off position cuts off the fuel supply entirely.

Since you’re drawing from the main and only returning part of that fuel to that tank, a fuel imbalance will grow beyond the airplane’s ability to maintain lateral balance. Before the 9-gallon limit, the pilot turns on an electric transfer pump to move fuel from the right wing to the left—but not during takeoff and landing.

Flight Controls

My overall impression of the airplane’s handling finds a good balance between the nimbleness you desire for hands-on flying—to tackle a crosswind, for example— with the stability to make it quite comfortable on a long cross-country flight off the autopilot.

The length of the stick and its connection to the rest of the flight control system may have a lot to do with this. I move regularly between aircraft that utilize a yoke and one with a center stick, and find little transition time is needed for me—but the yoke-controlled aircraft is more of a cross-country machine, while the one in which I use a stick is highly maneuverable.

The stick in the DA50 RG is also a bit taller than the one I usually fly with, putting the push-to-talk trigger-style button and electric trim split rocker switch a wee bit of a stretch for my short thumb if I rested my left arm on my leg. It took me a couple of flights to find the sweet spot—and maybe because this was an almost-confirming prototype, it explains why the stick in the DA62 I also flew during my visit felt a bit shorter and thus just slightly easier to find that spot on.

However—when we got out of the cross-country mode on my first flight from EDNY to LOAN and into a bit of stationkeeping, I really appreciated the stick and its direct feedback—in a straight line to the control cable bellcrank rather than the up and down movement of the yoke. These are fine details, but I think a clear reason why some pilots prefer a given airplane over another.

READ MORE: The Diamond Aircraft Story Continues to Evolve

The idea came home to me the next time I got into the TB-30 model I sometimes fly—that direct control gives confidence in both aggressive and finely-tuned maneuvering flight. In the DA50 RG, it’s somewhat dampened by the aileron actuation—and a bridge between worlds.

Therefore my final assessment makes sense—that if you are looking for a solid performer that makes you feel like you’re still flying an airplane rather than pushing buttons and managing systems, the DA50 RG will resonate with you.

Diamond aircraft take their DNA from the gliders that formed the core product line when the Austrian OEM first launched its H36 then the Super Dimona HK36 in 1980 (see “The Diamond Story”). One out- come? Advanced aerodynamics in the wings add significantly to the DA50 RG’s excellent low-speed handling characteristics and reduced approach speeds.

For example, the DA50’s flaps consist of two pieces—an inner part attached to the center wing, and the outer part to the wing itself. The sections are independently pushrod controlled, and they slide out and back to produce two tiered channels for the air to flow through, ensuring adhesion to the upper surface of the flap along with the increased camber for the wing overall.

Cross-Country Cruising

The DA50 RG has been one of the first new single-engine retracts to hit the category—with the Pipistrel Panthera also currently seeking approval beyond EASA—since the FAA granted type certification to the Mooney Ovation 3 in 2007. Besides looking great, there’s one solid reason to put the gear in the wells—speed.

In cruise, that speed comes to call. The airplane has an operating altitude maximum of 20,000 feet, but most pilots will flight plan below the oxygen-required flight levels—so it’s a good thing that the DA50 RG finds a sweet spot at 10,000 feet msl, where it easily makes its 172 ktas book speed. We conducted formation work for much of our 2.3 hours from EDNY to LOAN at lower altitudes, like 7,500 feet, and ticked off true airspeeds between 160 and 167 ktas at 90 percent load.

Diamonds burn diesel for reasons of efficiency and economy—as well as the ability to source fuel virtually anywhere—and so we also pulled the CD-300 back into economy mode. At 60 percent load, 5,500 feet msl, and ISA plus 8 Celsius, we made 156 ktas, above book—and using 10.1 gph. Pulling back to a loitering speed of 119 ktas and 45 percent load at that altitude and condition, and fuel flow drops to 7.9 gph. Our precise Austrian friends have built on this efficiency philosophy throughout their model lineup, and the DA50 RG fits right in.

On Landings

Sight picture on landing feels straightforward not only for a pilot transitioning up the Diamond food chain, but also from other four-seat fixed-gear aircraft like high- wing Cessnas and the PA-28 series. With a substantial engine out front, you have cowl references to use while determining your height above the runway (the DA50 RG definitely sits tall on its gear) without cheating a glance to the side. I found it easy to find the mains for a normal landing, as well as during the specialty take- offs and landings we performed.

Approach speeds fall firmly where you’d expect them to in the category, and the runway at Wiener Neustadt—a VFR-only airport at 896 feet msl—is 1,067 meters (3,500 feet) long, which the airplane handles easily, flaps or not.

In fact, the no-flap landing demonstrates the power of the flaps, but also the general characteristics of the wing itself. Maintaining a higher approach speed of 94 knots indicated (versus 85 kias with takeoff flaps and 77 kias with full flaps) translates into more runway used—but still comfortably within touch-and-go territory on that 1,000 meters of pavement with a ground roll near book of half the runway distance (1,700 feet) at our lighter takeoff weight (roughly 3,950 pounds, about 500 pounds below the max takeoff weight of 4,407 pounds).

A short-field landing test with full flaps easily placed us with a ground roll of less than 600 feet—the 17 knots less for VREF plus good hydraulically actuated disc brakes combined to improve pilot confidence when taking the DA50 RG into airports of modest scale.

Haul the Whole Fam

We had four healthy adults and a week’s worth of show gear on board the DA50 RG on our departure from EDNY—along with full tanks. There was no compromise required. And the three seats across in the back made for a very comfortable ride for our colleagues enjoying the Alpine traverse. This was one of the more surprising revelations of flying the new model. The time to market with the right engine has meant time for Diamond’s engineering to dial out really important parameters—and the loading capability is one big one.

There is a combination of compartments in the rear cabin to work with, up to 198 pounds total.

For pilots completely satisfied with the DA50 RG’s range and carry-all flexibility, it could certainly prove a worthy companion for a long relationship. But with its honest low-speed handling enticing you to hand-fly more often, and a landing attitude common to both previous aircraft and what you might step up to—say, the Epic E1000 GX, Daher TBM, or Piper M-Series turboprops—it sets the stage for more real piloting to come. 

DIAMOND DA50 RG

Price, as tested: $1,237,650
Engine: Continental Diesel CD-300
Propeller: MT Propeller MTV-12-D/210-56, wood with composite coating, three-blade constant speed
Horsepower: 300 hp maximum power, 272 hp maximum continuous power
Seats: 5
Length: 30.31 ft.
Height: 9.69 ft.
Wingspan: 44 ft.
Wing Area: 176.85 sq. ft.
Wing Loading: 24.91 lb./sq. ft.
Power Loading: 14.69 lb./hp @ 300 hp
Cabin Width: 4 ft. 2.8 in.
Cabin Height: 4 ft. 2.4 in.
Max Zero Fuel Weight: 4,189 lb.
Max Takeoff Weight: 4,407 lb.
Empty Weight: 3,175 lb. (depending on options) Max Baggage Weight: 165 lb./33 lb.; 198 lb. total separated into 4 areas/compartments Useful Load: 1,232 lb. (depending on options) Max Fuel: Usable: 49; Total 51.5 USG
Max Operating Altitude: 20,000 ft.
Max Rate of Climb, MTOW, ISA, sea level: 786 fpm Economy Cruise Speed at 60% Power: 156 ktas, 2,300 rpm, ISA, 10,000 ft., 10.1 gph
Max Cruise Speed: 90% Power: 172 ktas, 2,300 rpm, ISA, 10,000 ft.
Max Range: 750 nm with 30-min. reserve
Stall Speed, Flaps Up: 71 kcas @MTOW
Stall Speed, Full Flaps: 58 kcas @MTOW
Takeoff Over 50 Ft. Obs: (ISA, sea level, MTOW) 2,408 ft.
Landing Over 50 Ft. Obs: (ISA, sea level, max landing wt.) 2,224 ft.

This article first appeared in the June 2023/Issue 938 of FLYING’s print edition.

The post We Fly: Diamond DA50 RG, the High-Performance Retract That Shines appeared first on FLYING Magazine.

They represent some of our most precious resources in aviation, and a collection of more than 11,000 volunteers coordinated by the RAF have helped maintain them and promote them to the flying community.

Join FLYING’s editor-in-chief Julie Boatman as she flies in with a work crew in a Daher Kodiak 100 to experience the camaraderie and satisfaction that participating in such an important effort can bring.

Look for the full story in our feature in the latest issue of FLYING, Issue 944 for December 2023/January 2024. Subscribers will receive it in their mailbox or inbox soon.

The post We Fly: The RAF at 20 Years Into Moose Creek appeared first on FLYING Magazine.