Backcountry Pilot • C 170A upgrade to O360

C 170A upgrade to O360

Have you modified your aircraft? STC? STOL Kit? Major rebuild from just a data plate?
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Re: C 170A upgrade to O360

fiftynineSC wrote:Coming from a 180/185 guy that flew a 170 early on....I do see a "mission" for a 180 horse 170. Great airplane, flies really nice. No, it doesn't make economic sense to convert in most cases, but I look at it differently. If you have a proven 170 that you have upgraded and trust in every way other than the C-145, mitigate the conversion cost and just wait till TBO. Not spending money rebuilding a C145 and doing the conversion at rebuild time can take the sting out. If I had a rock solid 170 that I loved, and my mission didn't creep to "4 place" then I'd do the conversion. Probably fixed pitch too.

Bill


You make good points on "Knowing the airplane". Seems like every airplane I buy, I have to spend a year and lots of $$ making it "right" for me #-o . So, starting with a known quantity that you're happy with is a good idea.

As to the fixed pitch prop point, I'd never go there with a 180 hp 170. That constant speed prop offers all sorts of advantages. Staying with a fixed pitch prop really limits many of the significant advantages of the conversion. And, the MT prop isn't that much heavier than a fixed pitch prop. But, they are expensive.

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Re: C 170A upgrade to O360

You’ll never make sense of how someone else spends their money.

And it’s confirmed: 170’s are not 180’s…probably why they have different model numbers. Converting a 170 to 180hp vs buying a 180 is an interesting economic yin and yang, but that’s a pretty narrow view of the entire decision process, especially for someone who already owns a 170 that they are fond of. Like a lot of people, I’ve spent the years I’ve owned my plane making it better… Everything from avionic and instrument upgrades to new wires all the way to the P-leads, fine wire spark plugs, Bass harnesses, new tail springs and axel hardware and brake lines and gas lines and pretty much anything else that I ever saw and thought I could improve on… and I started out with a very, very nicely restored airplane to begin with. Lots of those improvement are not things I’m ever going to get my money back out of in a sale; they’re things I did because it makes me feel better when I look out the window and see nothing but rocks and trees for miles and miles. Hitting the reset button with a unknown airplane is not a small decision, especially for a backcountry bird. Something as simple as a broken tail spring probably won’t hurt you, but the cost of getting it repaired in the backcountry sure could sting a bit. On the other hand, a corroded 30-cent wire from the ignition switch can kill you a sure as a bullet if it fails at the wrong time.

As for economic hogwash, I think that cuts both ways. If it’s just as cheap to run a 180, I’m hard pressed to understand why anyone is flying anything smaller. There are lots of old sticks that USED to own 180’s and now fly something smaller, and it’s not because the 180 ever let them down. To be fair, I believe that the fuel cost per mile is about the same between the 180hp 170 and a 180. But acquisition costs, insurance, property tax, airframe maintenance, time to TBO, cost of overhaul, and expected engine maintenance before TBO are not the same between the two planes. That stuff counts, too. If I’m completely wrong then please pardon my ignorance. I did the math and decided the 170 was considerably less expensive to own and operate over the long haul, and I had no reason to try and convince myself one way or another. I could easily pay cash for any 180 or 185 on the market if I so desired. But I’ve got a lot of hobbies and there’s a finite amount of money I want to spend on aviation. Again…forgive me if my conclusions don’t match yours.

Mike, you’ve probably forgotten more about flying than I’ve ever learned, and I don’t doubt for a minute that you could hop in my plane and show me a thing or two or ten, but I respectfully disagree about a 180hp 170 being a capable backcountry performer at GROSS weight, at least where I like to play. Lightly loaded my STOL 170 gets off the ground like a flea and climbs faster than Russian inflation, but there’s just a limit to what 180hp can do and a couple hundred pounds makes a huge difference.

Any of the Middle Fork or Big Creek airstrips are going to have an average summertime DA of between 4500 and 6000 feet, at DAWN. Lots of them also have a down-canyon tailwind until it warms up ten degrees, and +/- 1,000 foot, rough airstrips. Add to that some serious obstacle clearance issues, downdrafts over the rivers, and the need for maneuvering immediately after take off, and I sure won’t use the tighter ones at anything close to gross weight in my 170. You’re a better stick than I am and maybe you would, but I kind of doubt it.

Even the wide open, super-long airstrips like Chamberlain Basin (5,765 msl), Cold Meadows (7,030 msl), Meadow Creek (3,984 msl) or Schafer (4,856 msl) require a substantial rate of climb to clear terrain after take off. At gross weight on a typical summer morning I’d be pretty unhappy if I wasn’t flying just as soon as it was light enough to see, and even then I’d be cursing myself for being heavy. I’ve gotten close enough to the trees at a couple hundred pounds under gross, thank you very much. Now I’m no hot stick and I get that, but I’ve got about 1000 hours in my 170 and a pretty intimate understanding of what it does and how to get the most out of it. Maybe I’m overly cautious. Clearing the tree tops by 50 feet isn’t good enough for me, especially if I have to do it for an extended period of time with the CHT’s and oil temp creeping up to the red line.

Hence my aversion to larger fuel tanks. Even stock tanks cary too much fuel with two people and camping gear n' food for most of these strips, most of the time, at least for me. My fuel bladders are no more likely to get contaminated and easier to inspect and clean than a tip tank is…I don’t see the risk there. Fuel bladders don’t make for the most comfortable cargo I agree, but those wing tanks inches from our heads are anything but crash worthy. And I’ve seen tip tank’s getting installed…brand new they are worse than the vintage Cessna tanks they feed into. I guess if it bothered me enough I’d go back to steel jerry cans strapped into the Atlee Dodge rear seat rails, which, in my opinion, are less likely to rupture in a crash than the wing tanks. But at the end of the day I rarely cary extra fuel at all, and if I do it’s a forgone conclusion I’m going into a pretty easy strip, so I accept the risk.

Whether it’s economically prudent for Fishdoc to convert his 170A vs buy a already converted 170B or a 180 is a question only he can answer. I’d rather have syphilis than take on a project that big, but I also know people who would have as much fun doing the conversion as they’d have owning the end result. To each his own.

But in the event he does convert his 170A, my humble opinion is that he should seriously consider keeping the 39 gallon tanks…
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Re: C 170A upgrade to O360

^^^Hey Hammer, it's good to see you posting on here again. Always enjoyed your contributions. Long-time members who we don't hear from for a while make me wonder if they've hung it up- good to see you haven't.
-DP

p.s. to the O.P.- There's no such thing as one perfect airplane for all occasions, so don't sweat the false dichotomies. What puts a smile on YOUR face?
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Re: C 170A upgrade to O360

As I said before,if fishdoc likes the 170A do the conversion and good for him. For me it comes down to one thing, legal useful load. The 180 hp 170B I just bought has 701 on wheels and just 590 on wheel skis, the lightest of them may have 800 at best. I want to operate on wheel skis., I am the fat guy at 250 lbs. I would like to be at 230 but you can call me lazy if you want but that is the way it is and has been for 25 years. So I can't carry full fuel with another guy on skis, and lets face it most of the guys I know are 200 or better. That is why I will finish and fly the 180H project I have, and yes it will have the Kenmore 3190 STC, not because I want to operate at 3190 but to be legal at 2801 or what ever it takes that day. I know that at heavy weights I will have less performance but not every runway I use requires maximum performance. If the legal gross was 2400 with the conversion I would keep the 170 as it does what I want, just not with company.

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Re: C 170A upgrade to O360

bat443 wrote:As I said before,if fishdoc likes the 170A do the conversion and good for him. For me it comes down to one thing, legal useful load. The 180 hp 170B I just bought has 701 on wheels and just 590 on wheel skis, the lightest of them may have 800 at best. I want to operate on wheel skis., I am the fat guy at 250 lbs. I would like to be at 230 but you can call me lazy if you want but that is the way it is and has been for 25 years. So I can't carry full fuel with another guy on skis, and lets face it most of the guys I know are 200 or better. That is why I will finish and fly the 180H project I have, and yes it will have the Kenmore 3190 STC, not because I want to operate at 3190 but to be legal at 2801 or what ever it takes that day. I know that at heavy weights I will have less performance but not every runway I use requires maximum performance. If the legal gross was 2400 with the conversion I would keep the 170 as it does what I want, just not with company.

Tim


That is one heavy 170 for sure. You could put it on a diet and gain a lot of useful load back. I believe MTV's 180hp 170 was 1350ish empty on wheels. Depending on how I have my plane configured it's between 1285 and 1336 with the stock motor. 1285 is with 8.00s and no rear seats and 1336 is with rear seats and 26" bushwheels.

I've thought long and hard about if I will ever do the 180hp conversion, or sell the 170 and get a Skywagon. I think I will eventually go another route though.... Keep the 170 how it is for fun flying, and buy a 2nd airplane to fill the family hauling and cross country aspect of my mission. I can probably have both for less than the price of a nice 180-185 set up the way I would want it. Plus I just don't want to sell the 170 after all the time and money I've put into it.
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Re: C 170A upgrade to O360

Hammer,

Many of your points are well taken. And, I'm no super pilot, believe me. But, in response to a couple points you made:

You've stretched what I posted regarding STOL performance waaaaay out of shape, and molded it to represent something I never intended.

The STOL performance information I provided was near sea level, at gross weight. My point was not that you'd operate at that weight at high DA, but offered as a benchmark of what the airplane is capable of.

The Valdez STOL contests are fun, but somewhat unrealistic, since the airplanes are typically stripped to the extent possible and de-fueled and of course the contest is near sea level and cool weather. Still, their performance at the contest does suggest something about the performance these airplanes are capable of in more realistic conditions. And, a couple of high hp 170s did pretty well this year at Valdez. So, my point was simply that the high hp 170, under a specific set of conditions, will get in and out of a spot tighter than a 180 will, and more comfortably, under the same conditions.

Secondly, I have no idea how you'd GET to any of the strips you mentioned at or even close to gross weight, unless you started your trip well over gross weight. It takes some gas to get to these places. That's where the extra gas helps as well. I can put on a load of gas where it's relatively cheap (and with a big runway) and fly non stop to those places (200 miles or so) land, and still have enough gas to go roam around some, then get to a gas station. Saving $$ on every gas fill up means more flying for this kid.

Likewise, hardly anybody is launching out of those remote strips at gross weight, early morning or not, so your lecture on that topic is a good reminder, but has nothing to do with what I was discussing.

But, if you're happy with stock fuel, that's great. Aux fuel tanks are expensive, no doubt. But, there's a reason that Part 135 air carriers aren't allowed to carry gas cans in the cabin with passengers. As you say: To each his own.

Finally, your comment about reliability in your first paragraph may be well intended but you used the wrong example: "On the other hand, a corroded 30-cent wire from the ignition switch can kill you as sure as a bullet if it fails at the wrong time."

In fact, if ALL the wires connected to your ignition switch were to fail simultaneously, you likely wouldn't even know it had happened. The ignition system in your airplane is designed to fail to the "hot" condition, so if a wire from the switch fails, you simply have a hot magneto and no engine failure.

MTV
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Re: C 170A upgrade to O360

mtv wrote:
fiftynineSC wrote:Coming from a 180/185 guy that flew a 170 early on....I do see a "mission" for a 180 horse 170. Great airplane, flies really nice. No, it doesn't make economic sense to convert in most cases, but I look at it differently. If you have a proven 170 that you have upgraded and trust in every way other than the C-145, mitigate the conversion cost and just wait till TBO. Not spending money rebuilding a C145 and doing the conversion at rebuild time can take the sting out. If I had a rock solid 170 that I loved, and my mission didn't creep to "4 place" then I'd do the conversion. Probably fixed pitch too.

Bill


You make good points on "Knowing the airplane". Seems like every airplane I buy, I have to spend a year and lots of $$ making it "right" for me #-o . So, starting with a known quantity that you're happy with is a good idea.

As to the fixed pitch prop point, I'd never go there with a 180 hp 170. That constant speed prop offers all sorts of advantages. Staying with a fixed pitch prop really limits many of the significant advantages of the conversion. And, the MT prop isn't that much heavier than a fixed pitch prop. But, they are expensive.

MTV


Mike,

I'm sure you are right....with the MT it would be even better. I just early on flew a straight model 170 that was stripped, a field approved (allegedly :P ) O-360, a fixed Mac climb prop and 8.50's. I remember being overwhelmed how cool it was. I always kind of the liked the "clean" economy of how simple that plane was. Of course, that's coming from me....the guy who bought a 185 that only flies solo, locally and 30 gallons of gas. My "mission" selector is broken. :oops: :D
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Re: C 170A upgrade to O360

You've stretched what I posted regarding STOL performance waaaaay out of shape, and molded it to represent something I never intended.


I'm glad to hear that Mike...I was starting to feel a bit insecure about my pilotage. I mean I've always been a cautious cat, but maybe I was taking it too far? I guess the guy who bought your plane doesn't live in Bozeman.

Secondly, I have no idea how you'd GET to any of the strips you mentioned at or even close to gross weight, unless you started your trip well over gross weight. It takes some gas to get to these places.


Obviously nobody would take off over gross weight...it's against the rules. But I guess shooting an elk would be one way to have the option to leave a backcountry strip at gross weight. Or in my case, my wife collects rocks. Lots and lots of rocks...

But, there's a reason that Part 135 air carriers aren't allowed to carry gas cans in the cabin with passengers.


I'm pretty sure that's because the passengers would steal them?


n fact, if ALL the wires connected to your ignition switch were to fail simultaneously, you likely wouldn't even know it had happened.


I believe you, but I still replaced all the wiring. When my mechanic asked why I was doing it I shrugged, replaced all the wires and connectors, and wrote him a check. Then I tapped the ignition five times (five for alive), walked around the airplane anti clockwise four times and then clockwise four times (eight keeps things straight), and buckled and unbuckled each seatbelt six times (six is the fix) so as to put the world back in order. Don't laugh, it worked.
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Re: C 170A upgrade to O360

Hammer wrote:...Then I tapped the ignition five times (five for alive), walked around the airplane anti clockwise four times and then clockwise four times (eight keeps things straight), and buckled and unbuckled each seatbelt six times (six is the fix) so as to put the world back in order. Don't laugh, it worked.


Hard to argue with success.
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Re: C 170A upgrade to O360

fiftynineSC wrote:My "mission" selector is broken. :oops: :D


This is one of the most common equipment failures in aviation.
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Re: C 170A upgrade to O360

Zzz wrote:
fiftynineSC wrote:My "mission" selector is broken. :oops: :D


This is one of the most common equipment failures in aviation.


:D

Closely followed by another key failure. "A short" between the pilot's seat and the yoke.
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Re: C 170A upgrade to O360

I have enjoyed reading this thread immensely!

I must ask the question now, what if the 170 GW was bumped up to 2400 for the 180 horse Lycoming...

How much more usefulness, legally, are we even looking at with the extra 200lbs getting approved? After all, I don't expect a show of hands, but how many guys have found themselves obviously over gross with their Lycoming, yet still made the decision to fly? Then furthermore.. how did the aircraft perform?

I should expect the pireps from you guys flying Idaho backcountry are going to differ significantly from many of the AK destinations..

My initial impression, is that if you're flying at a DA of 2-3k, that extra 200lbs might be welcomed with enthusiasm. However, if it's common to fly at 5K and above, perhaps not so much ...

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Re: C 170A upgrade to O360

VFRsim wrote:My initial impression, is that if you're flying at a DA of 2-3k, that extra 200lbs might be welcomed with enthusiasm. However, if it's common to fly at 5K and above, perhaps not so much ...


Hell, at only 2-3kft DA I would love a 200lb gross weight increase with the stock engine. I've routinely climbed to 10-12k with my C-145 at gross, went to 15k once with oxygen.... Ok it took a while. A 180hp 170 should handle an extra 200lbs just fine, just don't try the shorter strips at that weight.

WingX is approved in Canada on the 170 and gives a 200lbs gross weight increase when combined with180hp or greater. They say they are working on the U.S. STC.
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Re: C 170A upgrade to O360

Rob,

I was essentially thinking of back country flying, so yes, shorter strips.

There's another U.S.STC that I have in mind, besides the Wing-X. Something that I hear, through the grapevine, might be pretty close to getting approved.

- Joseph
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Re: C 170A upgrade to O360

I don't really know anyone who flys out of true backcountry strips at gross weight no matter what they fly.
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C 170A upgrade to O360

robw56 wrote:I don't really know anyone who flys out of true backcountry strips at gross weight no matter what they fly.


I think Battson has said he's operated his BH at gross (2500 lbs) in the NZ backcountry, not sure what DA. I think the power to weight ratio heavily stacked in your favor is the key. Even with 180hp the 170B is still not in the STOL performance arena at gross. And of course, there's no specific definition of how short STOL is.
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Re: C 170A upgrade to O360

How much more usefulness, legally, are we even looking at with the extra 200lbs getting approved?


In my opinion the legality issue is really important to commercial operators...not as important to Joe Sixpack. It's almost unheard of for a 170 model Cessna to be used commercially...at least where a gross weight increase would be of any value. I've looked at the WingX site and cannot determine if the spar reinforcement is necessary because of the additional wing surface and longer bending arm, or if it's what really makes the gross weigh upgrade. I understand how more wing lifts more weight, but I don't understand how more wing lifting more weight is any safer than less wing lifting the same weight, assuming there is power to do so and the pilot knows enough not to stall.

If an engineer could show me why it was inherently dangerous for me to accidentally fly at 2400 lbs, and how the WingX upgrade would make it safe to do so, I guess I'd be interested, or at least curious. If the WingX simply improves lift performance enough to meet some arbitrary criteria important to the FAA, but not affecting the safety of flight for someone who knows enough not to hit the trees at the end of the runway, I wouldn't spend the money just to be legal.

There are certainly some long, low-elevation backcountry airstrips with easy departure profiles where a guy hauling a carcass out in November could use a full 2400 lbs. Of course, there are a whole lot more where a GW increase wouldn't help at all, unless by some marvel of engineering you can now take off at 2200 lbs in the same space you used to need at 2000 lbs...which I rather doubt.
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Re: C 170A upgrade to O360

Hammer wrote:If an engineer could show me why it was inherently dangerous for me to accidentally fly at 2400 lbs, and how the WingX upgrade would make it safe to do so, I guess I'd be interested, or at least curious. If the WingX simply improves lift performance enough to meet some arbitrary criteria important to the FAA, but not affecting the safety of flight for someone who knows enough not to hit the trees at the end of the runway, I wouldn't spend the money just to be legal.

There are certainly some long, low-elevation backcountry airstrips with easy departure profiles where a guy hauling a carcass out in November could use a full 2400 lbs. Of course, there are a whole lot more where a GW increase wouldn't help at all, unless by some marvel of engineering you can now take off at 2200 lbs in the same space you used to need at 2000 lbs...which I rather doubt.


I disagree. Frankly, wing structure is not always what limits gross weight.....more often, landing gear, climb performance, and even engine cooling in the climb are the limiting factors.

In my opinion, those performance criteria are certainly not arbitrary. In fact, due to the significant over-engineering most planes have, it's performance that's most of concern to the pilot, or it should be.

Wing X , by increasing wing area, significantly increases takeoff performance, climb performance, and permits the plane to fly at a lower AOA in level flight, all because of that additional wing area.....more lift works. And that additional performance really helps when you're heavy.

And, in fact, in some cases, yes, you can take off heavier in the same distance with more wing area.

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Re: C 170A upgrade to O360

I disagree. Frankly, wing structure is not always what limits gross weight.....more often, landing gear, climb performance, and even engine cooling in the climb are the limiting factors.

In my opinion, those performance criteria are certainly not arbitrary. In fact, due to the significant over-engineering most planes have, it's performance that's most of concern to the pilot, or it should be.

Wing X , by increasing wing area, significantly increases takeoff performance, climb performance, and permits the plane to fly at a lower AOA in level flight, all because of that additional wing area.....more lift works. And that additional performance really helps when you're heavy.

And, in fact, in some cases, yes, you can take off heavier in the same distance with more wing area.

MTV


I'm not sure what you're disagreeing with.

I'm just curious why the WingX gets a gross weight upgrade, and if there is a safety of flight issue not related to the performance of the additional lift created by the extra wing.

If it's just as structurally safe for me to fly my 170 200 lbs over gross, as a private operator, I'd not be inclined to spend the money for a gross weight increase unless there was a serious performance improvement that came along with it. And maybe there is...I've never looked into it and have no idea.

Obviously from a performance stand point the 180hp upgrade is an improvement. I don't have any hard numbers, but I'd GUESS that a 180hp, CS prop 170 can fly the same profile as a stock 170 while carrying 200 additional pounds, so that makes me wonder what it is about the WingX that provides the GW increase, and if any or all or part of it is structural.
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Re: C 170A upgrade to O360

VFRsim wrote:...There's another U.S.STC that I have in mind, besides the Wing-X. Something that I hear, through the grapevine, might be pretty close to getting approved. - Joseph


"What if" -ing isn't much use. It either is legal, or not.
What's the other STC for, and does it increase gross weight?
Or is it one of those "I can tell you, but then Ill have to kill you" things? :roll:
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