Circle to Land Approaches

When I was doing my instrument and multi-engine training, we did a lot of circle to land approaches.  As a student, I could never figure out why these types of approaches would ever be practical when you could an approach straight in to another runway.  But, as a good student, I never asked my instructors the purpose of them, I just did them to the best of my ability.

Now, having been flying in the IFR system for almost a decade, I’m finally beginning to fully understand the practical purpose of a circle to land approach.  I have actually elected to do an approach where I had to circle to land on several occasions in actual IMC conditions.

One important note to remember on circle to land approaches is that the minimum descent altitude (MDA) is always higher than on a straight in approach.  The reason for this is that you are basically joining the pattern for a different runway and you have to be able to visually keep yourself clear of towers and other obstacles.  So, you need a higher visibility and a higher ceiling than if you were just lining up to come straight in.

Here are a couple of practical circumstances where it would make sense to do a circle to land approach.

Airports with only 1 straight in approach

This one is easy.  There are a number of airports scattered around the US that have only 1 straight in instrument approach published for it.  Around my part of Texas, the first one that pops into my mind is the RNAV 31 at T85 in Yoakum, TX.  Most of the year, the prevailing wind is out of the south, so 13 is the favored runway at T85.  During the winter is when most of the IMC weather happens in South Texas, so that is why the approach is for 31.

Of course, especially this year during the summer, there are some IMC days where an approach to T85 would be necessary.  When there is a strong wind out of the south, landing on 31 is impractical, so a pilot would fly the approach to 31, then circle to land on 13.

Approaching from the opposite direction

Take a look at the RNAV 19 at KBMQ, Burnet, TX.  The two initial approach fixes (IAF) are IXANY and JIBAJ.  If a flight is approaching BMQ from the west or north, this is an easy approach to join.  If a flight is coming from Austin (directly the the east and a little south) or San Antonio (almost directly south), it would be a bit of extra flying to get configured properly for the approach.  Especially coming from Austin, because the degree of turn to join at JIBAJ wouldn’t make the approach practical.

Well, how about vectors?  Unfortunately, Houston Center doesn’t have this approach depicted so vectors aren’t a possibility.  Center can give you vectors north to make the angle a little easier to join at JIBAJ, but they can’t vector you onto the approach.

Direct DLORA to join is another option, but again, if you are approaching from the southeast, the angle is wrong.

Insert the RNAV 01 approach with a circle to land.  AMUSE is right on V163, so it’s really easy to join the approach there coming from the south.  Coming from Austin, joining the approach at SUBIE works out great. Fly down to the MDA, join the left downwind for 19, and everyone is happy.

VOR Circle to Land Approaches

Every instrument pilot has had an instructor “force” them to do a VOR A or VOR B approach and no one enjoys them.  I personally think they are good practice.  With the number of RNAV systems and RNAV approaches out there, though, VOR approaches are becoming a bit archaic.

They do have a place in this discussion, though.  A VOR approach is given an A or B designation when the angle of the final approach course is greater than 30 degrees to the runway (VOR A KLZZ), or the final approach course is lined up with the runway, but the MDA is too high to practically descend and land (VOR A KGRK or the VOR/DME C KASE).

So, there are practical uses for a Circle to Land approach.  The next time you do some IMC work with an instructor, ask him/her if you can include one.

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  • I Learn To Speak Seaplane

    From the time I started flying, I have always had the dream to learn how to fly a seaplane.  As I learned in November, it’s actually learning to land a seaplane, and the veterans call them floatplanes.

    ProMark Aviation at the Burnet Airport (KBMQ) offers a weekend float plane course that is high on fun and low on stress.  The school has a Piper PA12 Super Cruiser on amphibious floats (amphibs as I was corrected at one point.  I mean, if you’re going to fly a seaplane, er, floatplane, you have to know the lingo) that will land and takeoff on water, but does little else with ease and grace.  At 150 HP with those big floats and all the associated rigging hanging underneath the airplane, you are lucky to get to 500 feet before you get to your destination.

    We weren’t working on setting any speed records.  I was learning the lay of the water.  I learned about the step, the keel, pumping the floats, how to read the water, currents, ducks (yes, ducks and birds are important to know about when you are flying low on the water), buoys, docking, and ditching.  Step taxiing was fun as you are basically at 3/4 throttle screaming across the top of the water just below flying speed.  It’s the best way to taxi a seaplane (truly, it is.  You get more air in your engine, you can see better, and you are moving.  Just don’t try and turn sharp).

    Floatplanes also don’t have any shock absorbers, so the higher the wave, the more you get knocked around, so wind velocity and, in turn, wave height is very important.

    A very important nuance of an amphibious floatplane compared to a straight floatplane (one that doesn’t have wheels that come out of the floats), is at one point, you want to make sure your gear is down for landing (runway landing) and at another, you want to make absolutely sure your gear is up for landing (water landing).  If you land wheels down in the water, you will capsize, 100% of the time.  Thankfully from my good instruction, I did not capsize.

    Ken Wittekiend, my instructor, and I spent the majority of the weekend landing and taking off on Lake Buchanan (I was informed by locals it is pronounced “Buk-cannon”, not “Bue-cannon”), which is more open and therefore has more waves.  We did one landing on Inks Lake so my kids could see me land, which they thought was the best thing since cheese sticks.

    There is a check ride at the end of the training, but, as Ken reassured me, it’s the most fun check ride you’ll ever have.  I still hate check rides, but that one I think I hated least of all.

    I hope someday I can put my floatplane skills to practice, but for now, I can vouch that I now speak seaplane!

    From the time I started flying, I have always had the dream to learn how to fly a seaplane.  As I learned in November, it’s actually learning to land a seaplane, and the veterans call them floatplanes. ProMark Aviation at the Burnet Airport (KBMQ) offers a weekend float plane course that is high on fun…

  • An Educational Runup

    When a pilot thinks of an engine runup in a single engine piston airplane, typically it is let’s find out if the engine is running rough or not, meaning a spark plug is fouled.  Believe it or not, there is a little more to learn from a runup than just checking the spark plugs.

    A distinct advantage to having an engine monitor that monitors all EGTs and CHTs is you get a better idea of engine health.  When switching to one magneto or the other during the runup, all the EGTs should rise, showing that the temperature of the exhaust gas is going up from each cylinder.  This occurs because when running on only one magneto and one set of spark plugs in each cylinder, the mixture takes longer to burn, so, when the exhaust valve in the cylinder opens, the burn is still on going and this hits the EGT probe, causing a temperature rise.  An indication of a magneto failure in flight would be a rise in all the cylinders EGT without a change in mixture setting.

    Now that we know what to look for when checking each magneto, what would one look for to show that there is a problem?  The basic that each student pilot is taught still applies.  The engine manufacturer puts a limit on RPM drop during the runup.  When checking one magneto or the other, watch for an excessive RPM drop.  If the RPM drops past the limit, this usually will be accompanied by engine roughness.

    Why is that?  Let’s look at the cause for the excessive RPM drop.  For this, we need to go back to our EGT indicators.  Let’s say we have a 6 cylinder engine.  When the key is turned to the right magneto, the RPM drops 250 RPM and the engine gets very rough.  Look at the EGT gauge.  The cylinders where the spark plugs are firing normally will all show a temperature.  The cylinder (or cylinders) where there is no combustion, meaning a bad plug, will show no temperature.  This is because the mixture is just sitting in the cylinder and not igniting, therefore, no exhaust gases will be pushed out so there will be no EGT indication for that cylinder.  This is also how you tell a mechanic which cylinder to check for the bad plug.

    It could also be a bad magneto.  If multiple cylinders EGT all drop, or the engine wants to quit entirely, you have a bad magneto or bad ignition harness.

    What else can you learn during the runup?  Electrical system health is key, especially in all electric airplanes (meaning no vacuum system).  It’s a very good idea to turn on all the lights and pitot heat to ensure that a rise is indicated on the ammeter.  This means the alternator is carrying the load and working properly.

    The next time you do your runup, keep an eye on your EGT to see the rise during a magneto check.

    When a pilot thinks of an engine runup in a single engine piston airplane, typically it is let’s find out if the engine is running rough or not, meaning a spark plug is fouled.  Believe it or not, there is a little more to learn from a runup than just checking the spark plugs. A…

  • The Importance of Transition Training

    In September, the FAASTeam at the San Antonio FSDO put a special emphasis on transition training (AOPA put out a free course last year covering general transition training topics).  A lot of pilots don’t understand the need for transition training or what it even entails.

    Transition training deals mainly with piston engine aircraft, regardless of whether the airplane is a single or twin.  The FAA doesn’t have any special requirements for changing from one piston engine airplane to another, as long as the pilot has the appropriate endorsements (high performance, complex, high altitude, etc.) and is rated in that category and class.

    Transition training is promoted mostly by insurance companies. An insurance company looks at a pilots experience when deciding to insure him or her in a new airplane.  If the pilot has only flown Cherokees and Comanches and is now upgrading to a Malibu, then the insurance company is going to require some transition training with a knowledgable instructor.

    What is transition training?  It is when an appropriate rated pilot needs to learn how to fly a different airplane.  These are referred to commonly as checkouts, but with more complicated airplanes, the training is actually very in depth.

    Using the example above, Pilot A just sold his Comanche 260 and bought a 1987 Malibu.  Pilot A says, “A Malibu is a complex, high performance, single engine piston, which is what I had in my Comanche.  I can fly that, no problem.”  In reality, a Malibu has a lot of differences.

    pa46-transition-training

    First, there are more systems in a Malibu.  You have pressurization, air conditioning, emergency oxygen, turbo charging, and possibly radar.  Not to mention you are dealing with a Continental engine instead of a Lycoming.  And, is it a factory TSIO 520 or a converted 550?  2, 3, or 4 blade prop?  Glass panel or steam gauges?  What kind of autopilot?  Plus, it’s a much heavier airplane so it’s going to fly different, have different rotation and landing speeds and handle differently in stalls.  What’s the sight picture supposed to be on final approach?  What are the emergency procedures?

    Overwhelmed yet?

    An experienced, insurance approved instructor and training program is a necessity when getting into new airplanes.  It makes for safe pilots and safer skies.

    Texas Top Aviation offers Cirrus Transition Training as well as Bonanza Transition Training and Columbia/Corvalis Transition Training.  We are working on an insurance approved Piper PA 46 piston transition course as well (Malibu and Mirage) and will have the course approved by the end of 2016.  Contact us today to schedule your transition training.

    In September, the FAASTeam at the San Antonio FSDO put a special emphasis on transition training (AOPA put out a free course last year covering general transition training topics).  A lot of pilots don’t understand the need for transition training or what it even entails. Transition training deals mainly with piston engine aircraft, regardless of whether…

  • Shock Cooling in a PA46

    We’ve all heard it said…”reduce the throttle by no more than 1-inch every minutes to ensure you don’t shock-cool your engine”. Does this advice apply to a PA46 engine? Can a PA46 engine (Lycoming 540 or Continental 520/550) really be shock-cooled? How should the engine temperature be managed?

    Metals expand and contract with temperature, and the various metals in an air-cooled aviation engine expand and contract at a different rates. Shock-cooling supposedly occurs when the engine changes temperature quickly and the different metals in the engine cool (and therefore change shape) at different rates. When the change occurs dramatically supposed scoring, rubbing, and marking of the metal can occur, which can cause catastrophic results.

    So, let’s back to the original question…can a PA46 engine suffer shock-cooling and should a pilot operate the engine so as to avoid shock cooling? Simply put, I’ve never seen nor heard of any piston PA46 engine suffer shock-cooling. In 5000+ hours flying the piston PA46 and 16 years of flying/managing/training in the Malibu/Mirage/Matrix, it simply has not happened to me nor anyone I know. Does it mean that it cannot happen or has never happened? No. But, it is certainly not a prolific threat to our fleet.

    Should the owner/pilot operate the engine with a cautious eye cast toward the potential of shock cooling? Well, sort of…but, let’s flesh this out. My suggestion is that a pilot should operate the engine with conservatism in movement of temperature, but only because this is a good operating practice with any machine, and any flying machine is (by definition) not “overbuilt”. And, there are many ways to change the temperature of the engine…not just by reducing power. Here’s a partial list of ways to cool your PA46 engine:

    • Reduce power: Obvious…yes. When the engine produces less power, less heat is generated. Reducing power in a piston engine will almost always result in less temperature.
    • Lower the nose: By descending (and leaving power in a cruise setting) the airspeed will increase and cool the engine.
    • Enrichen the mixture: Fuel has a cooling effect on the engine, so the richer the mixture the cooler the engine.
    • Lower the landing gear: Yes…you read that right…engine cooling will occur when you lower the landing gear because more air will flow over the cylinders. Notice the landing gear doors on the PA46 have air louvers. Air flows into the engine nacelle on the front, passes down through the cylinders (along with the oil cooler, intercoolers, and other components) and then out the louvers of the closed gear doors. When the landing gear is lowered the “back door is opened” and a LOT more airflows over the cylinders.

    My suggestion is that a pilot only perform ONE of these actions at a time when beginning a descent. This suggestion was presented to me by Chad Menne (Owner, Malibu Aerospace) some time ago and I’ve operated engines this way ever since. If you are at a higher altitude and simultaneously reduced the power, lowered the landing gear, started a big descent, and enrichened the mixture in one flail swoop, I think there’s a chance that your engine would suffer some negative effects that could be called “shock cooling”. So, when you do start a descent, pick one “cooling action” to accomplish at a time. I’m sure you’ll not hurt your engine.

    Simply put, shock cooling is not a huge factor in the PA46 community, and a PA46 pilot does not need to be overly cautious. The “one inch per minute” rule may apply in some other airframes, but in the PA46 world it is not applicable.

    Joe Casey’s aviation story began in 1990 with his first flight near Nacogdoches, TX in a Cessna 172. From lift-off, Joe knew he would have a lifetime passion flying just about anything that will leave the ground…He was completely hooked.

    Along with being an FAA Designated Pilot Examiner (DPE), Joe is an ATP/CFI-AHMG and Commercial Rotorcraft/Glider Pilot in the civilian world and also a UH-60/AH-64 Pilot-in-Command/Instructor/Examiner Pilot in the US Army Reserves.  His passion for the last 19 years, however, has been the PA-46 Malibu/Mirage/Matrix/Jetprop/Meridian. Has has amassed over 6,500 hours in various PA-46 airframes and believe it to be one of the finest flying machines available for the serious cross-country pilot with an eye for efficiency.

    Now, Joe has flown more than 12,200 hours in just about every imaginable environment. Whether providing initial/recurrent training in the PA-46’s, TBM’s, instructing in NVG’s in a UH-60 Blackhawk, flying the King Air series of airplanes, giving tailwheel endorsements, or taking kids flying for the first time, he simply loves flying machines and the people who fly them.

    We’ve all heard it said…”reduce the throttle by no more than 1-inch every minutes to ensure you don’t shock-cool your engine”. Does this advice apply to a PA46 engine? Can a PA46 engine (Lycoming 540 or Continental 520/550) really be shock-cooled? How should the engine temperature be managed? Metals expand and contract with temperature, and…

  • Cirrus G2 Vision Jet

    Well, that was fast.

    In January, Cirrus announced the Generation 2 SF50 Vision Jet.  After getting the Generation 1 Vision Jet certified in late 2016, Cirrus didn’t waste any time in starting in on improvements.

    The improvements are pretty sweet, making the G2 Vision Jet even easier to fly and step into for Cirrus’ target market, SR22 owners.

    Here are the improvements on the G2 Vision Jet.

    RVSM Approval

    The G2 Vision Jet has received RVSM approval, allowing the airplane to fly at 31,000 feet.  RVSM stands for Reduced Vertical Separation Minimums (read more about RVSM here).  RVSM airspace starts at 28,000 feet, the G1 Vision Jet’s ceiling.  Now that the G2 Vision Jet is RVSM certified, it can fly at 31,000 feet.

    For piston pilots, you are left scratching your head as to the advantage of this.  In a jet, the higher you go, the thinner the air, so the faster you go, and the less fuel you burn since the thin air needs less fuel to mix with.  This caps out at a certain altitude and the speed begins dropping and you start losing efficiency (even though the fuel burn is quite low).

    According to Cirrus, at 31,000 feet, the G2 Vision Jet cruises over 300 KTAS and gets a range boost to almost 1,200 nm.

    Garmin Perspective Touch+

    Cirrus & Garmin have taken the new NXi interface and paired it with the Garmin Perspective Touch to create the Touch+.  You can read about the improvements on the NXi here, all of which are included in the Touch+ in the G2 Vision Jet.

    The big improvement that is included in the Touch+ is Autothrottle capability.  An Autothrottle is integrated with the autopilot.  It automatically adjusts power settings and speeds based on the phase of flight without the pilot having to touch the throttle.  Pretty cool.

    New Cabin

    The G2 Vision Jet has a redesigned cabin as well, making it an extremely passenger friendly airplane.  The second row has been redesigned and equipped with a center console.  There is also a drop down TV screen that allows passengers to connect their mobile devices to it to watch movies or videos while traveling (no internet on board, yet.  That’ll probably be the G3 Vision Jet!).

    Cirrus also put in more noise reduction in the cabin, creating a quieter ride for passengers.  Cirrus also allows for multiple different seating configurations, depending on the needs of the owner.

    As always, Cirrus is on the leading edge of airplane technology, creating airplanes that are easy as well as fun to fly.  I’m excited to see how they continue to improve the design to both the SR22 and the Vision Jet.

    Well, that was fast. In January, Cirrus announced the Generation 2 SF50 Vision Jet.  After getting the Generation 1 Vision Jet certified in late 2016, Cirrus didn’t waste any time in starting in on improvements. The improvements are pretty sweet, making the G2 Vision Jet even easier to fly and step into for Cirrus’ target…

  • The Avidyne Equipped Cirrus Upgrade

    A History Lesson

    11 years ago, in April of 2009, the Avidyne Corporation unveiled the much bally-hooed Release 9, or R9 as it is commonly known, as a hardware replacement for the Avidyne EX5000 Entegra system in Cirrus Aircraft. The Entegra system was way outdated by that point. Even though Avidyne was the first company to put together a glass PFD in a single engine piston airplane, the company had quickly fallen behind Garmin in keeping up with the ever changing technology landscape.

    Rewind to 2008. Cirrus had been going strong with the Avidyne Entegra since the SR20 and SR22 went to full glass in 2003 (a PFD and an MFD; prior to that, Cirrus aircraft only had an MFD with steam gauges and a Sandel Electronic HSI). Cessna, on the other hand, vaulted past the Avidyne Entegra and went straight to the Garmin G1000 in it’s aircraft, starting in 2004 with the 182 G1000 and 2005 with the 172 G1000. Beechcraft and Columbia went to the G1000 (Columbia started with the Avidyne as well) in 2005.

    Garmin’s technology in 2007 was so much better than Avidyne’s technology that Cirrus decided to switch. I’m sure there were many promises made by Avidyne to Cirrus about what Avidyne was working on (the R9), but the G1000 was out there, available, and being used in a lot of different airplanes with very good results.

    So, in 2008, Cirrus made the switch from the Avidyne Entegra to the Garmin G1000, dubbing it the Cirrus Perspective by Garmin avionics package. Avidyne finally got the R9 to market in 2009, but by that time, Piper was the only airplane manufacturer left putting factory Avidyne panels in their airplanes, and they switched to G1000 later that year.

    The R9 is a fabulous product. It’s fully integrated, has great graphics, has fully redundant displays, a QWERTY keypad (which, by the way, Garmin didn’t do for another 8 years), and a lot of other neat features. There’s a bit of a learning curve, but it’s a really good product for what it is.

    Avidyne, though, was late to the game with their technology. By the time it debuted in 2009, all the GA aircraft manufacturers had long since switched to the Garmin G1000 and weren’t looking back. That left Avidyne with the retrofit market for the many different Avidyne Entegra Cirrus aircraft out there. The only problem was, the retrofit was $80,000 ($95,000 if you wanted to throw in the DFC 100 Autopilot, which is a must have) and not many owners were up for paying that much money, then or now.

    To sum up our brief history lesson, Avidyne knew the Entegra needed to go, but couldn’t get the R9 out quickly enough to convince anyone to stick with Avidyne products. The retrofit market didn’t amount to many sales, so Avidyne doesn’t even make the R9 anymore.

    As a side note, I really, really like the Avidyne R9 and am sad that it didn’t make it into more airplanes.

    So, when the Avidyne Entegra starts to have issues, what’s an owner to do? Keep reading!

    There is Hope

    There are thousands of Cirrus aircraft out there flying with the Avidyne Entegra instrumentation, which is basically 20 year old technology (I’ve had a computer engineer tell me the programming in an Entegra is Windows 98 tech). These things are going to start having problems at some point (many already have), but what solution do owners have that is cost effective and get’s them new technology?

    Remember that little company named Garmin? Well, they have come through again. Announced this summer, the Garmin G500 TXi is now certified as a replacement in the Cirrus Avidyne Entegra equipped aircraft. This means pulling out both the PFD and MFD and replacing them with the G500 TXi on both sides. Engine data is also displayed on the G500TXi MFD, including the percent power and TIT indications, if equipped.

    Cirrus SR22 Equipped with Dual G500 TXi Screens and Dual Garmin GTN 650Xi GPS Units

    The cost for the panel? Two 10.6″ G500 TXi’s run about $16,000 apiece for the units, not including labor. $32,000 for a brand new panel isn’t terrible. Plus, the G500 TXi’s work with the DFC90 autopilot if the Cirrus is already equipped with it. If not, the Garmin GFC 500 autopilot is now approved for the Cirrus at a relatively low price of $7,000, including the servos.

    Still have the original Garmin 430s in your Cirrus? Upgraded to the Avidyne IFD 540/440 stack? Put in dual GTN 650Xi’s? Put in a GTN 750Xi? All are compatible with the G500 TXi panel.

    Want to upgrade everything? It does get kind of pricey at that point, but for just equipment, the cost for a complete panel conversion is somewhere in the area of $65,000 plus labor, still below what the R9 cost, but not cheap either. That would include 2 G500 TXi’s, 2 GTN 650Xi’s, a GFC 500 Autopilot, and all the engine monitoring equipment that the G500 TXi would need.

    Cirrus SR22 Equipped with Dual G500 TXi Screens, a GTN 750Xi, and a GTN 650Xi

    Thankfully, some new technology has finally come to the Generation 1-3 Cirrus. Oh, and by the way, your steam gauge Cirrus is fully upgradable as well.

    Want to read more? Check out Garmin’s website.

    A History Lesson 11 years ago, in April of 2009, the Avidyne Corporation unveiled the much bally-hooed Release 9, or R9 as it is commonly known, as a hardware replacement for the Avidyne EX5000 Entegra system in Cirrus Aircraft. The Entegra system was way outdated by that point. Even though Avidyne was the first company…

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