Archive for the ‘Mike Busch’ Category

Misfueled!

Monday, January 11th, 2016
Decals

Jet fuel contamination of avgas remains a killer.

On March 2, 2008, a turbonormalized Cirrus SR22 was destroyed when it crashed shortly after takeoff in Rio de Janiero, Brazil, killing all four people aboard. Shortly after the aircraft departed from runway 20, the airplane’s engine lost power, and the aircraft hit a building and exploded. Further investigation revealed that the aircraft had been refueled with Jet A instead of 100LL.

This report reminded me of an incident 16 years earlier during which my own 1979 Cessna T310R was misfueled with Jet A at San Carlos (Calif.) Airport, a busy GA airport just south of SFO. Fortunately, I caught the (mis)fueler in the act, red handed. Had I not been lucky enough to do that, I probably wouldn’t be writing this column.

Normally, I either fuel my aircraft myself (at a self-serve pump) or watch it being fueled (when avgas is supplied by truck). On this occasion, I’d radioed for the fuel truck and waited patiently for it to arrive. After 10 minutes of waiting, Mother Nature intervened and compelled me to walk into the terminal building in rather urgent search of a loo. By the time I took care of my pressing business and returned to the ramp, there was a fuel truck parked by my airplane and a lineperson pumping fuel into my right main tank.  As I approached the aircraft, I observed to my horror that the truck was labeled “JET A.”

Theoretically impossible

At first, I was not too worried, because I believed that misfueling my airplane with Jet A was physically impossible. That’s because in 1987 (the year I purchased by T310R), all turbocharged twin Cessnas became subject to Airworthiness Directive AD 87-21-02 which mandated installation of restrictor ports on all fuel filler openings. The restrictor ports were designed to make it impossible to insert an industry standard Jet A nozzle, while accommodating the smaller diameter avgas nozzle.

The AD was issued because the FAA became aware that a large number of misfueling indicents and accidents were occuring in turbocharged aircraft. These aircraft typically were prominentaly decorated by the factory with the word “Turbo” and apparently linepeople were confusing it with “Turbine” and pumping Jet A into the tanks.

So the FAA mandated that jet fuel trucks install a wide spade-shaped fuel nozzle, and that vulnerable airplanes (like turbocharged twin Cessna) have restrictor ports installed into which the wide jet fuel nozzle would not fit. This made misfueling of piston aircraft with jet fuel theoretically impossible. (They also said that it’s theoretically impossible for bumblebees to fly.)

But as I arrived at my airplane, I discovered that indeed my left main tank had been topped with Jet A. How was this possible? A subsequent investigation by the local FSDO revealed that the Jet A fuel truck at San Carlos Airport had not been fitted with the correct spade-type nozzle. (I suspect they got in trouble for that.)

Jet-A nozzle vs. avgas nozzle

Jet fuel nozzles have a wide spade top that is theoretically incapable of being inserted in an avgas fuel filler equipped with a restrictor ring—but don’t count on it!

Undoing the damage

I spent literally hours trying to find an A&P on the field that would assist me in purging the fuel system of its witches’ brew of 100LL and Jet A. That turned out to be surprisingly difficult. The fueling company was falling all overitself to be helpful (because I’m sure they feared a big lawsuit) but they had no mechanics or maintenance capabilities. There were several maintenance shops on the field, but none wanted to go near my contaminated airplane, clearly afraid of the potential liability exposure. Finally, I persuaded one maintenance manger to help me out after writing and signing an omnibus waiver absolving the shop and its mechanics of any liability in connection with their work on my aircraft.

The purging process itself was quite an eye opener. We drained the tanks as completely as possible, putting the noxious effluent into a 55-gallon drum provided by the fueling company (who had agreed to deal with the costly disposal of the nasty stuff). We disconnected the fuel line going to the engine-driven fuel pump and drained all the fuel from that as well.

Next, 5 gallons of 100LL (donated gratis by the fueling company) was poured into the main tank, and then pumped through the system using the electric boost pump and drained from the disconnected fuel line into a 5-gallon bucket.  The fuel in the bucket was tested for Jet A contamination using the paper-towel test: A few drops are placed on a paper towel and allowed to evaporate completely. Pure 100LL will not leave an oily ring on the towel, but even small amounts of Jet A contamination will leave an obvious ring. The stuff in the bucket flunked the test.

Another 5 gallons of 100LL were poured into the tank, and the process repeated. Once again, it flunked the paper-towel test. We had to repeat the procedure three more times before we were satisfied that the system was essentially kerosine-free. We reconnected the fuel line, cowled up the engine, the fueling company then topped off the airplane (again gratis), and I was finally good to go…fully six hours after the misfueling incident.

Restrictor filler & GATS jar

Be sure all your fuel filler ports have restrictor rings. The big GATS jar (available at Sportys, Aircraft Spruce, and elsewhere) does a far better job than the slim screwdriver-type testers.

Lessons learned

I learned some important lessons that day. Perhaps the most important is that it’s impossible to distinguish pure avgas and a mixture of avgas and Jet A by color alone. My main tanks had been about half-full of avgas, so after the misfueling they contained roughly a 50-50 mix. If you take a jar full of pure 100LL and another jar full of a 50-50 mix of 100LL and avgas, I guarantee you will not be able to see any difference in color or clarity between the two.

I hadn’t realized that before. I has always been taught that you sump the tanks and observe the color—100LL is blue and Jet A is straw color. What I was not taught is that a mixture of 100LL and Jet A is also blue and that you simply can’t tell the difference visually. In retrospect, I shudder to think what would have happened had I not caught that Jet A truck in front of my airplane.

I was also taught that since Jet A is significantly heavier than avgas (6.7 lbs/gal versus 5.85 lbs/gal), the Jet A and 100LL will separate just like oil and water, with the Jet A at the bottom (where the sump drain is) and the 100LL at the top. That’s true, but only if the contaminated fuel is allowed to sit for hours and hours. It turns out that 100LL and Jet A mix quite well, and the mixture takes a surprisingly long time to separate.

There are at least two good ways to distinguish pure 100LL from kerosine-contaminated 100LL. One is by odor: Jet A has a very distinctive odor that is detectable even in small concentrations. The other (and probably best) is by using the paper-towel test: Pour a sample on a paper towel (or even a sheet of white copy paper), let it evaporate, and see if it leaves an oily ring.

Nasty stuff

What effect does Jet A contamination have on a piston engine? Enough to ruin your day.

You can think of Jet A as being fuel with a zero octane rating. Any piston engine that tries to run on pure Jet A will go into instant destructive detonation. However, in real life, we almost never encounter that situation because the tanks (at least the main tank used for takeoff) is almost never completely dry when the aircraft is misfueled.

Therefore, the real-world problem is not running on pure Jet A, but on running on a mixture of 100LL and Jet A.  Depending on the mixture ratio of the two fuels, the effective octane rating can be anything between 0 and 100. A mixture with a lot of Jet A and just a little 100LL might be detectable during runup.  A 50-50 mix might not start to detonate until full power is applied, and the engine might fail 30 seconds or 3 minutes after takeoff. Just a little Jet A contamination might produce only moderate detonation that might not be noticed for hours or even weeks. Like so many other things in aviation, “it all depends.”

The Cirrus SR22 accident in Rio reminds us that the problem of misfueling is still with us, despite all the efforts of the FAA to eradicate it. We need to be vigilant. Always watch your airplane being fueled if you possibly can. Make sure its fuel filler ports are equipped with restrictor rings. Don’t just look at the fuel you drain from your sumps—sniff it, and when in doubt, pour it on a paper towel.

Buying the right plane

Thursday, December 17th, 2015

TAP CoverFinding the right airplane to buy is hard work. Who among us hasn’t spent hours looking through Controller or Aircraft Shopper Online or Trade-A-Plane or Barnstormers looking for that perfect candidate—one with low time, a fresh overhaul, new paint and interior, great avionics, and a bargain price?

Dream on!

Common sense says you’re unlikely to find an airplane like that—and if you do, there’s probably a good reason that it’s underpriced … like maybe lost logbooks, major damage history, wing spar corrosion, an expensive AD that hasn’t been complied with, or some other big-time skeleton in the closet.

Nothing’s perfect

Many of the aircraft you see advertised are in reasonable shape, decently maintained, and worthy of consideration. But if you expect them to be in pristine condition—or even in as good condition as represented in the ads—you’ll probably be disappointed. If you have your heart set on buying a perfect airplane, you’d better buy a new one and be prepared for sticker shock. A well-equipped new Cessna 182T costs about $500,000 these days, and a Cirrus SR22 or Cessna T206H goes for about $750,000, and a Beechcraft Baron G58 now sells for $1.35 million.

If these prices are beyond your pay grade (and they sure as heck are beyond mine), you need to accept the fact that any “pre-owned” airplane you buy will be somewhat less than perfect and will require some fixing up after the purchase.

There’s absolutely nothing wrong with buying a “fixer-upper” so long as you go into the deal with your eyes open, have a good understanding of what it will cost to correct the airplane’s deficiencies, and are confident that this cost is adequately reflected in the negotiated purchase price.

High-time engine

Lycoming EngineOf course, some kinds of deficiencies are easier to deal with in this fashion than others. The easiest of all is an airplane with a high-time engine that’s close to (or beyond) TBO.

I say it’s easiest because engine time is almost always fully reflected in the selling price. In other words, an aircraft with a run-out engine is almost always priced sufficiently below the price of a similar aircraft with a zero-time engine to account for the cost of a major engine overhaul or factory-rebuilt exchange engine. I bought my own airplane with nearly run-out engines, and I’m convinced that buying an airplane with run-out engines has a lot of advantages.

One advantage is that the new owner gets to choose whether to overhaul or exchange for a factory rebuilt. If he opts to overhaul, he gets to choose the overhaul shop, the kind of cylinders he wants on his new engine, and any special items that may be desired when reinstalling the new engine (such as Teflon hoses, new Lord mounts, exhaust system repair, etc.) And that’s as it should be, since it’s the new owner who will have to live with the consequences of these decisions for years to come.

A second advantage of buying an airplane with a run-out engine (or engines) is that the seller is probably motivated to sell (rather than shell out big bucks for a major overhaul or factory rebuilt), and so may be a bit more flexible during price negotiations. In fact, I’m always a bit suspicious when I see an aircraft listed for sale with a “fresh overhaul” or unusually low engine time. I can’t help but think that the seller most likely knew he was about to get rid of the airplane when he had the engine overhauled, and it seems to me it would be mighty tempting to cut corners and minimize cost in that situation. Maybe I’m just cynical.

A third advantage of buying an airplane with an engine at or near TBO is that you might just wind up getting a pleasant surprise. After buying my T310R with engines just 100 hours shy of published TBO, I wound up flying the airplane for 600 more hours of trouble-free operation before deciding to overhaul the engines at TBO+500. With reserve for overhaul of $30/hour/engine, that wound up being a $36,000 windfall for me.

Most aircraft listed for sale have engines somewhere in between “fresh overhaul” and “run-out.” The problem here is that it’s often impossible for the buyer to know how much time he can expect to get out of the engine before overhaul. A good friend of mine—let’s call him “Frank”—bought a gorgeous 1978 Cessna T310R some years ago with mid-time RAM engines. Now RAM is arguably the country’s premier overhaul shop for TSIO-520 engines, and the engines got a clean bill of health during the pre-purchase inspection, so Frank fully expected it to be years before he’d have to think about major overhaul. At the first oil change after Frank bought the airplane, however, some ferrous metal showed up in one of the oil filters. Frank sent the filter contents to RAM, and they determined that one or more cam lobes were coming apart. Frank wound up having RAM tear down and overhaul the engine. Ouch!

Bottom line is that I think the best way to buy a used aircraft—all other things being equal—is to buy one with a high-time engine, plan to overhaul it or swap it for a factory engine shortly after the purchase, and make sure the cost of doing so is priced into the selling price.

High-time airframe

Jacked AirframeIn contrast, an airframe with beaucoup hours is much more difficult to analyze. Unlike engine time, airframe time cannot be “rolled back” by doing an overhaul. It is what it is.

High time on an airframe isn’t necessarily a bad thing. An airframe with high time has probably been flown regularly and often throughout its life. That’s good. Also, a high-time airframe usually belongs to a “working airplane” (flight school, charter, cargo, etc.), and such aircraft tend to receive better and more regular maintenance than owner-flown “hangar queens.”

In contrast, an airframe with unusually low hours is often one that has experienced lengthy periods of disuse, and unless the aircraft was based in a dry climate or stored in a heated hangar, it’s a likely candidate for having hidden corrosion damage.

Low-time airframes tend to command premium prices. Some years ago, a study of light twins listed for sale indicated nearly a linear inverse correlation between selling price and airframe hours (after adjustment for engine time and equipment), with depreciation of almost exactly $10 per airframe hour. (In other words, all other things being equal, a 6,000-hour twin sold for $30,000 less than a 3,000-hour twin.)

I’m not sure that’s rational—but market forces are often not rational. Personally, I’d be more comfortable buying a 25-year-old airplane with 4,000 hours on the airframe (average 160 hours/year) than a 25-year-old airplane with 1,000 hours on the airframe (average 40 hours/year). Of course, I’d really want more information about how those hours were distributed over the aircraft’s life, whether there were extended periods of disuse, whether the aircraft was hangared or tied down outdoors, where it was based (Tucson or Tampa), and so forth.

Very high-time airframes are another matter, however. We used to think that airframes would pretty much last forever if adequately protected from corrosion. That may still turn out to be true for some airframes (like strut-braced high-wing singles), but in recent years there has been increasing concern over the useful fatigue life of cantilever-wing airframes, particularly single- and twin-Cessnas and Beechcraft Bonanzas and Barons. There’s already a very costly spar-strap AD for high-time Cessna 400-series twins, and a good possibility of more such ADs in the future that could have a big impact on owners of high-time airframes.

As a general rule, you probably shouldn’t pay a big premium for an ultra-low-time airframe, and might even do well to be a bit suspicious of one. A mid-time airframe—with hours commensurate to its chronological age, indicating that it has been flown regularly and often—may be a more worthy candidate, not to mention a better bargain.

I warned you it wasn’t easy.

Older aircraft

1960 Cessna 210AFiguring out what model year to buy is another toughie. Market valuation of airplanes tends to drop precipitously with calendar age, and you occasionally see older aircraft for sale that have been well maintained, are corrosion-free, and are offered at what seem to be screaming bargain prices.

My advice to all but the most experienced aircraft buyers is to be wary of older airplanes, particularly older complex airplanes. There’s a good reason for their enticingly low asking prices: An older airplane can easily turn into a money pit. In fact, that may be precisely why it’s for sale.

You may figure that if the selling price is cheap enough, you can afford to spend the money to refurbish that older airplane into something really nice. Take an old, clapped-out 1960-model Cessna 210, for example, that you see in Trade-A-Plane for only $30,000. Add $30,000 for a zero-time engine, $20,000 for new paint and interior, and maybe another $15,000 to replace those old tube radios with a modern comm and GPS. So for $95,000 you’ll wind up with a first-class speed merchant, right?

Unfortunately, your “better than new” refurbished airplane won’t be worth anything close to the $95,000 you have invested in it. It might appraise at $60,000 at best, so you’ll be $35,000 underwater and in a world of hurt if you have to sell it. Unless you’re sure that you’ll be keeping the airplane for a many years, it’s generally wise to avoid purchases that involve spending substantially more than fair market value for the aircraft.

What’s worse, 1960 was the first year that Cessna produced the 210, and not surprisingly the earliest models are saddled with expensive Airworthiness Directives and maintenance problems. Cessna learned a lot from building that aircraft for 26 years, and later models of the Cessna 210 are truly outstanding airplanes. But the earliest models are… well… somewhat less outstanding.

I don’t mean to be picking on the Cessna 210 either. The same holds true for early model Bonanzas, Cherokees, Mooneys, etc. You can often buy one for a song, only to discover your new acquisition is eating you out of house and home. Unless you’re an A&P with lots of free time and looking for a “project airplane,” my advice is generally to buy the latest model year you can reasonably afford, and to avoid aircraft requiring high-ticket refurbishment.

Outdated avionics

Old Narco AvionicsThe conventional wisdom used to be that it was better to search for an airplane with suitable avionics than to buy one with older radios and refurbish the radio stack. That’s because a new radio stack increases the resale value of the aircraft only a small fraction of what it costs to buy and install. So it’s a lot more economical to let the other guy upgrade the panel than for you to do it.

These days, however, you may have little choice in the matter. We’re in the midst of a major avionics revolution, with terrestrial navaids getting phased out and GPS WAAS and ADS-B and real-time weather fast becoming a must-have for serious cross-country flight. Unless you luck out and stumble across an airplane for sale with a G-1000 or Aspen Evolution already in the panel—and that’s not terribly likely—you may have to bite the bullet and spring for the gear yourself.

Still, it’s best to find an aircraft with reasonably up-to-date avionics and minimizing the amount you’ll have to invest in electronics refurbishment. Installing a new autopilot is especially expensive, and it’s a big plus if you can find an aircraft that already has a decent autopilot installed.

Worn paint or interior

Worn SeatDon’t hesitate to buy an aircraft just because the paint or interior are getting long in the tooth. Inexperienced buyers tend to get way too hung up on cosmetics. What really counts is what’s under the paint and beneath the carpets. I’d buy a mechanically sound, corrosion-free airplane with shabby paint and interior in a heartbeat.

Think of paint and interior like you think of engines: Something that wears out and has to be redone every ten years or so. It really makes more sense for the buyer to do this after the sale than for the seller to do it before. After all, shouldn’t the new owner get to pick the paint colors and upholstery materials?

Much like engine time, the cost of paint and interior tends to be well reflected in the aircraft selling price. If you buy an aircraft with fully depreciated cosmetics, you can reasonably expect the selling price to be discounted enough to compensate for a substantial portion of the cost of refurbishment.

Mechanical discrepancies

Inspection

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You’ve found a plane you really like a lot, and arranged to have a prebuy examination by a mechanic you trust. The inspection turns up some significant mechanical discrepancies. Now what do you do?

That’s easy: First, talk to your mechanic and determine what it will cost to correct the problems. Next, present the inspection findings and repair estimates to the seller, and see if he’s willing to reduce his selling price enough to cover all, or at least most, of the repair cost. If so, you’ve got a deal; if not, you may want to pass and find another aircraft.

Some discrepancies—corrosion damage to a wing spar, for example—may be so costly to repair that they’re instant deal-breakers. But most discrepancies—say, a soft cylinder or an inoperative autopilot servo—should be readily resolvable.

I’ve seen the prospective buyer of a half-million-dollar Cessna 421C walk away from the deal because the prebuy revealed two cylinders with poor compression. In my view, that’s nuts. The cost of replacing those two jugs is less than one percent of the purchase price. The purpose of a prebuy on a 421C should be to uncover the $50,000 discrepancies, not the $5,000 ones. (If you’re buying a Bonanza or Arrow or Skylane, scale these figures down appropriately.)

Good, clean, mechanically sound, corrosion-free airplanes are getting harder and harder to find, so don’t let a good one get away because of a problem that’s easy to fix.

Why I fly high

Monday, November 23rd, 2015

I take a lot of long trips in my Cessna T310R, and more than half of them involve cruising up in the high teens and low Flight Levels, simply because those are the altitudes at which my airplane is happiest, fastest, and most efficient. But from what I’ve been able to tell, the great majority of piston pilots shy away from using the high-altitude capabilities of their airplanes. Most pilots of normally aspirated airplanes seem to confine most of their flying to altitudes of 10,000’ and below, and even many pilots of unpressurized turbocharged airplanes like mine have never flown in the Flight Levels. It’s even surprising how many pilots of pressurized birds seem averse to flying much above the low teens.

That’s a shame, because it’s at the high end of the altitude spectrum that most of our airplanes achieve their best efficiency—and in many cases, their best speed as well. I’m not just talking about turbocharged airplanes. Most normally-aspirated birds are perfectly capable of cruise altitudes well into the teens.

Look at a plain-vanilla, fixed-gear, normally-aspirated Cessna Skylane:

Cessna 182Q Range Profile

Cessna 182Q Skylane range profile page from POH.

At a low altitude like 4,000’, maximum cruise speed is 139 KTAS at 75% power. Continue climbing until the airplane “runs out of throttle” at 8,000’ and max cruise climbs to 144 KTAS. That extra 5 knots will save you 9 minutes on an 800 NM trip when you take the extra climb into account. (5:38 instead of 5:47, no big deal).

Continue climbing to 12,000’ and max cruise drops back to 139 KTAS (same as at 4,000’), but at a much more fuel-efficient 64% power (which is all you can get at that altitude with wide-open throttle). The same 800 NM trip will take 6 more minutes at 12,000’ than at 4,000’ (5:53 to be exact) because of the longer climb, but burn a whopping 12 gallons less fuel in the process—if avgas costs $5/gallon, that’s $60—and increase IFR range by a full hour and 130 NM!

How far can we take this? Don a cannula and climb to 16,000’—high enough to fly right over the Front Range of the Rocky Mountains IFR—and max cruise drops to a still-respectable 130 KTAS at a miserly 53% power. Because it takes a Skylane nearly 40 minutes to climb from sea level to 16,000’ at max gross, the 800 NM trip will take a half-hour longer than at 12,000’ (6:23), but will save 20 gallons ($100?) and increase IFR range by a full two hours compared to our 4,000’ benchmark.


Cruise
Altitude
Max
Cruise
IFR
Range

To fly an
800 NM Trip

4,000 139 K 820 NM 5:47 78 gal
8,000 144 K 840 NM 5:38 79 gal
12,000 139 K 950 NM 5:53 67 gal
16,000 130 K 1,040 NM 6:23 59 gal

Normally-aspirated, fixed-gear 182Q
(maximum gross weight, standard day, no wind,
88 gallons, 45 min reserve)


Unless you just happen to like low-and-slow, there’s no logical reason to cruise a Skylane lower than 8,000’ because doing so makes all the numbers worse: cruise speed, trip time, and range.  On the other hand, climbing to 10,000’ or 12,000’ will cost you a negligible amount of time, and reward you with substantially lower fuel burn and increased range.

These calculations are all based on zero-wind, but in real life the winds aloft are often a decisive factor in determining the best altitude to choose. If you’re headed eastbound, odds are you’ll have a tailwind—and the higher you fly, the better it’ll be.

In wintertime, climbing up high to catch favorable winds can pay off spectacularly. In the low-to-mid teens, 50 knot tailwinds are commonplace and a 70 or 80 knot tailwind is possible. Even in summer, when winds tend to be relatively light, going high can pay off. Here are some typical summer winds I pulled off of DUATS:


      6000    9000   12000   18000
 STL 2410+18 2809+12 3110+07 2917-04
 SPI 2510+18 3010+12 3211+07 2919-05
 JOT 2511+17 3012+12 3116+06 2926-07
 EVV 2509+17 3012+11 3216+07 3018-05
 IND 2411+16 3011+11 3114+07 2922-06
 FWA 2312+15 2812+10 2916+06 2926-07
 CVG 2210+15 2809+11 3012+07 3021-05
 CMH 2210+14 2710+10 2914+06 3026-07
 CRW 2108+15 2509+10 2908+06 3225-05
 AGC 2010+12 2510+09 2813+05 2930-09
 EKN 1907+13 2608+09 2810+06 3028-07
 PSB 1911+11 2509+08 2813+04 2930-11
 EMI 9900+11 2905+09 2811+05 2927-10

Even in these docile summertime conditions, we can expect 10 to 15 knots more tailwind component at 16,000’ than at 8,000’, which almost exactly offsets the TAS advantage of the lower altitude (144K vs. 130K). By climbing up high on an eastbound trip, we’ll go just as fast, burn considerably less fuel, and increase our IFR range nearly 400 NM! Not to mention that it’s almost always smoother and cooler up high. What’s not to like?

During the winter, when the winds tend to be stronger, going high on eastbound trips tends to be an even better deal, saving both time and fuel.

For turbos, it’s even better

If you’ve got a turbocharger, the argument for flying high becomes compelling, because the higher you fly in a turbo, the higher your speed, range and efficiency—at least up to the low Flight Levels in most turbocharged airplanes. These birds really shine up in the high teens and low twenties, and pilots who don’t take advantage of this capability don’t know what they’re missing.

For example, take a look at the “Range Profile” page for my Cessna T310R:

Cessna T310R Range Profile

Cessna T310R range profile page from POH.

Starting at 180 KTAS at sea level, max cruise speed at 73.6% power steadily increases with altitude to a relatively blistering 221 KTAS at FL200. (Above that altitude, available power starts dropping off fairly rapidly.)


Cruise Altitude Max
Cruise
IFR
Range
To fly an
800 NM Trip
5,000 190 K 860 NM 4:14 143 gal
10,000 199 K 890 NM 4:04 137 gal
15,000 209 K 930 NM 3:55 131 gal
20,000 221 K 970 NM 3:45 125 gal

Turbocharged, twin-engine Cessna T310R
(73.6% cruise, maximum gross weight  standard day, no wind,
163 gallons, 45 min reserve)


At the same time, range with IFR reserves climbs from 820 NM to 970 NM. Naturally, trip time and fuel burn for the proverbial 800 NM trip both drop accordingly—from 4:14 and 143 gallons at 5,000 to 3:45 and 125 gallons at FL200.

Personally, I don’t push my engines this hard. I almost always throttle back to between 60% and 65% power and settle for around 205 KTAS at FL200 at a miserly fuel burn of 26 gallons/hour, giving me a range of well over 1,000 NM with IFR reserves (or 1,200 NM if I fill my 20-gallon wing locker tank).

Once again, these figures assume no-wind conditions. Add in the wind on an eastbound trip and the results can get downright exciting. In the winter, I’ve seen my groundspeed edge above 300 knots from time to time. That’s fun! During the summer, on the other hand, I’m happy with 230 or 240 on the GPS readout.

Needless to say, you pay the piper going westbound. But if the winds aren’t too strong, it may still pay to go high rather than low. In my airplane, I gain 22 knots of true airspeed by climbing from 10,000’ to FL200. So if the headwind at FL200 is only 10 or 15 knots stronger than at 10,000’ (which is usually the case in summertime), higher is still better.

In wintertime, of course, westbound aircraft are all in the same boat, turbo or non-turbo. We bounce along at the MEA, try not to look at the groundspeed readout, hope the fillings in our teeth don’t fall out, and think about how much fun the eastbound part of the trip was (or will be).

Enjoy the high life!

If you’re one of those pilots who comes from the “I won’t climb higher than I’m willing to fall” school, you’ve got nothing to be embarrassed about. Believe me you’ve got plenty of company. But you’re also missing something really good.

Do yourself a favor: give high a try. It’s cooler and smoother up there. Your airplane flies faster and more efficiently up high. ATC will usually give you direct to just about anywhere. You’re above terrain, obstructions, and often the weather and the ice. The visibility is usually terrific. So are the tailwinds, if you’re lucky enough to be going in the right direction. Try it…you just might like it!

Assault on GA Down Under

Friday, October 9th, 2015
Nick McGlone

Nick McGlone with one of his Cessna 210s.

I just got off the phone with my good mate Nick McGlone from Sydney, Australia. For decades, Nick has operated Nautilus Air Services at Sydney’s Bankstown Airport. His firm operates a fleet of Cessna 210 Centurions whose primary mission is to haul sushi-grade fresh fish every day from Tasmania to Sydney. It’s roughly 650 miles from Sydney to Tasmania as the crow flies, about one-third of it overwater.

Now 70, Nick might just be the highest time Cessna 210 pilot in the world, with well over 30,000 hours in type. He’s also a master mechanic (they call them “LAMEs” down there) who maintains his airplanes in tip-top shape. He has to because he depends on them to be mission-ready every day.

After we exchanged a few pleasantries, Nick told me that his airplanes hadn’t flown for months and he was not confident that they would ever fly again. That stopped me dead in my tracks; he had my attention.

CASA’s War on Aging Aircraft

Nick explained to me that in recent years, Australia’s Civil Aircraft Safety Authority (CASA)—the Aussie counterpart to our FAA—had been implementing a series of draconian policies calculated to make it economically impossible for owners of legacy GA aircraft to keep them flying. He said that Bankstown Airport—traditionally the busiest GA airport in Australia—had become a virtual ghost town.

It seems that in 2014, the powers-that-be at CASA handed down a startling ruling that all operators of Australian-registered Cessnas would be required to comply with Cessna’s Supplemental Inspection Documents (SIDs). These SIDs set forth an extraordinarily extensive program of structural inspections that Cessna wants performed on a regular basis.

Some of the inspections in Cessna's SIDs are invasive, labor-intensive, and expensive.

Some of the inspections in Cessna’s SIDs are invasive, labor-intensive, and expensive.

Some of these inspections are relatively easy, but some are extraordinarily invasive and labor-intensive and costly. The SIDs specify a complex matrix of initial and repetitive compliance times for these various inspections. The most invasive and labor-intensive ones are to be done initially when the aircraft reaches 20 years old, and then repetitively every 3, 5, or 10 years thereafter. Of course, since all Cessna 300/400-series piston twins and all 200-series singles and the vast majority of 100-series singles are 30-60 years old, all of them are now past due for these inspections.

The FAA has ruled that compliance with these SIDs is strictly voluntary—NOT compulsory—for U.S.-registered aircraft that are maintained in accordance with the U.S. FARs. But CASA’s 2014 ruling was the exact opposite, and mandates that all Australian-registered aircraft MUST comply with the SIDs, whether the aircraft are in commercial service or private use.

Nick said that this is a catastrophe for Cessna owners in Australia (and in other nations like New Zealand and Germany and Spain who have also ruled that the SIDs are compulsory). Although the FAQ on CASA’s website says that compliance with the SIDs should cost about $20,000, Nick indicated that owners are finding that the actual cost of compliance is between $80,000 and $120,000 for Cessna singles, and close to $200,000 for Cessna twins. This is more than many of these aircraft are worth—or WERE worth before CASA made its ruling. Now, says Nick, the market value of these aircraft in Australia has dropped to near-zero, and many Australian owners are being forced to crate up their aircraft and ship them for sale in the U.S. (where compliance with the SIDs is not required).

Not Just Cessnas, Not Just SIDs

This catastrophe isn’t just limited to Cessnas, either. Now that Cessna’s parent company Textron Aviation owns Beechcraft, they’re feverishly working on developing a SID program for Bonanzas and Barons and other aging Beech airplanes. CASA has made it clear that the moment these Beech SIDs are published, CASA will mandate their compliance. There is even a rumor that Piper is working on a SID program for aging Piper airplanes.

All stainless steel control cables on Australian aircraft have to be replaced by the end of 2017.

All stainless steel control cables on Australian aircraft have to be replaced by the end of 2017.

And if that wasn’t bad enough, CASA has a few other tricks up its sleeve to make operation of aging GA aircraft unaffordable in the land down under. There’s a new Australian AD issued last February that requires that all primary flight control cables that use stainless steel end fittings (as almost all do) must be replaced with new cable assemblies by the end of 2017.  And another Australian AD that requires that all propellers undergo a complete disassembly inspection every six years and a major overhaul at the prop manufacturer’s specified TBO. None of these things are mandated by the FAA for U.S.-registered airplanes, nor is there a history of accidents or incidents in either country to justify such costly maintenance burdens on the owners of GA aircraft.

Nick told me that he is convinced that Textron and perhaps other manufacturers simply want their older aircraft to go away, and that they’ve been successful in enlisting CASA and various other national CAAs in helping them to achieve that goal. All of this is shrouded in the mantle of “aviation safety” despite the fact that there’s virtually zero history of accidents being caused by structural failure, control cable failure, or failure of high-time propellers. Nick could be right.

So next time you start griping about the high cost of personal flying, you might pause and thank your lucky stars that you’re based in the U.S. and not in the land down under. Compared to the rest of the world, we American aviators have it mighty good.

The A&P Exam

Thursday, September 17th, 2015

Although I’ve been an aircraft owner since the late 1960s and heavily involved in GA maintenance since the late 1980s, I didn’t actually become an official card-carrying A&P mechanic until 2001. By the time I decided to go for my A&P ticket, I was already a pretty seasoned aircraft mechanic with a reputation for encyclopedic knowledge of aircraft systems and an aptitude for being able to troubleshoot thorny maintenance issues that had other mechanics stumped. I figured that passing the A&P exam would be a piece of cake.

I figured wrong.

An applicant for an A&P certificate must take and pass three multiple-choice 100-question knowledge tests.

An applicant for an A&P certificate must take and pass three multiple-choice 100-question knowledge tests.

By way of background, an applicant for an A&P certificate must surmount three sequential FAA-imposed hurdles. First, the applicant must prove to his FSDO that he has the minimum required experience performing maintenance on civil aircraft: 30 months on a full-time basis, or 4,800 hours on a part-time basis. Second, the applicant must take and pass three multiple-choice 100-question knowledge tests—mechanic general, mechanic airframe, and mechanic powerplant—and score at least 70% on each one. Third, the applicant must submit to an exhaustive (not to mention exhausting) oral and practical test with a Designated Mechanic Examiner—the mechanic’s equivalent to a checkride—which is normally at least a full-day affair.

When I started studying for the three A&P knowledge tests, my first surprise was the study syllabus, which struck me as being firmly anchored in the 1940s. For example, in preparing for the powerplant test, I reviewed more than 1,000 multiple-choice questions from the FAA’s “question bank” and found that the overwhelming emphasis was on radial engines, pressure carburetors, Hamilton Standard hydramatic propellers, and similar subjects of unquestionable interest to warbird buffs but of absolutely no relevance to contemporary GA aircraft of the sort that interested me. There were only a handful of questions about horizontally-opposed engines, perhaps two or three about fuel injection, only one about modern Hartzell compact hub propellers, and nothing at all about McCauleys.

The question bank for the powerplant test contained not a syllable about any technology that was less than 30 years old. Nothing about engine monitor data analysis, borescope inspections, spectrographic oil analysis, or scanning electron microscopy of oil filter contents. Nothing about compression ignition (Diesel) engines or electronic ignition systems or FADECs or lean-of-peak operation. Similarly, the airframe test was devoid of questions about composite construction (unless you count wood and fabric, which I suppose is the original composite).

To be fair to the FAA, there were actually lots of questions about “modern” 1960-vintage technologies, but they were all related to turbine and transport aircraft. To score a decent grade on the tests, it was obvious that I would need to master lots of material about turboprop and turbojet engines, air cycle machines, Roots blowers, and other esoterica that I knew I’d never remember or have any use for once the test was done.

Mastering the wrong answers

I took my three A&P knowledge tests at a local computerized testing center.

I took my three A&P knowledge tests at a local computerized testing center.

This was frustrating enough, but what really bugged me was that the “official FAA answer” to many of these multiple-choice questions was often the wrong answer. It became obvious that if I wanted to get a good score on the mechanic knowledge tests, I’d have to commit these “FAA answers” to memory even though I knew that they were the wrong answers.

Would you like to see some examples? Here are some actual questions from the 2001 FAA mechanic exam question bank, with the “official FAA answer” that would be used by the FAA to grade the exam:

#8072. Which fuel/air mixture will result in the highest engine temperature (all other factors remaining constant)?

A—A mixture leaner than a rich best-power mixture of .085.

B—A mixture richer than a full-rich mixture of .087.

C—A mixture leaner than a manual lean mixture of .060.

FAA-approved answer: C.

Discussion: Stoichiometric mixture (peak EGT) is around 15:1 or .067, so the FAA-approved answer C (“leaner than .060″ or about 17:1) would be very lean-of-peak, far leaner than most engines can run without unacceptable roughness (unless they are fuel-injected and have tuned fuel nozzles). This is definitely a mixture at which the engine would run cool, not hot. Of the three choices given, the “most correct answer” is A. The FAA-approved answer (C) is just plain wrong, and perpetuates the Old Wives’ Tale that rich mixtures are cool and lean mixtures are hot. With training like this, is it any wonder so many A&Ps blame almost every cylinder malady to LOP operation?

#8678. Why must a float-type carburetor supply a rich mixture during idle?

A—Engine operation at idle results in higher than normal volumetric efficiency.

B—Because at idling speeds the engine may not have enough airflow around the cylinder to provide proper cooling.

C—Because of reduced mechanical efficiency during idle.

FAA-approved answer: B

Discussion: None of the given answers is correct, but the FAA-approved one is the probably the worst possible choice, because it suggests that pilots should keep the mixture full-rich during idle and taxi in order to obtain proper cooling. Do you suppose that OWT explains why so many pilots taxi around at full-rich and foul the crap out of their spark plugs? Are they learning this from their A&Ps? Here’s the correct answer: “Because a very rich mixture is required for cold-starting, and aircraft carburetors don’t have a choke to provide such a rich mixture (the way automotive carbs do), so the idle mixture has to be set extremely rich … which is why as soon as the engine starts to warm up, you need to come back on the mixture control.” Of course, that answer isn’t one of the choices offered.

#8773. Carburetor icing is most severe at…

A—air temperatures between 30 and 40 degrees F.

B—high altitudes.

C—low engine temperatures.

FAA-approved answer: A

Discussion: Are you kidding me? The AOPA Air Safety Foundation briefing on carb ice states, “Icing is most likely to occur—and to be severe—when temperatures fall roughly between 50°F and 70°F and the relative humidity is greater than 60%.” It shows a gory photo of the fatal crash of a Cessna 182 caused by carb ice that formed at OAT 80°F and dewpoint 45°F. If the FAA genius who wrote this question was a pilot, it’s a sure bet that most of his experience is flying Gulfstreams, not Skylanes. (Keep in mind that to get a decent grade on the A&P knowledge test, you have to memorize these FAA-approved wrong answers, or risk failing!)

#8829. Which of the following defects would likely cause a hot spot on a reciprocating engine cylinder?

A—Too much cooling fin area broken off.

B—A cracked cylinder baffle.

C—Cowling air seal leakage.

FAA-approved answer: A

Discussion: Once again, the FAA offers three possible answers and then claims that the “wrongest” one is the one they consider correct. Every IA I’ve asked agrees with me that by far the most likely cause is a bad baffle (answer B), and none has ever seen a case where a cooling fin was broken off badly enough to create an issue.

#8982. If a flanged propeller shaft has dowel pins…

A—install the propeller so that the blades are positioned for hand propping.

B—the propeller can be installed in only one position.

C—check carefully for front cone bottoming against the pins.

FAA-approved answer: B

Discussion: Well that’s interesting. The Continental TSIO-520-BB engines on my 1979 Cessna T310R have flanged propeller shafts. Each flange has a pair of identical dowel pins spaced 180° apart. This permits my three-bladed McCauley C87 props to be installed in two possible orientations, one that results in the vertical blade pointing down when the engine stops, and the other that results in the vertical blade pointing up. According to the Cessna service manual, only one of these orientations is the correct one, so you need to be careful when installing the prop. The FAA-approved answer (B) is just plain wrong. So are the other two answers.

I could go on, but you get the idea.

Mind-numbing

results.

Here’s irrefutable proof that I was able to remember all those FAA-approved wrong answers long enough to score 96, 99 and 99 on my three mechanic knowledge tests.

Well, it took me many hours of study, practice and drill to memorize all of the FAA-approved wrong answers to the thousands of multiple-choice questions in the question bank. As you can imagine, going through this mind numbing exercise was a character-building experience that greatly expanded my vocabulary (of expletives) and bolstered my respect for the cutting-edge mindset of our favorite friendly federal agency.

I guess I must’ve done a workmanlike job of studying and memorizing, because when I finally took the three FAA knowledge tests at my “Don’t try this at home, kids” LaserGrade computerized testing center, I scored 96% on the general and 99% on both the airframe and powerplant. (See Figure 1.) I don’t want to brag, but it’s a rare skill to master so many wrong answers so consistently in such a short period of time, if I do say so myself.

Once the exams were done and my scores were in the bag, I celebrated with the obligatory overnight soak of my brain’s medial temporal lobe (seat of long-term memory) in a 50-50 mixture of cheap champagne and methyl ethyl ketone, just to make absolutely sure all those FAA-approved wrong answers and Old Wives’ Tales were permanently purged from my gray matter. After all, it would certainly be embarrassing to inadvertently pass any of them on to the next generation of A&P mechanics, wouldn’t it?

Is Your Aircraft Okay to Fly?

Thursday, July 23rd, 2015

Who decides whether or not your aircraft is airworthy?

Airworthy steampEarlier this year, I wrote an article titled “Fix It Now…Or Fix It Later” that was published in a major general aviation magazine. The article discussed how to deal with aircraft mechanical problems that arise during trips away from home base. It offered specific advice about how pilots and aircraft owners can decide whether a particular aircraft issue needs to be addressed before further flight or whether it can safely wait until the aircraft gets back home. I considered the advice I offered in this article to be non-controversial and commonsense.

I was surprised when I received an angry 700-word email from a very experienced A&P/IA—I’ll call him “Damian” (not his real name)—condemning my article and accusing me of professional malfeasance in advising owners to act irresponsibly and violate various FARs. Damian’s critique started out like this:

After reading Mike Busch’s commentary “Fix It Now … Or Fix It Later,” I must take exception to most, if not all, the points made in his column. I believe his statements are misleading as to the operation of certified aircraft, to the point of being irresponsible for an A&P to suggest or imply that it’s up to the owner/operator whether or not to fly an aircraft with a known discrepancy. The FARs are quite clear on this matter, and there have been numerous certificate action levied on pilots who have operated aircraft with known discrepancies.

Damian went on to state that the FARs require that any aircraft discrepancy, no matter how minor, must be corrected and the aircraft approved for return to service “by persons authorized under FAR 43.7 (typically the holder of a mechanic certificate).” He went on to explain that the owner/operator may only approve for return to service those preventive maintenance items listed in FAR Part 43 Appendix A. He went on:

It should be noted that the FAA does not take into consideration the inconvenience or cost related to addressing a known discrepancy. Nor is it up to the owner/operator to determine the significance of a discrepancy as the FARs do not confer this discretion privilege to the owner/operator.

Damian’s attack on my article continued at great length, making it quite clear that his believe is that pilots and aircraft owners are mere “appliance operators” in the eyes of the FAA, and that only certificated mechanics are empowered to evaluate the airworthiness of an aircraft and determine whether or not it is legal and safe to fly. He ended his diatribe by saying:

I hope that others in the aviation community such as FAA Airworthiness Safety Inspectorss and aviation legal professionals weigh in on this commentary. I believe all will agree that this commentary is misleading and uninformed to the point of being irresponsible even to publish. At the very least, pilots that follows the advice of Busch’s commentary should enroll in the AOPA Pilot Protection Services plan because they’re likely to need it!

Whew! Strong stuff! If Damian is right, then the FAA had better lock me up and throw away the key. Fortunately for me, I believe he isn’t and (at least so far) they haven’t.

Where Damian Has It Wrong

Damian and I do agree on at least one thing: FAR 91.7 does indeed say quite unequivocally that it is a violation to fly an unairworthy aircraft, and that if the aircraft becomes unairworthy in flight, the PIC is obligated to discontinue the flight. I would never suggest for a moment that any pilot fly a known-unairworthy aircraft, at least without a ferry permit. That’s a no-brainer.

The much more difficult question is: Exactly how does the PIC decide whether or not an aircraft is airworthy or unairworthy, and therefore whether he is or isn’t allowed to fly it? On this question, Damian and I part company. In fact, his view and mine seem to be diametrically opposite.

Damian’s view is that almost any aircraft discrepancy requires the involvement of an A&P mechanic to evaluate and clear the discrepancy and approve the aircraft for return to service. I see absolutely nothing in the FARs to support such a position, particularly when it comes to non-commercial aircraft operated under Part 91.

To begin with, the basic airworthiness rule (FAR 91.7) is crystal clear about who is responsible for determining whether or not the aircraft may be flown. It says:

The pilot in command of a civil aircraft is responsible for determining whether that aircraft is in condition for safe flight.

The regulation places the burden squarely on the shoulders of the PIC. I don’t see anything there about A&Ps or repair stations having to be involved, do you?

Looking a bit deeper into the FARs, I can find only three circumstances under which a mechanic is required to get involved in making any sort of airworthiness determination on a Part 91 aircraft used for non-commercial purposes:

  1. Exactly once a year, FAR 91.409 requires that an annual inspection be performed by an A&P/IA or a Repair Station. But the other 364 days of the year, it’s the PIC who determines whether the aircraft is airworthy.
  2. When an Airworthiness Directive or Airworthiness Limitation becomes due, FAR 91.403 requires that a mechanic must certify that the AD or AL has been complied with (with rare exceptions where the PIC may do so).
  3. When an owner actually hires a mechanic to perform maintenance on an aircraft, in which case the mechanic is required to document his work and sign it off to testify that the work was performed properly. Note, however, that the mechanic’s signature in the logbook entry does NOT signify that the aircraft is airworthy, only that THE WORK PERFORMED by the mechanic was done in an airworthy fashion.

This third point is one that is frequently misunderstood by mechanics and owners alike. When I teach this stuff at IA renewal seminars, the hypothetical example I often use to illustrate this important point involves an owner who takes his aircraft to a mechanic for repair. The mechanic immediately observes that the aircraft has two obvious discrepancies: the right main landing gear tire is flat, and the left wing is missing. The owner asks the mechanic to fix the flat tire. The mechanic does so, makes a logbook entry describing the work he did on the right main landing gear, and signs it. His signature denotes only that the work he did (fixing the flat tire) was done properly. When the owner picks up the aircraft, the mechanic tells the owner, “I couldn’t help but notice that your left wing is missing. If you’ll permit me to offer you a word of friendly advice, I would not attempt to fly the aircraft until that issue is resolved.” But the missing left wing does not prevent the mechanic from signing the logbook entry. In fact, the mechanic is required by regulation to sign the logbook entry, regardless of whether the aircraft is airworthy or not. The mechanic’s signature addresses only the work performed by the mechanic, and nothing else.

The PIC’s Burden

If you’re on a trip and some aircraft discrepancy occurs – assuming the aircraft isn’t in the midst of its annual inspection and there’s no AD involved – it is up to you as PIC to determine whether or not that discrepancy makes the aircraft unairworthy or not. If you decide that it does, then you can’t fly the airplane until the airworthiness issue is rectified (and that might require hiring an A&P). On the other hand, if you decide that the discrepancy doesn’t rise to the level of making the aircraft unairworthy, then you’re free to fly home and deal with the issue later.

Under the FARs, it’s totally the PIC’s call. There’s no regulatory obligation for the PIC to consult a mechanic when making such airworthiness determinations. Having said that, however, it would certainly be a wise thing to do if you feel uncomfortable about making the decision yourself. It’s your call.

The FARs provide considerable help to the PIC in making such airworthiness determinations. FAR 91.213(d) describes a specific algorithm for deciding whether or not it’s okay to fly an airplane with various items of inoperative equipment. FAR 91.207 says that it’s okay to fly an aircraft with an inoperative ELT to a place where it can be repaired or replaced, no ferry permit required. FAR 91.209 says that position lights needn’t be working if you’re flying during daylight hours. And so on.

If your experience is anything like mine, what most of us call “squawks” are common occurrences, but the majority of them don’t rise to the level of being airworthiness items that cause us (in our capacity as PIC) to conclude that a fix is required before further flight. Even if you do encounter a genuine airworthiness problem – say a flat tire or dead battery or bad mag drop – that still doesn’t mean that you necessarily need to get a mechanic involved. The FARs provide (in Part 43 Appendix A) a list of roughly three dozen items that a pilot-rated owner or operator is permitted to perform and sign off on his own recognizance (without getting an A&P involved).

If you have a flat tire, for example, you (as a pilot-rated owner) are permitted to repair or replace it yourself. If you have a dead battery, you can charge it, service it, or even replace it. If you have a bad mag drop, the most common cause is a defective or fouled spark plug, and you’re permitted to remove, clean, gap, and replace spark plugs yourself. You are also allowed to make repairs and patches to fairings, cowlings, fabric (on fabric-covered aircraft), upholstery and interior furnishings. You can replace side windows, seat belts, hoses, fuel lines, landing and position lamps, filters, seats, safety wire, cotter pins, and more. You can even remove and install tray-mounted avionics from your panel.

Now, you might well prefer to hire an A&P to do some of these things rather than do them yourself, especially when on the road, far from your hangar and toolbox. I know I certainly would, and I’m an A&P myself. But Damian’s contention that you are compelled by the FARs to place your aircraft in the hands of an A&P any time any sort of discrepancy arises is simply not supported by the regulations.

Contrary to what Damian and many of his A&P colleagues may believe, the FAR’s place the responsibility for determining the airworthiness of the aircraft squarely on the PIC, except for once a year when an IA is required to make an airworthiness determination after performing an annual inspection

My colleague Mac McClellan pointed out to me that this closely resembles how the FAA determines whether a pilot is “airworthy.” One day every year or two or five, we pilots are required by regulation to go get an examination from an Aviation Medical Examiner who pronounces us medically fit to fly, or not. The remaining 364 or 729 or 1,824 days in between, the FAA expects us to self-certify that we’re medically fit. “Can you imagine,” Mac asked me rhetorically, “if we had to go to see an AME every time we got a sore throat or runny nose?”

The Back Door is Locked

Friday, June 12th, 2015

Cessna 210In my AOPA Opinion Leaders Blog post of September 2014 (“Backdoor Rulemaking?”), I discussed the unprecedented action taken by the Cessna Aircraft Company intended to compel the owners of cantilever-wing Cessna 210s to perform repetitive eddy-current inspections of their wing spars. Finally, I can fill you in on the punch line.

By way of background: Normally, if an aircraft manufacturer believes that an unsafe condition exists that justifies imposing special inspections, component life limits, replacement or overhaul times, or similar burdens on aircraft owners, they go to the FAA and ask for an Airworthiness Directive (AD) to be issued. If the FAA is persuaded that the alleged unsafe condition actually constitutes a significant safety concern and that the burden on owners is reasonable given the safety risk, then the FAA issues a Notice of Proposed Rulemkaing (NPRM) announcing its intention to issue an AD and soliciting comments on the proposal from the affected public. The FAA is then required to consider and respond to all public comments submitted during the comment period before issuing its final rule that makes the AD effective. This same notice-and-comment protocol is required of all executive-branch regulatory agencies of the U.S. federal government by a law called the Administrative Procedure Act (APA).

Indeed, that’s precisely what Cessna did in 2013: It asked the FAA’s Wichita Aircraft Certification Office (ACO) to issue an AD mandating repetitive eddy-current inspections on all cantilever-wing Cessna 210s. But to Cessna’s chagrin, the Wichita ACO turned down Cessna’s request and declined to proceed with an AD, presumably because the ACO was not persuaded that such an AD was justified.

That should have been the end of the matter. But it wasn’t.

In February 2014, Cessna very quietly published a revision to the Cessna 210 service manual that added three new pages to the manual. Those three pages constituted a new section 2B to the manual, titled “Airworthiness Limitations,” that called for the repetitive eddy-current spar inspections. Somehow Cessna persuaded the Wichita ACO to approve this amendment—something the ACO really shouldn’t have done, as you shall see.

Cessna then publicly took the position that compliance with the repetitive eddy-current spar inspections was compulsory because those inspections were now part of an FAA-approved Airworthiness Limitations Section (ALS). Indeed, FAR 91.403(c) compels aircraft owners to comply with mandatory replacement times, inspection intervals, and related procedures specified in an ALS. And FAR 43.16 compels maintenance personnel to perform any inspections or maintenance specified in an ALS precisely “by the book.”

David vs. Goliath?

SlingshotI first learned about this at the beginning of September 2014, when my colleague Paul New—owner of Tennessee Aircraft Services, Inc. (a well-known Cessna Piston Aircraft Service Center) and honored by the FAA in 2007 as National Aviation Maintenance Technician of the Year—discovered the new section 2B in the Cessna 210 service manual, and immediately realized its significance. Paul and I discussed the matter at length, and both felt strongly that Cessna’s actions could not be allowed to go unchallenged.

“If Cessna gets away with this,” I told Paul, “then any manufacturer will be able to effectively impose their own ADs whenever they want, bypassing the notice-and-comment protocol and the other safeguards built into the APA to protect the public from unreasonable government regulation.”

I helped Paul draft a letter to the Rulemaking Division (AGC-200) of the FAA’s Office of General Counsel, questioning the retroactive enforceability of Cessna’s newly minted ALS against Cessna 210s that were manufactured prior to the date the ALS was published (i.e., all of them, given that Cessna 210 production ceased in 1986). Our letter questioned whether Cessna could do what it was trying to do (i.e., make the eddy-current inspections compulsory) within the confines of the APA. We asked AGC-200 to issue a formal Letter of Interpretation (LOI) of the thorny regulatory issues that Cessna’s unprecedented actions raised.

And then we waited. And waited.

AGC-200 initially advised us that they had a four-month backlog of prior requests before they would be able to respond to our request. In fact, it took seven months. It turns out that our letter questioning the enforceability of Cessna’s ALS opened a messy can of worms. AGC-200 assigned two attorneys to draft the FAA’s response, and they wound up having to coordinate with AFS-300 (Flight Standards Maintenance Division), AIR-100 (Aircraft Certification Division), ACE-100 (Small Airplane Directorate), and of course ACE-115W (Wichita Aircraft Certification Office) who mistakenly approved Cessna’s ALS in the first place.

FAA Legal Does the Right Thing

FAA Headquarters

FAA Headquarters
800 Independence Ave.
Washington DC

Finally, on May 21, 2015, AGC-200 issued the Letter of Interpretation (LOI) that we requested. It was five pages long, and was everything we hoped it would be and more. It slammed shut the “rulemaking backdoor” that Cessna had been attempting to use to bypass the AD process, locked it once and for all, threw away the key, and squirted epoxy glue in the lock for good measure. You can read the entire LOI in all its lawyerly glory, but here’s the CliffsNotes version of the letter’s key bullet points:

  • Under FAR 21.31(c), an ALS is part of an aircraft’s type design.
  • The only version of an ALS that is mandatory is the version that was included in the particular aircraft’s type design at the time it was manufactured.
  • Absent an AD or other FAA rule that would make the new replacement times and inspection intervals retroactive, Cessna’s “after-added” ALS is not mandatory for persons who operate or maintain the Model 210 aircraft, the design and production of which predate the new ALS addition. The “requirements” set forth in the ALS would only be mandatory for aircraft manufactured after the ALS was issued. And of course, production of the Cessna 210 ceased in 1986.
  • If operational regulations were interpreted as imposing an obligation on operators and maintenance providers to comply with the latest revision of a manufacturer’s document, manufacturers could unilaterally impose regulatory burdens on operators of existing aircraft. This would be legally objectionable in that the FAA does not have legal authority to delegate its rulemaking authority to manufacturers. Furthermore, “substantive rules” can be adopted only in accordance with the rulemaking section of the APA (5 U.S.C. § 553) which does not grant rulemaking authority to manufacturers. To comply with these statutory obligations, the FAA would have to engage in its own rulemaking to mandate the manufacturer’s document, as it does when it issues ADs.

The bottom line is this: Manufacturers of certificated aircraft* are not permitted to impose regulatory burdens on aircraft owners by changing the rules in the middle of the game. Only the FAA may do that, and only through proper rulemaking action that complies with the APA (including its notice-and-comment provisions and other safeguards). If you ever encounter a situation where the manufacturer of your aircraft tries to do this, call their cards—the FAA lawyers will back you up.

*NOTE: The rules are completely different for S-LSAs.  The manufacturers of S-LSAs can do pretty much anything they like, and their word is the law. (A seriously flawed situation IMHO.)

The LOI concluded with the following surprising paragraph:

On February 19, 2015, the FAA’s Small Airplane Directorate sent a letter to Cessna that addressed some of the above issues, and pointed out the non-mandatory nature of the after-added ALS for the Model 210 aircraft. The FAA asked Cessna to republish the replacement times and inspections as recommendations that are encouraged, but optional, for those in-service aircraft, unless later mandated by an AD. To date [three months later –mb] Cessna has not provided a written response outlining its position on this matter.

Are we having fun yet?

When to say “no” to maintenance

Wednesday, May 13th, 2015

Ken is the proud owner of a late-model high-performance single-engine airplane. It’s a gorgeous machine, with wall-to-wall glass in the cockpit, a big turbocharged engine, 500 hours on the Hobbs meter, almost no squawks, and still under factory warranty on both engine and airframe. So when Ken took it to a well-known factory-authorized service center for its annual inspection, he expected that it would be relatively painless. Imagine his shock when the shop presented him with an estimate of more than $8,500. That’s when he called me for advice.

I reviewed the shop’s estimate. It started out with a flat-rate charge for the annual inspection (performed in accordance with the manufacturer’s annual inspection checklist) of $2,850. This was 30 hours of labor at the shop’s rate of $95/hour, which in my experience was right on target for this make and model.

Probing deeper

The next item that caught my eye was a $200 estimate for cleaning the engine’s fuel injector nozzles. I used to do such prophylactic nozzle cleaning on my own airplane until about 10 years ago, when I had an illuminating discussion with George Braly (of GAMI and Tornado Alley Turbo fame), who is arguably the world’s expert on fuel nozzles. George pointed out to me that there’s no valid reason to do such periodic nozzle cleaning, because the nozzles do not get dirty in service (since they are continuously being cleaned by a very effective solvent). He told me that in his experience with many thousands of GAMIjector nozzles, virtually all clogged nozzle events occurred shortly after maintenance during which the fuel system was opened up and some foreign material got into the system. That resonated with me, because in the first 12 years I owned my Cessna T310R, I experienced two clogged-nozzle episodes, and both occurred right after maintenance due to grease getting into the fuel system. So I stopped cleaning my nozzles 10 years ago, and haven’t had a clogged nozzle since. I advised Ken to decline the nozzle cleaning.

There was a $300 estimate to replace the O-rings on the brake calipers. I asked Ken whether he had spongy brakes or had any evidence of brake fluid leakage at the calipers. He said no. I suggested he decline the O-ring replacement.

Continental S-20 magnetoThere was a $1,700 estimate for “4-year overhaul of pressurized mags”—$700 for each magneto plus 3 hours to remove and reinstall. The aircraft is equipped with Continental S-20 mags, and the Continental Ignition System Master Service Manual X40000 calls for a 500-hour IRAN (inspect and repair as necessary), not an overhaul. The IRAN typically costs $300 to $400 per mag, depending on what parts need to be replaced. I suggested that Ken instruct the shop to do the 500-hour IRAN instead of the overhaul exchange, which would knock about $700 off the invoice.

There was a $400 estimate to replace the magneto pressurization filter. The filter is clear plastic (actually tinted green) so you can inspect it and see if it needs to be changed. It was clean as a whistle. I suggested that Ken decline the filter change.

Teledyne-Gill G-243 batteryNext was a $800 estimate to replace the battery. The aircraft manufacturer’s checklist recommends replacing it every two years, and Ken’s was two years old. But the battery manufacturer (Teledyne-Gill) recommends doing an annual capacity test and replacing the battery only when its capacity falls below 80% of specs. Using the capacity-test method, these batteries typically last 3 to 5 years before flunking the test. Another thing that bothered me was that the battery—a Gill G-243—cost $395 at Aircraft Spruce, but was listed on the estimate as costing $774. Now I don’t have a problem with shops making a fair profit on the parts they install, but marking up a $395 battery to $774 struck me as a bit much. So I suggested that Ken decline the battery change, wait until the battery flunks its capacity check, and then consider buying the battery and installing it himself.

Then there was a $320 estimate to change the filter in his TKS anti-icing system. The manufacturer recommends changing this filter every 2 years (and his was 2 years old), but in hundreds of filters changed we’ve never seen one that wasn’t spotlessly clean. The shop agreed with this observation. I advised Ken that unless he had some reason to believe someone dumped a Diet Coke into his TKS tank, he should decline the TKS filter change.

Bottom line

Ken called the service center and politely declined the various items that I’d recommended. Ken reported that the shop’s Director of Maintenance had no problem complying with Ken’s instructions, and the invoice wound up some $3,000 lower than it would have been otherwise. That’s enough to buy a fair amount of 100LL, even at today’s prices.

Now many of you are probably thinking that this service center was trying to rip Ken off, and he should never take his airplane back there again. I disagree.

Gavel + wrenchIn today’s litigious world, any mechanic or shop that doesn’t recommend following the manufacturer’s guidance to the letter risks being sued and taken to the cleaners if anything goes wrong. Therefore, in my view, Ken’s service center was almost compelled to present Ken with the estimate that they did. Call it “defensive maintenance” or “CYA” if you wish, but it’s the way things are in today’s post-GARA, non-tort-reform world.

The way I see it, the responsibility for “just saying no” to these over-the-top maintenance recommendations lies with the aircraft owner, not the shop. If the aircraft owner instructs the shop (in writing) that he declines some manufacturer-recommended maintenance task, that takes the shop off the liability hook and allows them to do things the way the owner wants them done without fear of being sued.

Therefore, if an owner wants to avoid paying through the nose for such defensive maintenance, he needs to learn when to say no.

When to say no

Learning when to say no takes a good deal of knowledge and experience, but there are some basic rules. The most important rule is that you never say no to any maintenance procedure that is required by regulation. For example, FAR Part 43 Appendix D requires that every annual inspection on a piston aircraft must include a compression test of the cylinders, cutting open the oil filter to inspect for metal, and running up the engine to check that critical engine operating parameters (oil pressure, static RPM, etc.) are within normal limits. Mechanics are also required to comply with any “Airworthiness Limitations” contained in the manufacturer’s service manual or ICAs. Any applicable Airworthiness Directives must be complied with. All these things are non-negotiable.

Airworthiness definedIt’s also best to avoid saying no to proposed repairs that the inspecting A&P/IA considers to be “airworthiness items.” Those are generally discrepancies that he considers to be safety-of-flight items, and will not be comfortable approving the aircraft for return to service until they are corrected. But don’t be fooled. Many of the items that I suggested Ken decline were listed on the shop’s estimate as “Airworthy Item,” yet when Ken instructed the shop not to do them, they accepted his direction without argument. So just because an item is listed on the estimate as an airworthiness item doesn’t necessarily mean that it really is one. When in doubt, say no and see how the IA responds. If he tells you he’s not comfortable signing off the annual unless you approve the repair, then it’s time to re-think your position.

Good candidates for saying no to include time-directed maintenance recommendations for things that can be readily done on-condition instead. Ken’s battery, pressurization filter, brake O-rings and TKS filter are good examples. (So are most engine and propeller TBOs in my opinion, but not everyone agrees with me.) Consider ignoring the time recommendations and replace or repair these items only when inspection shows that they need to be replaced or repaired. We should only be maintaining things on time (like the 500-hour magneto IRAN) if there’s no practical way to maintain them on-condition.

Also consider saying no to preventive maintenance items intended to prevent failures whose consequences you consider acceptable. For example, replacing your vacuum pump every 500 hours (per the manufacturer’s recommendation) is silly if you have dual vacuum pumps or a standby vacuum system or a backup electric attitude indicator. If a vacuum pump failure doesn’t affect safety of flight, why not simply run it to failure and then replace it? Ditto if you have dual alternators.

Finally, consider saying no to an overhaul if an IRAN will do the job (as with Ken’s mags), and consider saying no to replacing anything that can be repaired instead.

The art of saying no is definitely an acquired skill, but one that can save you a small fortune in reduced maintenance costs once you get the hang of it. Like any acquired skill, practice makes perfect.

How to destroy your engine in one minute

Monday, April 13th, 2015

At least once a year for as long as I can remember, I have been contacted by an aircraft owner whose piston aircraft engine was destroyed or severely damaged by a destructive detonation or pre-ignition event. In one recent 12-month period, I encountered three such incidents.

One incident involved British Cirrus SR-20 powered by a 200 horsepower Continental IO-360-ES engine. The plane was equipped with an Avidyne Entegra MFD with an integrated engine monitoring system called “EMAX.”

The CHT data downloaded from the EMAX system tells the short story of this engine’s demise:

SR-20 pre-ignition event

Click on image to open a higher-resolution version.

Everything looked fine until about two minutes after the pilot applied takeoff power, at which point the #1 cylinder’s CHT began to climb rapidly compared to the other five cylinders. At the three-minute mark after brake release—with the aircraft at roughly 2,000’ AGL—CHT #1 rose above 400°F and set off a high-CHT alarm on the MFD.

CHT #1 continued its rapid rise—nearly 1°F per second—that continued unabated until the piston and cylinder head were destroyed approximately five minutes after takeoff power was applied and two minutes after the CHT alarm was displayed. At that point, since the cylinder was no longer capable of combustion, CHT #1 started plummeting.

We can’t be sure just how hot CHT #1 got because the Avidyne EMAX system “pegs” at 500°F. A reasonable guess is that the CHT peaked somewhere between 550°F and 600°F. No cylinder or piston can tolerate such conditions for very long, and this one obviously didn’t.

Aftermath

Not long after CHT #1 went off-scale on the MFD, the pilot realized something was very wrong, and pulled the power way back. But he was a couple of minutes late, and the engine was already toast. Here’s what the #1 piston looked like after the event:

Piston with corner melting

Click on image for higher-resolution version.

Note the melted corners of the piston crown, the destruction of the top compression ring lands, and the severe metal erosion above the piston pin. (Much of this molten metal wound up inside the crankcase and contaminated the bearings and oil passages.) Also note the severely hammered appearance of the piston crown, the classic signature of heavy detonation. The cylinder head was found to have a big chunk of metal missing from it. Both spark plugs were destroyed by the event as well.

This engine was a low-time Continental factory engine, so the owner figured that the severe engine damage would be covered under Continental’s warranty. I advised him not to bother filing a warranty claim, because I’ve never known Continental to give warranty consideration for a destructive detonation or pre-ignition event. Continental considers this to be operational abuse, not a defect in materials or workmanship, and therefore not covered by warranty. (For what it’s worth, I agree with Continental’s position on this.) The owner didn’t believe me and filed a warranty claim anyway. Continental promptly and unequivocally denied the claim, just as I predicted.

The moral of the story is that it is important for aircraft owners to have a good digital engine monitor installed, to know the telltale symptoms of destructive detonation and pre-ignition, and to act fast when those symptoms appear. You may have less than one minute to react if you want to save your engine.

Another incident

Here’s another similar case that occurred to a Beech Bonanza very shortly after takeoff. The annotated JPI data for this event is courtesy of General Aviation Modifications Inc. (GAMI):

Preignition event

Click on image for a higher-resolution version.

This time, it was the #5 cylinder that experienced thermal runaway and pre-ignition. It was an even more severe event than the one suffered by the Cirrus, and took only two minutes from the application of takeoff power to the complete destruction of the #5 piston, which wound up with a large hole melted through the piston crown:

Holed Piston

Click on image for a higher-resolution version.

Now that’s ugly!

In yet another case (for which I unfortunately have no photos), a drop-dead gorgeous Lancair IV-P kitplane powered by a fire-breathing 350-hp TCM TSIO-550 engine went up for its first test flight after 10 years of laborious building time by the owner. Within minutes, the airplane was back on the ground with an engine that was totally destroyed. A forensic post-flight evaluation revealed that the magnetos had been timed approximately 10 degrees advanced from the proper timing. That turned out to be a $50,000 mistake.

The Lancair’s instrument panel was wall-to-wall glass, including an ultra-sophisticated digital engine monitoring system. The engine monitor was literally crying out for attention throughout the short test flight, but the test pilot never noticed its warnings until the engine cratered.

What causes this?

There are a number of things that can cause or contribute destructive events like these. I’ve already mentioned one: advanced ignition timing. It’s astonishing how often we see engines with the magneto timing advanced several degrees from spec. (E.g., 25° BTDC when the engine data plate calls for 22° BTDC.) Even a couple of degrees is enough to significantly reduce the detonation margin of the engine. Add a hot day and perhaps a cooling baffle that isn’t quite up to snuff, and BOOM!

Owners should be particularly alert for mis-timed magnetos whenever maintenance is done that involves magneto removal or adjusting magneto timing. (More often than not, these occur during the annual inspection.) If mag timing is advanced, you’ll notice that your EGTs are lower and your CHTs are higher than what you were seeing prior to maintenance. (Retarded timing results in the opposite: higher EGTs and lower CHTs.) If you notice this after the airplane comes out of maintenance, take it back to the shop and have the mag timing re-checked. It’s a quick check and could save your engine (not to mention your gluteus maximus). Magnetos are required to be timed within one degree of the timing specified on the engine’s data plate, and any error should be in the retarded direction.

MP and FF guage comboAnother common culprit is inadequate fuel flow on takeoff. When taking off from a near-sea-level airport—or from any elevation if you’re flying a turbocharged airplane—you need to see fuel flow that’s right up against the red-line on the gauge (or the maximum fuel flow shown in the POH). Unlike most other gauges on your panel, hitting red-line on the fuel-flow gauge (or even going a smidgen over) is a good thing, not a bad thing. Takeoff fuel flow is a lot like tire pressure—a bit too much is a whole lot better than a bit too little. Anything less than red-line fuel flow on takeoff reduces the engine’s detonation margin, and significantly less can reduce it enough to cause a catastrophic event.

Not long ago, a client of my maintenance-management firm had a prop-strike incident that required a teardown inspection of the engine. When the inspection was complete and the engine was reinstalled in the airplane, the owner picked up the airplane from the engine shop and flew it back to his home base airport. Upon arriving there, he informed us that the fuel flow was 3 GPH below red-line on takeoff, and asked that we schedule a service appointment to have the fuel flow adjusted.

I was flabbergasted. What was this owner thinking? Why didn’t he abort the takeoff immediately when he noticed that the fuel flow was 3 GPH short, and ask the engine shop to adjust it? Why would he fly the airplane home in that condition? What part of “inadequate detonation margin” didn’t he understand?

Yet another cause is a partially clogged fuel injector nozzle. This can occur anytime, but most frequently occurs shortly after the aircraft comes out of maintenance because that’s the most likely time for foreign material to get into the fuel system. (I’ve had two serious clogged-nozzle episodes in my airplane over the past 25 years, and both occurred shortly after an annual inspection.)

Save your engine!

ThrottleRegardless of the cause, the solution is not rocket science. There are two simple rules that will almost always prevent these sorts of destructive events from occurring:

First, check your fuel flow gauge early on every takeoff roll. If the fuel flow is not at red-line or very close to it, reject the takeoff and sort things out on the ground. (The exception is takeoffs at high density altitudes in normally-aspirated airplanes, and detonation is quite unlikely under those conditions.)

Second, set your engine monitor CHT alarm to 400°F or less for Continental engines and 420°F or less for Lycoming engines. (On my own Continental-powered airplane, I have my alarm set to 390°F.) When the alarm goes off, do whatever it takes right now to bring the CHT back down below 400°F. Verify that the mixture is full-rich. Turn on the boost pump if it isn’t already on. Open the cowl flaps if you have them. And if CHT triggers the alarm and appears to be rising rapidly, throttle back aggressively to stop the thermal runaway. Don’t be shy about doing these things immediately, because you may only have a minute or two to act before your engine craters.

(Oh, and if your airplane isn’t equipped with a digital engine monitor with CHT alarm capability, do yourself a favor and install one. Trust me, it’ll pay for itself quickly.)

When you get on the ground, put the airplane in the shop and have the spark plugs removed and inspected for damage, the cylinders borescoped, and the magneto timing checked. If takeoff fuel flow was short of red-line, have it adjusted before further flight.

Champion Aerospace: From Denial to Acceptance

Thursday, March 19th, 2015

Champion Aviation Spark PlugsAccording to the model popularized by Dr. Elisabeth Kübler-Ross in her seminal 1969 book On Death & Dying, there are five stages of grief: denial, anger, bargaining, depression, and acceptance. This is apparently what Champion Aerospace LLC has been going through over the past six years with respect to the widely reported problems with the suppression resistors in its Champion-brand aviation spark plugs. I last discussed this issue in my August 2014 blog post Life on the Trailing Edge.

I first became aware of the Champion spark plug resistor problem in 2010, although there’s evidence that it dates back to 2008. We were seeing numerous cases of Champion spark plugs that were causing bad mag drops, rough running and hard starting even though they looked fine and their electrodes weren’t worn anywhere near the retirement threshold. The thing these spark plugs had in common were that they were all Champion-brand plugs and they all measured very high resistance or even open-circuit when tested with an ohmmeter.

We also saw a number of cases where high-resistance Champion plugs caused serious internal arc-over damage to Slick magnetos (mostly in Cirrus SR20s). If the damaged mag was replaced without replacing the spark plug, the new mag would be damaged in short order. The cause-and-effect relationship was pretty obvious.

In researching this issue, I looked at the magneto troubleshooting guide on the Aircraft Magneto Service website, maintained by mag guru Cliff Orcutt who knows more about aircraft ignition systems than just about anyone I know. Cliff owns and operates my favorite mag specialty shop, and that’s where I send the mags on my own airplane every 500 hours for inspection and tune-up. In reading Cliff’s troubleshooting guide, I came across the following pearls of wisdom:

  • Take an OHM Meter and measure the resistance value from the connection in the bottom of the barrel to the clean center electrode at the firing end, electrode must be bare metal.
  • A new Champion plug will have a value of 800 to 1200 OHMS. New Tempest (formerly Unison-Autolite) will measure 1000 OHMS.  Replace any plug above 5000 OHMS.
  • A spark plug bomb tester can test a bad plug and lead you to conclude it is serviceable. The OHM Meter check is simple, readily available, and amazingly accurate in finding misfiring plugs.

We started asking the maintenance shops we hired to maintain our clients’ aircraft to ohm out the plugs at each 50-hour spark plug maintenance cycle. The number of plugs that measured over 5,000 ohms was eye-opening. Many plugs measured tens or hundreds of thousand ohms, and it wasn’t unusual to find plugs that measured in the megohm range or even totally open-circuit. Here, for example, is a set of 12 Champion plugs removed for cleaning and gapping from a Cirrus SR22 by a shop in South Florida:

Champion spark plug resistance

Notice that only two of these 12 plugs measured less than 5K ohms, and one of those had to be rejected because its nose core insulator was cracked (a separate issue affecting only Champion fine-wire spark plugs, and unrelated to the resistor issue that affected all Champion plugs).

Why spark plugs have resistors

Worn spark plug

A worn-out spark plug.

Early aviation spark plugs didn’t contain resistors. They didn’t last long, either. The reason was that each time the plug fired, a significant quantity of metal was eroded from the electrodes. Magnetos fire alternate spark lugs with alternate polarities, so half of the plugs suffered accelerated erosion of their center electrodes, and the other half suffered erosion of the ground electrodes. Eventually, the ground electrodes became so thin or the center electrode became so elliptical that the plug had to be retired from service.

Spark plug manufacturers found that they could extend the useful life of their plugs by adding an internal resistor to limit the current of the spark that jumps across the electrodes. The higher the resistance, the lower the current. And the lower the current, the less metal eroded from the electrodes and the longer the plug would last before the electrodes got so worn that the plug had to be retired.

Adding a resistor to the plug also raised the minimum firing voltage for a given electrode gap. The result is a hotter, more well-defined spark that improves ignition consistency and reduces cycle-to-cycle variation.

The value of the resistor was fairly critical. If the resistance was too high, the plug would fire weakly, resulting in engine roughness, hard starting, excessive mag drops, and (if the resistance was high enough) arc-over damage to the magneto and/or harness. If the resistance was too low, the plug electrodes would erode at an excessive rate and its useful life would be short. Experimentation showed that a resistance between 1K and 4K ohms turned out to be a good compromise between ignition performance and electrode longevity. Brand new Champion-brand aviation spark plugs typically measure around 1,200 ohms fresh out of the box. New Tempest-brand plugs typically measure about 2,500 ohms. Both of these represent good resistance values right in the sweet spot.

Denial

As word of these erratic and wildly out-of-spec resistance values began reaching aircraft owners and mechanics (primarily via the Internet), Champion went on the defensive. At numerous aviation events and IA renewal seminars, Champion reps dismissed the significance of resistance measurements. They explained that the silicon carbide resistor in Champion-brand plugs is made to show the proper resistance whenever a high-voltage pulse is present, and can’t necessarily be measured properly with an ohmmeter. Further, they stated that the proper way to test a spark plug is on a spark plug testing machine (so-called “bomb tester”), and claimed that if a plug functions well during a bomb test, it should function well in the airplane.

Champion old insulator assembly

Champion old insulator assembly.

Of course, this “company line” from Champion didn’t agree with our experience. We’d seen numerous instances of high-resistance Champion plugs that tested fine on the bomb tester but functioned erratically in service. Nor did it agree with the Mil Spec for aviation spark plugs (MIL-S-7886B) which states clearly:

4.7.2 Resistor. Each spark plug shall be checked for stability of internal resistance and contact by measurement of the center wire resistance by the use of a low voltage ohmmeter (8 volts or less). Center wire resistance values of any resistor type spark plug shall be as specified in the manufacturer’s drawings or specifications. 

One enterprising Cessna 421 owner named Max Nerheim performed high-voltage testing of Champion spark plugs, and found that plugs that measure high-resistance or open-circuit with a conventional ohmmeter also had excessive voltage drop when fired with high voltage, and required a higher minimum voltage to produce any spark. Max Nerheim wasn’t just an aircraft owner, mind you, he was also Vice President of Research for TASER International, Inc. and was exceptionally qualified to perform high-voltage testing of Champion spark plugs. Nerheim’s findings flatly contradicted Champion’s company line, and agreed with what we were seeing in the field. Nerheim also disassembled the resistor assemblies of a number of high-resistance Champion plugs and found that the internal resistor “slugs” were failing.

Anger

What's your resistance?The spit really hit the fan when Champion’s primary competitor in the aviation spark plug space, Aero Accessories, Inc., launched a marketing campaign to promote sales of its Tempest-brand aviation spark plugs by highlighting the resistance issue. (Aero Accessories acquired the Autolite line of aviation spark plugs from Unison Industries in 2010, an re-branded them under its Tempest brand.) In February 2013, they issued a Tempest Tech Tip titled “The Right Way to Check Spark Plug Resistors,” started selling a fancy spark plug resistance tester, and launched a big “What’s Your Resistance” advertising campaign in the general aviation print media.

Predictably, this provoked a rather hostile response from Champion. Their field reps ratcheted up their public relations campaign claiming that the ohmeter check was meaningless, and insisting that Champion spark plugs didn’t have a resistance problem that affected the performance of their plugs.

Bargaining

In the face of both overwhelming technical evidence from the field that their spark plugs had a resistor problem, and a virtual blitzkrieg from their principal competitor that was starting to erode their dominant market share, Champion began having some self-doubts. Max Nerheim discussed his high-voltage test findings with Kevin Gallagher, Manger of Piston and Airframe at Champion Aerospace, and Gallagher acknowledged that Champion was looking into the issue with the resistor increasing in impedance, but did not have it resolved yet. Meanwhile, the Champion field reps continued to insist to anyone who would listen that claims of resistor problems in Champion spark plugs were false and that the ohmmeter test was meaningless.

Finally…Acceptance

Sometime in late 2014, it appears that Champion very quietly changed the internal design of their spark plugs to use a sealed, fired-in resistor element that appears to be quite similar to the design of the Tempest/Autolite plug. They didn’t change any part numbers. So far as I have been able to tell, they didn’t even issue a press release. The Champion Aerospace website makes no mention of any recent design changes or product improvements. But the cutaway diagram of the Champion spark plug now on the website shows the new fired-in resistor. Here are the old and new cutaway diagrams. Compare them and you’l clearly see the difference.

Click on images below to see higher-resolution versions.

Champion spark plug cutaway (old)

Champion spark plug cutaway (old)

Champion spark plug cutaway (new)

Champion spark plug cutaway (new)

I checked with a number of A&P mechanics and they verified that the latest Champion spark plugs they ordered do indeed have the new design. It’s easy to tell whether a given Champion spark plug is of the old or new variety. Simply look at the metal contact located at the bottom of the “cigarette well” on the harness end of the plug. The older-design plugs have a straight screwdriver slot machined into the metal contact, while the newer-design plugs do not.

As I write this, it’s still too early to tell whether Champion’s quiet resistor redesign will cure the drifting resistance problem, but my best guess is that it will. If I’m right, this is very good news indeed for users of Champion aviation spark plugs. I applaud Champion Aerospace for improving its product.

Still, I can’t help but wonder why it took six years for the company to work through its grief from denial to acceptance. I suppose grief is a very personal thing, and everyone deals with it differently.