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    Aviation

    Airplane Intel Podcast – Aviation Podcast

    Welcome to The Airplane Intel Podcast, the only aviation podcast that helps aircraft buyers, owners, and operators make smarter, more informed decisions. On the show, we compare airplanes, interview airplane owners, and industry experts and, of course, share our real-world tips as professional pilots and mechanics working in the field with aircraft buyers and owners.

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    Copyright: © 2016-2019 Airplane Intel, LLC

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    Latest Episodes:
    033 - Aircraft Turbocharging + More | Aviation Podcasts Dec 08, 2017
    Show notes

    Access Airplane Intel Podcast Show Notes here


    032.5 - The Cessna Cardinal Part 2 | Aviation Podcast Nov 21, 2017
    Show notes

    This week, we hear from our friend Arthur Billingsley to continue our conversation about the Cessna Cardinal. Art tells us what it was like to own, fly and maintain a Cessna 177RG, and why he chose the Cardinal over competing aircraft such as the Mooney 201 and Piper Arrow.


    032 - The Cessna Cardinal, 1090ES, Aircraft Polish + More | Airplane Intel Podcast Nov 13, 2017
    Show notes

    Access the Show Notes here


    031 - Hawker/Beechjet 400, WAAS, Thrust Reversers + More! Oct 25, 2017
    Show notes

    Access the Full Show Notes Here!

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    This week, we discuss one of the most interesting light jets in the sky, the Hawker/Beechcraft 400, with corporate pilot and aircraft manager Mark Feldman. Mark also tells us about his Boeing Stearman, which you won’t want to miss. Then we talk about WAAS in our new segment Alphabet Soup. Plus, aircraft ownership news, Don’s Tip of the week, and your feedback.

    More about the Hawker/Beechjet 400

    The aircraft was originally designed in 1977 by Japan’s Mitsubishi, the same company that built the MU-2 turboprop. The new jet was designated the MU-300 with an eye to reassembling it in Texas with Mooney. Mooney went bankrupt and Mitsubishi went it alone at its manufacturing plant in San Angelo, Texas, rebranding the aircraft the Diamond one and getting FAA certification in 1981. The airplane featured a flat floor and a squared oval fuselage that gave passengers more shoulder room and made the 305-cubic-foot cabin seem larger. Overall luggage capacity is 800 pounds. The Diamond featured other innovations not typically seen on light jets of its day: a supercritical wing with a 20-degree sweep to cut drag and increase speed; roll spoilers, which assist with high-speed turns; and anti-skid brakes.
    1977 Mitsubishi designed and built two prototypes of a twin-turbofan business aircraft designated the MU-300, the first flying on 29 August 1978. A cantilever low-wing monoplane with a pressurised fuselage and retractable tricycle landing gear, the MU-300 was powered by two JT15D-4 turbofan engines, Mitsubishi Heavy Industries’ MU–300 Diamond has roots dating back to 1969, when the company analyzed the same market Cessna was targeting with its Citation line. Cessna, however, got a huge lead on Mitsubishi when it came time to start pushing airframes out the door—nearly a decade, in fact. Much of the delay was meeting rigorous Part 25 certification rules the FAA had imposed. Diamonds emerged some 500 pounds heavier than target weight. Unlike Cessna, which installed a straight wing on its Citation line at the time, Mitsubishi’s Diamond used a large cabin on a swept wing to differentiate its entrant. Standard accommodation was provided for a crew of two and seven passengers. At the end of the development programme the prototypes were dismantled and shipped to the USA, where they were reassembled by the company's US subsidiary Mitsubishi Aircraft International Inc. Redesignated the Diamond I, the two aircraft were used in the US certification programme, which was granted on 6 November 1981. Initial customer deliveries began in July 1982 and 62 were built. Don was at the Beechcraft airport in Wichita viewing one of the first built in the USA, in the after show. Don has a story about that.
    Beech was decidedly behind the power curve and needed to play catch-up. Its solution: buying the Diamond program from Mitsubishi in 1985 and acquiring kits to assemble 64 aircraft. These are known as Beechjet 400s. In 1991, Beech began native manufacturing of the airplanes with a few improvements; these are called 400As. That same year, the Air Force ordered 211 Beechjet 400As to use as trainers for tanker and transport pilots (the 400T or T-1A “Jayhawk”).
    In 1983, the manufacturer launched an improved model, the Diamond IA, which featured uprated Pratt & Whitney Canada JT15D-4D engines and first-generation glass-panel avionics. The next iteration, the Diamond II, offered more fuel capacity and still more powerful engines.
    The 400A, later rebranded the Hawker 400XP by Hawker-Beechcraft, introduced improvements. These aircraft begin with serial numbers “RK” and range in price on the used market from as little as $700,000 to $2.5 million for a Hawker 400XP from 2010, the last year they were produced. Production of the XP began in 2003, and if you don’t want to invest in a complete makeover, this is the model to buy. It features Rockwell Collins Pro Line 4 avionics and an updated interior.
    Similar to its MU–2 stablemate, the Diamond uses nearly full-span flaps to lower approach speeds while utilizing spoilers for roll control. This allowed the Diamond to keep approach reference speeds within a reasonable range, while the swept wing allowed the Diamond to best the Citation II’s high- speed cruise by about 50 knots at a nominal fuel penalty of 13 gallons per hour.
    Pilots loved that the Diamond was fast and easy to fly, while passengers raved about the large cabin with a trenchless floor. Comfort is enhanced by a 9.0 psi cabin differential, providing sub-6,000-foot cabin altitudes at typical Diamond cruise altitudes in the mid to upper 30s. It’s certified to FL410.
    Beechcraft, which created follow-on designs—the Beechjet 400, 400A, and Hawker 400.
    Then called the Beechjet, it falls into the light-jet category: two pilots, up to seven passengers, a range of up to 1,885 nautical miles (with the throttle pulled back; otherwise plan on a little more than 1,400 nautical miles with four passengers) and a top cruise speed of 465 knots. More than 600 have been produced for civilian use. It is currently being remanufactured with many improvements by Nextant Aerospace as the 400XTi and by Beechcraft as the 400XPR
    The 400XTi is essentially a Beechjet 400/Hawker 400A/XP with new Fadec-controlled 3,050-pound-thrust Williams International FJ44-3AP engines replacing the original 2,965-pound Pratt & Whitney Canada JT15D-5Rs, aerodynamic improvements to the nacelles and pylons, a new Rockwell Collins Pro Line 21 flight deck, fresh interior and other enhancements. The jets undergo 60 engineering changes, replacement of more than 40 time-controlled components, compliance with A-, B-, C- and D-check inspections as well as compliance with all FAA airworthiness directives and applicable manufacturer service bulletins during a 6,000-man-hour renewal/overhaul process. The resulting remanufactured 400XTi carries a two-year tip-to-tail warranty (three for the engines), which can be extended to five years as an option.
    The first remanufactured version was the 400XT, but last year Nextant introduced the 400XTi, with an improved and more spacious composite cabin shell that takes full advantage of unused space in the fuselage, a new noise insulation package, Nextant-designed winglets, Luma Technologies LED warning panels and a Mid-Continent Instruments LCD standby attitude module and True Blue Power MD835 lithium-ion backup battery units. The MD835s eliminate a 90-day inspection interval for the jet’s original lead-acid backup batteries.
    An improved version, the Diamond IA, fitted with uprated JT15D-4D engines giving overall performance increases, an EFIS cockpit and with maximum take-off weight increased to 7361kg, was announced in 1983 and the first of 27 built, distin guished by the extra port side window, was delivered in 1984. With an MTOW reduced to 7157kg, but with extra fuel, and more powerful JT15D-5 engines, a further eight aircraft were pro duced as the Diamond II. However, in December 1985, Mitsubishi sold the Diamond II design rights to Beech, together with components for 64 aircraft. These were assembled at Wichita and marketed as the Beechjet 400. Beech then initiated full manufacture of the type and by the beginning of 1991 had received orders for 113 slightly modified Model 400As In February 1990 the US Air Force chose the type as the airframe. element of the Tanker/Transport Training System under the designation Beech 400T T-1A Jayhawk. The USAF requirement is for 211 aircraft and the first of these was delivered in July 1991 and entered service in March 1992, training KC-135, C-5, KC-10 and C-17 crews. Performance-wise, the Diamond IA is good for 420 knots at FL350 to FL370 on about 1,200 pounds per hour. There’s enough fuel for three hours at high-speed cruise or about four hours at long-range cruise.

    There is a comparison chart of the deferent models. Buy the remanufactured Nextant Aerospace, as the 400XTi and by Beechcraft as the 400XPR. Just visit our show notes, for the details. And for more history and stories about Don’s involvement in these jets. Don reveals stories of his experiences with these jets, for our patreon subscribers.


    030 - TBM-700 vs. Piper Meridian + More! Oct 09, 2017
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    This week, we’re talking about single-engine turboprops with a side-by-side comparison on the Socata TBM-700 to the Piper PA-46T Meridian. Then we introduce a new segment called the Alphabet Soup. Also, there’s a new AD out there that might affect your ELT. Plus, aircraft ownership news, Don’s Tip of the week, your feedback, and an aftershow.

    Closer Look: TBM700 vs. Piper Meridian

    If you’re looking for an upgrade in speed, range, and comfort from your high-performance piston such as a 210, Bonanza, Cirrus, or Saratoga, both aircraft will fit the bill. The TBM and Meridian may appear on your list of candidate aircraft because, as you might expect, they have a lot of similarities. For example, both aircraft feature a pressurized cabin with room for six, a low-wing design and a single Pratt & Whitney PT-6 engine bolted to the front end. However, the similarities really stop there. As we’re about to find out, each aircraft fits a different mission and is really intended to fill the needs of two different markets.

    Let’s start with a quick background on each aircraft.

    First the TBM-700. The 700 was the first of a new generation of single-single turboprop aircraft from Socata. It first flew in 1988 and was introduced to general aviation in 1990. As of the beginning of this year, 822 aircraft have been produced and delivered. While this aircraft has evolved into more sophisticated, higher performance variants such as the TBM-850, 900, 910, and 930 respectively, the later generation aircraft are outside the scope of this discussion. Why? Primarily because of price. A new TBM930 is a $4 million airplane, whereas an early model TBM 700 can be acquired for under $1 million. Now before we dive deep into the performance specs of this airplane, let’s put things into perspective with a brief history lesson.

    You might be surprised to learn that the TBM-700 is the direct descendent of the Mooney 301, a prototype aircraft built by Mooney in the early 1980s. The Mooney 301 was designed to be a six-seat pressurized single-engine piston-powered airplane capable of flying 260 knots at flight level 250. If you’ve never heard of a Mooney 301 or seen pictures, visit the show notes. You’ll see a lot of similarities in design features between the TBM and this Mooney 301.

    Unfortunately, the 301 never saw production following financial troubles and Mooney’s eventual acquisition by French owners. The now French-owned Mooney launched a joint venture with French manufacturer Socata called TBM International. To this day, the “M” in TBM stands for Mooney. The team’s objective was to develop a larger turboprop version of the Mooney 301 to be called the TBM-700. Designers and engineers began working on the aircraft with several priorities in mind: speed, performance, and reliability. I would say they got it right—the “700” in TBM-700 stands for the 700 shaft horsepower PT-6 engine bolted to the front end. However, the partnership between Socata and Mooney did not last long. In May of 1991, Mooney withdrew from the program leaving Socata as the primary company involved in the project.

    Upon entry into service in 1990, the TBM was the first production single-engine turboprop on the market, and still among the fastest turboprop airplanes in the sky. During the first few years of production, the TBM was a big hit among owner-pilots, corporate flight departments, and charter operators alike. However, the aircraft did not have good maintenance or parts support in the United States. Socata recognized their shortcomings and intervened. After listening to customers, Socata decided to invest in building company-owned maintenance support facilities and a network of parts distributors in the United States. As a result, TBM-700 sales increased dramatically.

    While I’ve also mentioned the subsequent TBM models that followed the 700, there are actually a number of variants and configurations of the 700. The first model was the 700A, which had a gross weight of 6,579 lbs, seating for up to seven, range of about 1,300 nautical miles, and a cruise speed of 290 knots. The aircraft featured a Pratt and Whitney PT6-64 engine, capable of, you guessed it, 700 shaft horsepower.

    Next came the 700B. The most obvious change to this aircraft was the large cabin entrance door that replaced the smaller entrance door found on many jets. The new entrance door is significantly larger – in fact, it resembles more of a cargo door than a passenger entrance door. Nevertheless, the new addition was a smart one – every subsequent TBM model now has this door. Other improvements made to the 700B include an increase in zero fuel weight and a nicer cabin.

    Next came the 700C1, which featured minor improvements such as the addition of an unpressurized cargo compartment and new air conditioning system. Then came the 700C2 with an increase in maximum takeoff weight from 6,579 lbs to 7,394 lbs. Finally, the 700N was produced which later became known as the TBM-850 featuring a flat-rated 850 shaft horsepower PT6-66D engine.

    As far as construction, the TBM is primarily a traditional metal airplane with tail surfaces constructed out of composite honeycomb. The flaps are another interesting talking point. They consume nearly 80% of the wing’s trailing edge. These wide-span fowler flaps help get the aircraft’s stall speed down to an impressive 65 knots. Roll control is still more than adequate despite their small span thanks to the implementation of roll spoilers on the upper surface of each wing.

    As far as systems and avionics, the earlier TBM feature a Bendix EFIS system. Most aircraft have been upgraded to Garmin GPS navigators such as the 530 and 530 WAAS. The fuel, ice protection, and environmental systems were designed to be simple and mostly autonomous – even the fuel selector automatically switches tanks to keep you balanced.


    While it’s possible to get into an early-model TMB-700 in the mid $700,000 range, but the average price for these aircraft is still in the $1.6 million range. What do you get for that sort of investment? Well, you get a full-seats range of about 975 nautical miles with useful fuel of about 274 gallons, average block speed of about 280 knots, and fuel consumption of about 50-55 gallons per hour. You can fly up to 31,000 feet with a full-fuel useful load of about 640 pounds. The cabin is ten feet long, four feet wide, and just over four feet tall giving about 143 cubic feet of room. You also have 35 cubic feet of internal baggage space and an additional five feet externally. Not to mention a gorgeous cabin fit for a King – or a queen. And the pressurization system on these aircraft is quite good, giving you a 2,500 foot cabin at 18,000 feet and an 8,000 foot cabin at FL300, with a max delta of 6.2 psi.

    TBM owners can also join the TBM owner club TBMOPA for great support, documents, and training resources. And speaking of training, like any high-performance airplane, training is a must! In fact most insurance companies will deny coverage unless you’re instrument rated and attend initial and recurrent training on the aircraft from a reputable organization such as Simcom.

    Obviously the TBM is a lot of airplane for the money. But what about ownership costs? Well 700 shaft horsepower provides a lot of speed, but for a price. I already mentioned fuel burn is around 55 gallon per hour for typical cruise altitudes in the mid-20s at maximum cruise power. Obviously this is an average figure that is subject to change based on outside temperatures and weight. At lower power settings, you can see about 46 gallons per hour. For long-range cruise, you can expect about 240 knots burning only 35 gallons per hour At $5 per gallon, fuel burn will run you between $175 and $275 per hour. Moreover, 700 horsepower doesn’t come cheap in terms of maintenance, either. Depending on inspection programs, the PT6-64 has a TBO of either 3,000 or 3,500 hours, and the cost for an overhaul is about $400,000 which comes out to about $115 per hour in engine reserves. On average you can expect to budget for about $40,000 per year in maintenance, with a total variable cost of about $234,000 per year. If you fly 300 hours a year you can expect to see about $700 per hour in variable costs. Additionally, new paint and interior can run about $50K.

    Shifting gears to the Meridian, we already covered the Piper Meridian in episode 004, and it’s little brother the Malibu in episode 002. So if you’re interested in a more detailed look at the Meridian, have a listen. But here’s what you need to know: The Piper Meridian is a turboprop variant of Piper’s PA-46 Malibu. Introduced in 1997, the Meridian is a 6-place pressurized high-performance single-engine turboprop equipped with a Pratt PT6-42A engine producing 500 shaft horsepower. Officially designated the PA-46T-500, the aircraft can fly 260 knots for up to 1,000 nautical miles. Like the TBM, the Meridian has undergone a myriad of improvements over the years including subsequent models with upgraded avionics and increases in power.

    Now let’s compare these aircraft side-by-side to see which one meets your needs. When it comes to choosing an airplane – whether it’s a single-engine piston pusher or a jet, it all comes down to what you need the airplane to do and which airplane can do the job most effectively. For this comparison, we’ll look at an early-model TBM700B and a circa 2000 model Meridian. Both aircraft can be acquired for about $750,000, both aircraft have 6 seats, and both can fly at 30,000 feet for close to five hours.

    The TBM has a cabin volume of 140 cubic feet where the Meridian comes in at 120. Pressurization in the TBM is also slightly better at 6.0 psi where the Meridian has a 5.5 psi system giving you a slight increase in cabin altitude in the Meridian. Speed clearly goes to the TBM with 200 extra ponies out front for a maximum cruise speed of 292 knots true compared to the Meridian’s 260. However, that speed really does come at a price. The TBO on the TBM’s -64 engine costs about $400K to overhaul, giving us an engine reserve of $115 per hour where the Meridian’s -42A is half that for a reserve rate of about $56 per hour.

    The TBM has a gross weight of 6,500 pounds compared to the Meridian just shy of 5,000. The TBM wins again in the useful load category – 2,554 pounds with a full fuel payload of 699 pounds. On the other hand, the Meridian’s useful load is 1,490 pounds with a payload of 350 pounds. And speaking of fuel, the TBM has room for 280 gallons compared the Meridian at just 170. Fuel burn for the TBM is 50-55 gallons per hour on average, where the Meridian is right at about 42 gallons per hour. That means the Meridian is about 26% better on fuel for just a 12% loss in speed compared to the TBM. You can expect to spend about $0.97 per nautical mile on the TBM compared to about $0.83 per mile on the Meridian. In car speak, the TBM gets around 5.5 nautical miles per gallon (NMPG) compared to the Meridian at 6.5. However, if you need to get in and out of shorter strips, the TBM has the Meridian beat. According to the book, the TBM only needs 2,034 feet to clear a 50 foot obstacle in normal conditions. The Meridian would need 2,775 feet for the same runway. Landing distance is also marginally better on the TBM.

    Finally, avionics are different for both aircraft. The current generation of both airplanes come standard with the Garmin G1000 package, but in the earlier-generation aircraft that we’re talking about aren’t as sophisticated. All TBM-700s come standard with a Bendix two-tube EFIS where the earlier Meridians had either a Meggitt EFIS system with Bendix radar, GNS530s and either an STEC 550 or Meggitt 1500 autopilot. Models between 2006 and 2010 were equipped with a fully glass Avidyne Entegra package. Both the TBM and the Meridian can be retrofitted with upgraded avionics such as Garmin’s G600 and GTN650/750s, which also reduces weight and improves useful load.

    What about ADs? Well, like any production airplane, there are ADs. Both aircraft have a number of ADs that you’re going to want to watch out for including recurring ADs. And by the way, when calculating your annual ownership costs, be sure to include the cost of complying with recurring ADs and scheduled inspections. You can budget that in as part of your hourly costs or simply include it as a fixed expense. Most AD notes that come from the FAA include a ballpark figure for complying with the AD. While it’s not 100% accurate, it does help by giving you a starting point. Finally, remember that all aircraft are to be evaluated on condition – meaning that the overall condition, value, airworthiness, and inspection status of every aircraft is different. You can get a head start of what to watch out for by going to the FAA.gov website and searching for service difficulty reports and special airworthiness information bulletins. These items will give you some idea of what to look for when looking at an airplane. Of course, we can help you navigate through all that stuff as well.

    So which aircraft should you choose? That really depends on what you need the airplane to do, your list of priorities (i.e. avionics set up, speed, costs, performance, range, and useful load), and the price you’re willing to pay. Yes, you’re going to go a bit faster in the TBM and cover more distance in slightly more comfort, but you can expect to pay up to twice as much for such conveniences. In this instance, each aircraft has its pros and cons. Bottom line is the Meridian is a more efficient and cost-effective airplane for most owner-flown mission profiles. In fact, the Meridian is the least expensive out of all the production single-engine turboprops on the market – and you can get one for less than many newer piston singles. That said, it is up to you to do your homework or enlist the expertise of someone to do it for you so you can be sure you get the airplane that best meets your needs and fits your budget.

    Welcome to The Airplane Intel Podcast, the weekly General Aviation podcast for aircraft owners, operators, pilots and mechanics. We deliver practical advice, tips and strategies to make aircraft ownership simple, safe and cost effective.


    029 - The Cessna 310 w/ Owner/Pilot Art Billingsley, 3 Tips for More Speed + More! Sep 19, 2017
    Show notes

    This week, we interview Arthur Billingsley, the pilot and owner of a 1974 Cessna 310Q. Together, we’ll get the inside scoop on what it’s like to own, maintain, and manage a piston twin. Then I share some ideas for getting more performance from your airplane. Plus, aircraft ownership news, Don’s Tip of the week and your feedback.

    Access the Full Show Notes Here

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    Welcome to The Airplane Intel Podcast, the weekly General Aviation podcast for aircraft owners, operators, pilots and mechanics. We deliver practical advice, tips and strategies to make aircraft ownership simple, safe and cost effective.


    028 - The Piper Arrow, New Live Stream + More - Airplane Intel Podcast Sep 09, 2017
    Show notes

    This week, thanks to a listener request, we are covering the Piper Arrow series of single-engine airplanes. We also talk about a new weekly live stream series we want to start for current and future aircraft owners, as well as aircraft mechanics and pilots. Plus, aircraft ownership news, the tip of the week, and your feedback.

    Access the Full Show Notes Here

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    More About the Piper Arrow:

    The venerable Piper Arrow is a four-place, high performance, complex single-engine airplane loved by many pilots and owners. It has seen a lot of use for flight schools for commercial pilot training, as well as owners needing a little more performance. As Don alluded to, the Arrow may be a logical step up from your Skyhawk or Cherokee when you need a little more speed and useful load.

    Now some of you out there may be considering a Piper Arrow after owning or flying a Cessna product. Obviously there is much debate over the handling characteristics of a high-wing versus a low-wing airplane, as well as other factors such as visibility and accessibility. Fortunately, I’ve put a video into the show notes that goes into a lot of detail of the features, pros and cons of high-wing and low-wing airplanes that may help you get a better understanding of the advantages and disadvantages of both types. You can find that video under the “Bonus Video” section of the show notes.

    If you’re looking at purchasing a Piper Arrow, you’re also likely to be looking at other four-place high-performance aircraft such as the Cessna 182, Commander 112TC, Mooney M20 or Beech Bonanza. But it’s safe to say that Piper got virtually everything right with the Arrow series. The Arrow represents an easy-to-fly airplane with a well-balanced budget for performance and efficiency. The Piper Arrow is the big brother to the Piper Cherokee, officially designated the PA-28R. As with many Piper’s, the “R” is the designation for Retractable Gear. Now the Piper Arrow has undergone many revisions since its inception in 1967, including engines, interiors, systems, and even tail sections.

    The first in the series designated the PA-28R-180 equipped with a four-cylinder fuel injected Lycoming IO-360-B1E engine, producing 180 horsepower with a gross weight of 2,500 pounds. Two years later, the Arrow was upgraded with a 200 horsepower Lycoming IO-360-C1C engine, accompanied by a gross weight increase to 100 pounds. Being 200 horsepower, this version of the Arrow is considered a high-performance aircraft, requiring a check out and endorsement. It’s also a great airplane for commercial pilot training.

    The Piper Arrow II was certified in 1971 and includes a five-inch fuselage extension from the earlier model. The Arrow II is equipped with the Lycoming IO-360-C1C engine, producing 200 horsepower with some models having a –C1C6 engine. The Arrow II has a gross weight of 2,650 pounds and also features a larger horizontal stabilizer and wider wingspan.

    The next in the series is the Arrow III, officially designated the PA-28R-201, was certified in 1976. The biggest difference in this version is a gross weight increase to 2,750 pounds. Now the Turbocharged version of the Arrow III was certified and produced concurrently to the normally aspirated version. The turbocharged Arrow III, designated the PA-28R-201T, features a Continental TSIO-360-F or –FB engine. Both engine versions produce 200 horsepower with a gross weight of 2,900 pounds. Obviously if you do a lot of high-altitude flying, or do a lot of flying in and out of high density-altitude airports, you’ll want to consider the turbocharged version.

    Next on the list is the Arrow IV. The normally aspirated Arrow IV featured the same Lycoming IO-360-C1C6 engine, producing 200 horsepower and gross weight of 2,750 pounds. But the most notable difference between the Arrow III and the Arrow IV is the IV’s love-to-hate t-tail. More on thetail later. Again, the normally aspirated IV was produced concurrently with the turbocharged version featuring the TCM TSIO-360-FB engine with the same performance and gross weight. The Arrow IV series also saw minor changes to the cabin and cockpit.

    Now the Arrow IVs were built non-stop until the end of 1983. Thanks to the economic downturn in the early 1980s, Piper ceased production of the Arrow until 1989 when 27 more aircraft were delivered. In 1990, Piper traded the T-tail for a conventional tail and delivered 15 more aircraft between 1990 and 1994 before production ended. Following Piper’s bankruptcy, the Arrow went back into production with an upgraded panel and other features, none of which include a factory autopilot.

    It’s probably safe to say that the Arrow isn’t the fastest, roomiest, or even the most aesthetically- pleasing airplane, yet it has enough of those qualities to contribute to its nearly 50-years of popularity. According to AvWeb, “The Piper Arrow is a sensible, well-behaved, moderate airplane that never goes out of style.”

    The airplane has a fuel capacity of 25 gallons per side for the Arrow and II and 38.5 gallons per side for late-model Arrow IIIs and up. Earlier models burn anywhere between 9.4-10.2 gallons per hour at 75 percent power to just shy of 13 gallons per hour for later models, giving a safe endurance of about six hours or 650-700 nautical miles. Useful load for the aircraft range between 1,120 to 1,151 pounds depending on the model; each of the Arrow’s have baggage capacity of 200 pounds. As far as costs, you can expect to budget about $0.69 to $0.82 per nautical mile depending on engine reserves and turbocharging.

    Now when it comes to selecting an Arrow, it’s important to pay special attention to the gross weights and useful loads of each version. Depending on your mission, not all Arrows will fit the bill. Additionally, each of the engine options have different TBOs. For example, the 200 horsepower Lycoming engine has a TBO of 1200 hours compared to the 180 horsepower version at 2000 hours. However, much of the 200 horsepower fleet has been upgraded to 2000 hour TBO thanks to exhaust valve replacement. Overhauls for the engine variants can range between $27,000 and $35,000.

    When compared to competitor airplanes, the Arrow is a bit slower than the Bonanzas and Mooneys. The Arrow also has a lower wing loading so it will not ride as well in turbulence. It’s also known to require a lot of back pressure for liftoff and settle quickly during landing if not on speed. Some owners also report the Arrow IV is a bit challenging to handle in slow flight with controls feeling unbalanced.

    What about maintenance? Well, the average Arrow is more than 30 years old. Moreover, many have been used by flight schools. While there is a large inventory of aircraft, good ones will undoubtedly sell quickly. Nevertheless, there are some maintenance issues to weary of including corrosion and cracking. In fact, there’s a recent AD out there that requires inspection of the right wing rib for cracks. There are also a number of Service Bulletins that when complied with, add value to the airplane. Also, Dean Showwalter of the Airplane Owner Maintenance Podcast put out a video that we’ve included in the show notes that describes an important area to inspect... The Piper Cherokee series of airplanes incorporate a stabilator system. Interestingly enough, the stabilitor is only held in place with two quarter-inch bolts on either side. Thus, it’s vitally important to check the condition of the attach points and these bolts. Watch Dean’s video to see more.

    Welcome to The Airplane Intel Podcast, the weekly General Aviation podcast for aircraft owners, operators, pilots and mechanics. We deliver practical advice, tips and strategies to make aircraft ownership simple, safe and cost effective.


    Special Edition: An Aeronautical Engineer's Perspective Sep 02, 2017
    Show notes

    Airplane Intel Podcast Special Edition. This week, Don interviews podcaster, aeronautical engineer, and future pilot Lucas Weekley of The Logbook Podcast. He shares an engineer's perspective on aircraft design & construction, building airplanes, and experimental - plus a lot more.

    Check Out The Logbook Podcast with our guest, Lucas Weakley

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    Welcome to The Airplane Intel Podcast, the weekly General Aviation podcast for aircraft owners, operators, pilots and mechanics. We deliver practical advice, tips and strategies to make aircraft ownership simple, safe and cost effective.


    027 - Hawker 800XP, Cessna Conquest Follow-Up, New AD, Meet Ups + More Aug 26, 2017
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    This week, we’re talking about the Hawker 800XP, an aircraft we’re currently doing a prebuy on. Then, another new AD issued by the FAA that affects some Piper airplanes; listener feedback about the Cessna Conquest, 2 meet ups, and new members to our Plane Partnership Program. Plus, aircraft ownership news, the tip of the week, and an after show!

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    Welcome to The Airplane Intel Podcast, the weekly General Aviation podcast for aircraft owners, operators, pilots and mechanics. We deliver practical advice, tips and strategies to make aircraft ownership simple, safe and cost effective.


    026 - The Cessna Conquest, New ADs + More! Aug 12, 2017
    Show notes

    Today, Don and I are talking turboprops with the Cessna Conquest I and Conquest II. Then we share some new meet up ideas and talk about some special plans we have for next week’s episode. Plus, two new ADs, the tip of the week, and new members to our Plane Partnership Program.

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    The Cessna Conquest: A Logical Step Up

    The Cessna Conquest is a cabin-class, twin engine turboprop first introduced in 1975 to compete with the already successful King Air lineup. The Conquest comes in two flavors: The 425 Conquest I and the 441 Conquest II. The Conquest II actually came before the Conquest I. Introduced in 1975 to compete with the King Air 200, the Conquest 441 took first delivery in 1978. The aircraft is essentially a modified Cessna 404 Titan with Garret TPE-331-8 engines with either a three or four-blade McCauley or Harztell propeller bolted to the front. While the 441 resembles the 404 on the surface, its structure and systems are more in-line with Cessna’s jet products.

    The 441 typically seats 9, but has enough room for 11. The stock -8 Garret engines put out about 636 shaft-horsepower each, and can cruise up to 35,000 feet at 260 knots for 2,000 nautical miles. With 475 gallons of useable fuel, the 441’s gross weight is 9,850 pounds. Upgrade to the Garret -10 engines and performance improves tremendously, giving you 310 knots at FL350 burning just 75 gallons per hour for a range of about 1,600 miles with reserves. It’s goes even faster in the mid 20’s, but bring the power back some and you can stretch the range to about 2,200 nautical miles.

    The Garret engines have a recommended TBO of 5,000 hours compared to Pratt-powered King Air’s and Cheyenne’s at 3,600 hours. Moreover, the 441 burns about 20 gallons per hour less fuel and flies about 20 knots faster. While these numbers are notably better than King Air 200’s, the 441 wasn’t always an operator’s first choice. In late 1977, a crash killed all seven aboard due to structural failure of the tail. This incident prompted the FAA to ground the entire fleet and required Cessna to seriously beef up the tail section of the existing fleet and all subsequent Conquests coming off the line.

    Today the 441 is a sought-after airplane – they hold their value well and are selling for “like-new” prices in the low-to-mid $1 million range. A total of 362 were built between 1978 and 1986 with some 320 still flying today. According to Business Jet Traveler, average airframe time is approximately 8,000 hours with operators flying about 250-280 hours per year.

    Stepping into a Conquest 441 isn’t too bad if you’re coming from a 414 or 421. However, if you’re like most aircraft owners, stepping into the Conquest 441 is a big jump, especially if you’re coming from a high-performance single or light twin, which leads me to a perfect segue into the Conquest 425.

    Born in 1978, and produced from 1980 thru 1986, the 425 was introduced to compete with the King Air 90 as an intermediate step between light to cabin-class twins and the larger, faster turboprops and jets. Like the 441, the 425 boasts faster cruise speeds, greater range, and more efficiency than its closest competitor, the King Air C90. Equipped with two 450 shaft-horsepower Pratt and Whitney engines, the 425 is a great airplane for personal and business use. Fly four-to-six passengers 250 knots for 800-1,000 miles on about 15% less fuel than the competition.

    As I alluded to earlier, the Conquest 441 came before the 425. The 441 was originally just known as the Conquest, and the 425 was first known as the Corsair. However, customer demands forced Cessna to make a few changes to the original turboprop version of the 421 including increased gross weight, more robust systems, and improved cabin. When these changes were made, the Corsair was renamed the Conquest I and the 441 the Conquest II. The most notable difference between the original Corsair and the Conquest I is an increase in gross weight to 8,600 pounds.

    Your passengers will appreciate the spacious cabin, comfortable seats, a powerful cabin pressurizations system, and many more amenities that makes sitting in the cabin almost as nice as sitting up front. The cockpit is wide and spacious and provides excellent visibility. You’ll find a familiar cockpit, making transitioning fairly straight forward. As with any high-performance airplane, training is a must. SIMCOM and other providers offer five-day initial and three-day recurrent training for both models. Owners appreciate the aircraft’s handling qualities and its reputation for being easy to fly. The systems are capable, yet easy to operate, and you’ll also notice predictable maintenance costs and good part support. There’s even a Conquest Owner’s Club with tons of resources.

    Peter Bedell of the Aircraft Owners and Pilots Association writes, “AOPA owned a Cessna Conquest for some 20 years starting in the early 1980s. It was the first turbine airplane I ever flew. Over the years, I was always amazed at how it soldiered on, day after day, mission after mission, with rarely a squawk or hiccup. Even today, I continue to be surprised at just how reliable turboprops can be. As with the Conquest, their systems are robust and reliable.” Enough said, right?

    Well not so fast... As you may already know, things like service bulletins aren’t usually mandatory for part 91 operators flying piston airplanes, but that’s not necessarily the case for turbine-powered airplanes. One example is a supplemental inspection document, or SID for short, which addresses Cessna’s aging fleet. In a nutshell, the SID limits the aircraft’s life to 22,500 hours and requires recurring inspections as part of Cessna’s phase inspection program, which under Part 91.409f, requires mandatory compliance.

    Despite recent additions to inspection requirements, the Conquest line is still a cost-effective airplane for many operators. With a nearly endless list of upgrades and modifications available today, Conquests continue to hold their value, making them a prime contender among even the newest twin-turboprops offered by Hawker-Beechcraft.

    To find out more, I encourage you to check out the show notes for episode 26 where we’ve posted a ton of great videos, articles, and links about the Cessna Conquest series.

    Welcome to The Airplane Intel Podcast, the weekly General Aviation podcast for aircraft owners, operators, pilots and mechanics. We deliver practical advice, tips and strategies to make aircraft ownership simple, safe and cost effective.


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