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Autopilot Debate
My PA-30 has an Altimatic III Autopilot. Here's a pic of the control head:
Also related - it has a selector switch to govern what heading / nav source it's tracking and just under that is a separate on/off switch and trim adjustment for the backup "Autoflite" system. Here's another pic:
I've read the book several times and experimented with all this in flight. Basically the Autopilot itself is Attitude based and is based on the vacuum driven attitude indicator. As a backup Piper incorporated the "Autoflite" system which is based on an electric turn-coordinator type system and is really just a wing leveler. The idea being that if you are IMC and your vacuum-attitude based autopilot fails you can switch it off and turn on the Autoflite wing leveler as a secondary / backup system.
I have to say that from what I've read / experienced and understand, this autopilot was way ahead of it's time (perhaps not unlike Comanche aircraft in general). If working properly there is really nothing this autopilot won't do. It has altitude pre-select (albeit on a fairly "gross" scale), auto-trim, a glide slope coupler (where installed). and other features. It even incorporated an air-speed limiter to prevent the aircraft descending at such a rate it exceeded airspeed limitations (Vno / Vne) and on the climb it prevents climbing into a stall by swallowing the climb to avoid getting too slow. As an attitude based autopilot the turns are crisp and decisive. I am used to flying with a rate-based S-Tec 55X and have now come to realize how much more "crisp" the turn in and response are in an attitude based autopilot like this old Altimatic (also our S-Tec 55x in the Cirrus is not too good in turbulence being rate based).
On the down side... the altitude pre-select is on a pretty "gross" in it's scale. It's not like setting a digital altitude in tens of feet but rather turning a knob to rotate a drum (see the first pic). Also it has to be calibrated on each flight due to baro changes. The disadvantage of being attitude based is that it's based n a vaccum attitude indicator spinning 3x as fast as a turn coordinator. I've heard it argued that a rate based S-Tec and the turn coordinator gyro are more reliable.
My autopilot performed well on the test flight pre-purchase. I've read a post from Kristen Winter (pretty sure it was Kristen's post) where she advised the autopilot as an item to test thoroughly and carefully and I have to agree with this. I probably did not test mine enough pre-purchase and have discovered just how crazy expensive these things are to repair or replace.
Here's where I am today... my Altimatic III will track a heading or nav source (VOR/GPS) very well. On a LOC it will track but did seem to S-turn quite a bit before locking on. Probably an adjustment issue. I don't think I have a GS coupler or if I do it's not working. It will hold altitude if I play around with it. However I have never seen the autopilot adjust the electric trim so I think the autotrim is probably inop. Also, the altitude preselect works some of the time but not often and not with any precision. My impression is there are dirty contacts in there somewhere and I can get it to climb but not descend. Also it's out of calibration. The little round window with the horizontal line used for calibration is slanted slightly down when it thinks it's level. Finally... my Piper Autoflite system is completely Inop and I don't think it worked when I bought the plane. The prior owner said it did but candidly I did not test this and I've read alot about mis-understandings of how these systems work. For instance, if you don't turn the Altimatic Off before turning Autoflite on then the wing leveling you are getting is coming from the Altimatic not the Autoflite.
I spoke to Bob Furguson out at Autopilots Central. He said the systems can be made to work. He said the only part they can't get / replace is a "bellows" that is used in the altitude hold function. He said if mine holds altitude at all (which it does) then that is probably not a problem. He said to fix it they would really need me to fly the plane out to them in Oklahoma and let them pull the whole thing apart, overhaul it, then reinstall it all and test / calibrate. Cost wise he said he could only give me an "idea" but worst case it could approach $10K. So I might spend $4K if not much is wrong but maybe I'd spend close to $10K. If I went this route and everything was made to work like it should it seems like I would have a very capable autopilot with features that would cost more like $30K installed if I were going with a new S-Tec of similar capability. That said I worry that I'd be "throwing good money after bad" investing so much in a 45 year old autopilot with limited parts support.
Another idea is to spend say $15K installing a basic S-Tec 30 or 50. That would give me a new autopilot and while it would cost more (no knowing how much more since I really don't know if the Altimatic repair would be 4K or 10K) it would at least be a known outcome (or should be). it would have altitude hold but no vertical speed or altitude preselect or even a glideslope coupler but no big deal I'd just hand fly approaches, I often do anyway.
While I've had no problems with the S-Tec 55x in the Cirrus I have noticed quite a few posts on the web on different forums about S-Tec issues - particularly since they were acquired by Cobahn. I've read comment about lower quality components being used in servos and the like but I don't know if that's really true.
Another question... what about Century? A Century 2000 is attitude based and the costs seem lower but avionics suppliers and shops I've spoken to seem to recommend away from Century and towards S-Tec. Many seem to say that S-Tec is the "only game in town". I've heard shops say that Century won't work with shops they only work with owners so shops prefer S-Tec.
I've also called Avidyne and ended up emailing with the VP of Product Development in charge of the new DFC-90. Predictably he would not give me any info on if or when the DFC-90 would be available for PA-24/30/39 aircraft but he agreed it would be a good platform. He said a Mooney 201 or similar would probably be the next platform and that they need to get through their existing pipeline of commitments before considering other airframes. So for now the DFC-90 is not an option, maybe it will be one day.
Anyway that's a lot of commentary... I'd appreciate any thoughts or feedback from those who have already been down this path, especially recently...
Thanks,
- Charles
Charles Schefer- Posts: 563
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Re: Autopilot Debate
Agree on the work with owners but not shops comment.
Patricia Jayne (Pat) Keefer ICS 08899
PA-39 #10 Texas
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Re: Autopilot Debate
One thing I am investigating to converting the Altimatic III to an Altimatic IIIC/Century III, which is the same unit. The servos are the same, as is the computer/amplifer. The control head and the altitude sensing device needs to be changed. This unit has the control head with four rocker switches, one roll knob and one pitch wheel in the same sized package as the Altimatic III. It has not altitude preselect or speed control. Basically, they removed features and simplifed to improve reliability. It has the altitude hold feature instead of the preselect. The coupler etc is the same.
Piper put the Altimatic IIIC in thousands of airplanes from about 1975 through about 1983 or so. Century sold it as the Century III to Beech, Mooney, Aero Commander, so they are common and I understand that all parts are available. I am going to call Autopilot Central one of these days and see what they think about making that conversion. Both are STC'ed for the PA-30 and I believe PA-24, but didn't specifically check that.
Kristin Winter- ICS member
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Re: Autopilot Debate
The Stec tied to a 430W greatly simplifies ifr.
Good luck with your decision, Don
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Re: Autopilot Debate
Funny to hear someone go with S Tec due to V pump failures but not electric - in the past our problem was electric but not v pump failures.
Patricia Jayne (Pat) Keefer ICS 08899
PA-39 #10 Texas
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Re: Autopilot Debate
Mark Anderson
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Re: Autopilot Debate
Didn't I just read an article about a twin Comanche having a double vacumn failure?:-)
Don
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Re: Autopilot Debate
Yes, you did - that's why I was so careful in my phrasing ... "in the past". After 43 years in and around 22G, the vast majority of problems have been electrical in nature. The worst being the double alternator failure in IMC - just 3 hours after annual, a belt and a bearing - no warning.
As you saw in the article, one vacuum pump failure, about 6 hours of flying before the second - I can only guess, bad batch. These situations are why when I'm flying for keeping engines happy on my weekly flight, I hand fly and hand fly all 90% of all practice instrument work. I do use the A/P on most trips and to make sure it is still working as expected on 10% of the practice instrument flying.
There are risks any way you go. Do know Mom replaced S Tec altitude hold and original Piper A/P to get the C2000 in. I haven't been faced with an A/P decision, I just know we're happy with the C2000 and the added GPSS with 530W.
Patricia Jayne (Pat) Keefer ICS 08899
PA-39 #10 Texas
N3322G- ICS member
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Re: Autopilot Debate
I had one problem a cold solder joint in the wire harness to the radio coupler and one pulled wire from another connector under the floor board, both happened at different upgrade times. Once when removing 40 years of avionic wiring upgrade remains under the floor and once after redoing the panel. I was lucky to trace them without much trouble, but when people have problems with this older equipment often the answer is the cabling/ connectors. And regardless of who the shop is mistakes can be made so look around for the obvious and the not so obvious.
Also I believe that a lot of units out there were sent out for overhauls over the years and just put back into the airplane without doing the inflight setup. Its not hard to do but if not done you won't get the proper performance from it.
In my case when I got the airplane the autopilot would bank 35 degrees one way and only 20 the other way, I would descend at flutter speed and climb at 110 mph. With one flight with the front face removed and the limit pots adjusted properly it worked as new and 4 years later it still is rock solid.
If you have some time before dropping a lot of cash on new or overhauling, I would do a rough check on your connectors and cabling ( especially your auto trim sensor, there isn't much to go wrong with that unit except wiring connectors and dirty contacts)
Also if you have wandering headings or wing rocking this can be as simple as incorrect aileron cable tensions or the computer sensitivity set to high. There are 3 places where you can make adjustments to the altimatic 3, The computer installed behind the hatrack, the controller( pot switches behind the faceplate) and the radio coupler( adjusts the intercept angles).
If after you have exhausted the inexpensive things and you still have for instance wing rocking or heading problems then go for the servo overhaul or the new autopilot installation.
Good luck,
Gary
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Re: Autopilot Debate
- Charles
Charles Schefer- Posts: 563
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Charles Schefer- Posts: 563
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Re: Autopilot Debate
I would only keep it if you could get it operating with minimum investment. Like I said before alot of times the problem is in the cabling
and connectors, so overhauling units such as servos and computers will not fix the problem.
You could get a good idea of the money that is required by taking it to a shop that has all the century test equipment. They could test each unit individually
and if all passes, then they can test your cabling for problems. Not sure what they will charge for that, but if you are confident that most of the components are good,
it might be worth saving the old autopilot.
Regarding the level off within 100 feet, I must admit it isn,t that accurrate, I have to nurse it to the level....but it does work. Also with long flights and altimeter changes
you have to adjust the altitude on the controller as well.
Gary
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Re: Autopilot Debate
- Charles
Charles Schefer- Posts: 563
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Re: Autopilot Debate
because of the expansion differences between the aluminum hull and the steel cables. Anyway that would be an easy check to elliminate your autotrim
problem if its because of the cables being to tight or to loose.
Gary
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Re: Autopilot Debate
The stab Trim cable is 12 lbs +- 20 %. These specs are taken from the revised Piper Pitch Trim Manual dated 2/25/77.
I haven't checked to see if this is the latest manual, so use at your discretion.
Gary
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Re: Autopilot Debate
- Charles
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Re: Autopilot Debate
A. H. Powers ICS 2978
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Re: Autopilot Debate
Thanks,
- Charles
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Re: Autopilot Debate
- bernard nowlen
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Re: Autopilot Debate
One important thing to mention to you.... Whether it's for this autopilot issue or anything else avionics related, Mark Granger at Pro-Jet at JYO is outstanding. We have had a lot of work done by his shop, and are thrilled with his knowledge and ability. We had various autopilot / avionics issues and he has been able to zero in on each of them and get them fixed right away.
We were using Capital Aviation at HEF, and they were always decent folks with some good techs but Mark's crew got to the botom of our problems with much more precision.
-Steve
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Re: Autopilot Debate
- Charles
Charles Schefer- Posts: 563
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Re: Autopilot Debate
Gary
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Charles Schefer- Posts: 563
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Re: Autopilot Debate
The Piper Inspection Form calls for
Fuselage Group Item #25 to inspect security of A/P bridle cable clamps
Operational Inspection #20 Check Operation of Pitch Trim if installed
so unless you asked Heritage to check tension, I wouldn't expect it to be done.
Patricia Jayne (Pat) Keefer ICS 08899
PA-39 #10 Texas
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Re: Autopilot Debate
- Charles
Charles Schefer- Posts: 563
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Re: Autopilot Debate
Another tidbit was the inspection form i referenced. It is in the maintenance manual but they handed out a nice clean copy with more notes than I had previously seen. Always an education to browse it.
Patricia Jayne (Pat) Keefer ICS 08899
PA-39 #10 Texas
N3322G- ICS member
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Re: Autopilot Debate
Charles Schefer- Posts: 563
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Re: Autopilot Debate
It is off thread but i have to tell you I was very impressed by Cliff, his enormous Comanche knowledge and his humility. In turn, Cliff was quite excited to actually meet Tim Talley of Clifton and vice versa. Like Comanche owners get excited to meet other Comanche owners - so do the mechanics maintaining the same type aircraft. I heard them comparing tools after the session - I know they will be talking again.
Patricia Jayne (Pat) Keefer ICS 08899
PA-39 #10 Texas
N3322G- ICS member
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Re: Autopilot Debate
Cliff replied to my email this weekend and started off by saying that he had obtained new throttle rollers (for the micro switches - I'd been emailing with him on that too - think I'll still replace mine even though I think we've solved that for how) and as part of that Cliff said he'd been chatting with you on that topic. I told him you and I had been communicating as well on that and other topics... Funny
PS - back on thread - you are right... Cliff said they check the cables and only check tension if they suspect a problem. In the case of my plane they did not because cables were good.
Charles Schefer- Posts: 563
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Re: Autopilot Debate
I originally had your autopilot. Loved it, but i did build my avionics up piece meal, without a big picture in mind. Of course things are changing so quick, so who could?
But, the little trim window, top left that you say when you are in altitude hold, and the plane is level, but the trim indicator is pitched down slightly? I believe that is correct, IIRC, the twinky in flight gets on step and actually does a slight nose down.
I also think that is why a speed mod, or kind of mod, is the 3 degree aileron deflection, to take it out of drag.
steve
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Re: Autopilot Debate
On the autopilot - I believe the trim window (upper left of the AP unit) has nothing to do with the attitude of the aircraft. It has to do with the barometric pressure as sensed by the unit in comparison to the barometric pressure desired based on the altitude selector. As I understand it, all the trim window tells you is whether the autopilot believes it needs to initiate a climb or a descent from the current altitude (baro) to reach the pre-selected altitude (baro) on the altitude selector. This is based on barometric pressure not the pitch-up or down attitude of the aircraft in flight. So on mine, on the occasions where I can get it to hold altitude the trim is still saying that it wants to command a descent to reach the altitude I am already at when it should be level.
Anyway that's what I think based on my read of the book but I could be wrong - it wouldn't be the first time (just ask my wife )
- Charles
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