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Check your CS prop “low pitch” stops

We just performed this test on our 14. Took 2.25 turns in on fine pitch stop for our Hartzell CS prop to get below 2700 static. This is with an IO-390-EXP. I suspect Hartzell is setting these props up for 200HP, and the additional power needs more pitch.
 
I have been flying for a few years (RV-10 with a Hartzell Prop) and I have an RPM of 2580 at full power. When flying at full power and I adjust the Governor it takes some movement before there is a decrease in RPM - it is not immediate. Because of that I thought it was not Governor limited so I adjusted the low pitch stop by 1/2 of a turn with no change on a ground run. My next step is to adjust the Governor and leave the low pitch stop where it is for the moment and once I am able to increase RPM then cycle back to the low pitch stop adjustment. Does this make sense?
So your static RPM is 2580.. that’s ok, but you will get a little better acceleration at 2600 to 2650 static. The next question I have, are you able to hit 2700 rpm in climb? If not, then your governor needs to be raised. (You do have 1/8 to 1/4 inch before the knob hits the panel, right? You want the engine controls to fully hit their full range before they hit the panel)
I find that a lot of pilots or mechanics try to compensate for the overspeed surge by setting a lower governor setting to anticipate the surge, but that just makes the whole problem worse!
 
We just performed this test on our 14. Took 2.25 turns in on fine pitch stop for our Hartzell CS prop to get below 2700 static. This is with an IO-390-EXP. I suspect Hartzell is setting these props up for 200HP, and the additional power needs more pitch.
Yup.. I find it takes 2 and 1/3 turn to get it about right. Did you fly it yet? It’ll probably get to 2700 just about the time you lift off, and will glide better when you pull to idle..
 
I watched (and summarized for myself, list is below) Vic's video. My question is why does the Governor screw need to be backed out before adjusting the Propellor low pitch angle? It seems that if the target is 2,650-2,700 when adjusting the Propellor low pitch angle, that it can be made without making any changes to the Governor screw. Am I missing something?

Check Low Pitch Blade Stop:
Run to full throttle (flaps up and stick full back)
Move propellor control back, IF immediately decrease in RPM indicates governor is controlling max RPM and an adjustment is required

Adjust Low Pitch Blade Stop:
Cut safety wire on governor adjustment screw
Mark location of governor adjustment screw
Loosen governor adjustment screw lock nut
Back out governor adjustment screw to ensure governor isn't controlling the propellor
To set propellor low pitch blade angle:
Loosen Low Pitch Stop Jam Nut (clockwise to loosen)
Felt pin to mark starting location on hub and hex Low Pitch Stop thread
Make minor adjustment (each turn (IN) of the Low Pitch Stop thread is a 200RPM decrease)
Tighten Low Pitch Stop Jam Nut
Test run engine at full power
Repeat until full power produces 2,650 to 2,700 RPM

Adjust Governor Stop:
When breaking ground on take off should see 2,690 to 2,700 RPM
Loosen governor adjustment screw lock nut
Adjust governor adjustment screw
Tighten governor adjustment screw lock nut
Safety wire governor adjustment screw
Repeat 1-4 until 2,690 to 2,700 RPM is seen when breaking ground on take off)
 
You basically take the governor out of the loop. You want to make sure that the low pitch stop is adjusting your blade pitch so that at full power the prop "consumes" all the power without overspeeding. If you don´t back off the governor adjustment then it could be that the governor is doing it´s thing and push the blades off the low pitch stop at high power and so limits the RPM. The RPM surge is happening when the engine accepts power faster than the governor is reacting. The governor should take over during acceleration (only) on takeoff roll, now the angle of attack on the blades would decrease due to forward speed and so unloads the prop - now the governor is increasing blade pitch to absorb the power and give it a better bite.
 
As SuperCubDriver said, you take the controller out of the loop. But if you know your static RPM is already too high ( >= 2700 for most engines), then you can skip that step and go right to the fine pitch stop adjustment.
 
I have been flying for a few years (RV-10 with a Hartzell Prop) and I have an RPM of 2580 at full power. When flying at full power and I adjust the Governor it takes some movement before there is a decrease in RPM - it is not immediate. Because of that I thought it was not Governor limited so I adjusted the low pitch stop by 1/2 of a turn with no change on a ground run. My next step is to adjust the Governor and leave the low pitch stop where it is for the moment and once I am able to increase RPM then cycle back to the low pitch stop adjustment. Does this make sense?
Since governor adjustments should be tested in flight, I used another method. Before doing run up on ground to full throttle, loosen the jam nut of the governor just enough to allow you to turn the stop set screw out. (maybe 1/4 turn of jam nut). Then back out governor stop several turns. Enough to know for sure your governor is no longer slowing the RPM's down.

After that, do your ground run up at full throttle. Adjust the low pitch stop as necessary to get to 2650 RPM. Once that is achieved, THEN run the governor stop screw back down to the jam nut (this is where it started out) and tighten the jam nut. You will be VERY close to initial governor stop settings. Then go fly to test how close to 2,700 RPM you are getting. Adjust the set screw as needed. BTW, one 360* turn on governor set screw will equate to about 30 RPM's. It took me two test flights. 1st one showed governor was limiting RPM's at 2610 RPM. Turned set screw 3 full turns and re-tested in another flight. It was a perfect 2,700 RPM's on 2nd flight.
 
As SuperCubDriver said, you take the controller out of the loop. But if you know your static RPM is already too high ( >= 2700 for most engines), then you can skip that step and go right to the fine pitch stop adjustment.
Thanks, that is what I was thinking too.
 
I followed Vic’s procedures:

“Check Low Pitch Blade Stop:
Run to full throttle (flaps up and stick full back)
Move propellor control back, IF immediately decrease in RPM indicates governor is controlling max RPM and an adjustment is required”

My static was 2650. It took a couple of full turns of the governor control before any drop in RPM.

I assumed my governor was not limiting my prop per this instruction. Is this an incorrect assumption?
 
I wrote directions on how to to this last year when I adjusted mine. Let me know how these look.

PROPELLER GOVERNOR SETUP


  • Rotate the gov bezel to achieve full cable travel
  • Do a static ground run and adjust low angle stop to achieve a max RPM of 2550-2650
  • Fly the plane, initially taking off at less than max power to prevent overspeed. Check for max RPM on climb out, in cruise, and in a dive. If RPM exceeds 2700, adjust cockpit lever to hold 2700 and leave it there until on the ground.
  • Turn the low angle stop clockwise and keep testing until you can get 2700 max RPM in flight, and no more.
  • Adjust low angle stop to achieve the desired static RPM at takeoff, goal is to hit 2700 RPM as the tail lifts.
  • The governor arm throw may now need to be fine tuned to keep from slightly over-speeding. Fly the plane, and while in cruise adjust the lever to hit 2700 RPM and leave it there until on the ground. Now adjust the governor arm stop screw to match the prop lever position at the in-flight 2700 position.
  • Once adjusted, safety wire all bolts
 
I backed off the Governor Screw one turn and did a full power ground run and still am limited to 2580 RPM, I have previously turned the low pitch adjust a total of 3/4 of a turn without any change. Can the low pitch be that far off and I need to turn it more? Is there a limit before backing off will cause a problem? I tried to call Hartzell to get some guidance but it is after business hours.
 
I see so many airplanes that haven’t had the pitch stops adjusted properly. I know of one RV that overspeed to 3000 rpm’s on the initial flight because they did not set the pitch stops. I even mentioned it in my webinars this past week. Here’s a link to a video I made which should help you:


It’s also on page 113 in the Maintenance Handbook.



Vic
Vic, I bought an RV-9A some time ago with a CS prop. I’ve never had any issues with RPM (fortunately), but also never knew about the process of setting the low pitch limits. I just watched your video…it was very helpful. Many thanks for the continuing education for RV owners!
 
Is engine monitor data useful for evaluating the prop adjustment? Looking at the EDM data which is captured in 4 fractions of a second, I see the prop increase to above 2700 very quickly for a second then settles down to 2650 for the remainder of the ground roll. The aircraft is a -9A with a O-360, Hartzell prop and MT governor. Here is what the RPM graph looks like with 3 takeoffs and landings around the pattern.

2024-04-19 11_49_49-stream_0416_2055.csv - Excel.png
 
Is engine monitor data useful for evaluating the prop adjustment? Looking at the EDM data which is captured in 4 fractions of a second, I see the prop increase to above 2700 very quickly for a second then settles down to 2650 for the remainder of the ground roll. The aircraft is a -9A with a O-360, Hartzell prop and MT governor. Here is what the RPM graph looks like with 3 takeoffs and landings around the pattern.

View attachment 61016
Yes, it can be useful, though you'll want to zoom in a bit closer. What you've shown would tend to indicate that the low pitch stop is set low, and you're getting an overshoot before the governor catches it. The amount of overshoot will vary based on throttle application rate, and how low the stop is set.

A well set low pitch stop for an NA engine would tend to show max rpm less than governing, and a trend of increasing rpm with airspeed increase until reaching governing RPM.
 
Is engine monitor data useful for evaluating the prop adjustment? Looking at the EDM data which is captured in 4 fractions of a second, I see the prop increase to above 2700 very quickly for a second then settles down to 2650 for the remainder of the ground roll. The aircraft is a -9A with a O-360, Hartzell prop and MT governor. Here is what the RPM graph looks like with 3 takeoffs and landings around the pattern.

View attachment 61016
Looks like you can’t maintain 2700 rpm in the climb? Raise your governor setting be backing out the screw on the governor.. and adjusting the cable so the blue knob isn’t bottoming on the panel before the governor hits the stop. Then to get rid of the surge, adjust the propellor low pitch stops to provide 2650 static. If you can’t maintain 2700 in the climb, you are not using the full 180 hp..
 
Yes, it can be useful, though you'll want to zoom in a bit closer. What you've shown would tend to indicate that the low pitch stop is set low, and you're getting an overshoot before the governor catches it. The amount of overshoot will vary based on throttle application rate, and how low the stop is set.

A well set low pitch stop for an NA engine would tend to show max rpm less than governing, and a trend of increasing rpm with airspeed increase until reaching governing RPM.
Thanks for the feedback. Here is the data zoomed to 28 seconds of the takeoff role and climb. The RPM is on the left vertical axis and MP and fuel flow is on the right. It does look like the prop is overshooting and stays at 2670 in climb.

2024-04-19 21_48_31-stream_0416_2055.csv - Excel.png
 
Thanks for the feedback. Here is the data zoomed to 28 seconds of the takeoff role and climb. The RPM is on the left vertical axis and MP and fuel flow is on the right. It does look like the prop is overshooting and stays at 2670 in climb.

View attachment 61059
If you can’t dial in 2700 while you are climbing, you also need a governor adjustment
The governor adjustment screw is about 25 rpm per revolution. Just make sure your prop cable allows full forward
 
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I just did this on my 8 today. Night and day difference in the glide. Before, there was so much braking effect I was landing with the prop control back to keep from dropping like a rock and also not using full flaps. Now it glides like it should. Also, no surge on takeoff. I did as Tom suggested and it took exactly 2 1/3 turns and is now at 2600 static. As soon as it gets moving the RPM increases up to 2680 and the governor kicks in.

Had I had a governor failure before, I’m quite certain it would have gone 3100+ RPM and would not have climbed well at all. This took all of fifteen minutes or so to do.
 
If you are going to run your birds up to 2650 rpms, I would tie down the tailwheel really, really well. Seen a couple of airplanes on the nose from this sort of monkey motion. Makes for a bad day. If you think the nose draggers can't do it, I've seen that one too. So please be careful and responsible. Engine parts are getting harder and harder to find these days. Turn around for OH's could be 6 mos to 1 year. These planes are light with a lot of power so run ups need to be taken with extreme caution and good countermeasures in place.
 
If you are going to run your birds up to 2650 rpms, I would tie down the tailwheel really, really well. Seen a couple of airplanes on the nose from this sort of monkey motion. Makes for a bad day. If you think the nose draggers can't do it, I've seen that one too. So please be careful and responsible. Engine parts are getting harder and harder to find these days. Turn around for OH's could be 6 mos to 1 year. These planes are light with a lot of power so run ups need to be taken with extreme caution and good countermeasures in place.
Stick back, tail tied down, flaps up, and chocked.
My tail still lifted. FWIW

However, it would not have gone over on the nose as long as the stick is full back. I was expecting it, but still unnerving.
 
The guy that finished off my Rocket/F-1 EVO airplane was doing these run ups with no tail tie down and went right over on it's nose. In Germany of all places. I had to help him get his engine (that I built) back to the states for a rebuild. Ended up being a gorgeous airplane but man, what a downer day getting that call. I forgot to mention that torque loves to flip planes over as well. Big props, light airplanes. Seen a C206 with a brand new engine doing full power run ups on the ramp and then I heard this god awful noise from my hanger and peeked around the corner and it was on its nose/back. Back in the hanger it went for another 6 mos....... :(
 
Stick back, tail tied down, flaps up, and chocked.
My tail still lifted. FWIW

However, it would not have gone over on the nose as long as the stick is full back. I was expecting it, but still unnerving.
Flaps up, stick back, brakes held, if the tail starts to rise, release the brakes!! I would not chock it, because it removes an option for you to release the brakes. Heck, you could even do it on the runway and perform a takeoff with the check. If you don’t want to split your attention, either bring a passenger to video the tach or set up a GoPro aimed at the panel.
I thought some people were concerned about full power runup pulling on the tail tiedown.. I just do it in the runup area and if the plane starts to roll, I throttle back. Easy. Never had the tail lift with the stick back as long as the flaps are retracted.
 
I did a very small number of sustained full-power runups on the ground, pre-first-flight to ensure I was getting proper static RPM. Used heavy duty ratchet straps to tie both gear legs to the ground, as high up on the gear against the fuselage I could go. Since I have the -A model, I wrapped a third strap between the gear legs, to keep the main straps from sliding down the legs. Even strapped down like this, the thing bucked around like a horse. Pretty scary. I probably wouldn't do it again.

 
Yes, it can be useful, though you'll want to zoom in a bit closer. What you've shown would tend to indicate that the low pitch stop is set low, and you're getting an overshoot before the governor catches it. The amount of overshoot will vary based on throttle application rate, and how low the stop is set.

A well set low pitch stop for an NA engine would tend to show max rpm less than governing, and a trend of increasing rpm with airspeed increase until reaching governing RPM.
Bear with me as I get my mind around the low pitch stop setting and see if my logic is correct. I have a 0-360, Hartzell C2YK-1/7666A-4 Propeller and a MT P - 420 - 3 governor. On takeoff, my engine data shows RPM increasing to 2730 for 1 second then decreasing to 2650 - 2670 during the roll. I apply throttle slowly. The propeller never gets to 2700 RPM except for the brief surge. At rotation and during climb fuel flow settles in at 17 - 17.5 gals/hr and MP at 29. The data would indicate the low pitch stop is set too low preventing the prop from achieving full RPM or is the governor is limiting the prop RPM? How do I determine which one?

I hesitate to do a tied down static test for all the reasons mentioned in this thread.

The Hartzell manual says "The propeller low pitch stop is set at Hartzell Propeller Inc. in accordance with the aircraft TC or STC Holder's requirements and should not require any additional adjustment".

From the Hartzell manual " Turning the low pitch stop in will increase blade pitch to reduce RPM, and turning the low pitch stop out will lower blade pitch and increase RPM. The low pitch stop has 24 threads per inch. a Turning the low pitch stop 3/4 of a turn equals 0.030 inch (0.76 mm) of linear travel, and will change the blade pitch by approximately one degree. One degree of blade pitch will change the engine RPM by approximately 140-150 RPM. Turning the low pitch stop screw one revolution equals 0.042 inch (1.06 mm) of linear travel, and results in approximately 1.4 degree blade angle change. A 1.4 degree blade angle change results in an RPM increase/decrease of approximately 200 RPM."

If the low pitch stop is limiting max RPM, then I should turn the low pitch stop OUT one third of a turn to increase RPM by 40 RPM.

Does this logic sound correct?
 
Bear with me as I get my mind around the low pitch stop setting and see if my logic is correct. I have a 0-360, Hartzell C2YK-1/7666A-4 Propeller and a MT P - 420 - 3 governor. On takeoff, my engine data shows RPM increasing to 2730 for 1 second then decreasing to 2650 - 2670 during the roll. I apply throttle slowly. The propeller never gets to 2700 RPM except for the brief surge. At rotation and during climb fuel flow settles in at 17 - 17.5 gals/hr and MP at 29. The data would indicate the low pitch stop is set too low preventing the prop from achieving full RPM or is the governor is limiting the prop RPM? How do I determine which one?

Best way to understand the whole process is to watch the Vic Syracuse video on why/how to adjust the prop low pitch stop and the governor stop:

The Hartzell manual says "The propeller low pitch stop is set at Hartzell Propeller Inc. in accordance with the aircraft TC or STC Holder's requirements and should not require any additional adjustment".

EXCEPT....your aircraft doesn't have a TC, so there isn't any place to look up the required static rpm value. So Hartzell (or the prop shop that did the overhaul) has to take a best guess at where to set the prop low pitch stop. In my case, both the prop and the governor took some adjustment to get them to the max recommended rpm...both static and in flight.
 
Bear with me as I get my mind around the low pitch stop setting and see if my logic is correct. I have a 0-360, Hartzell C2YK-1/7666A-4 Propeller and a MT P - 420 - 3 governor. On takeoff, my engine data shows RPM increasing to 2730 for 1 second then decreasing to 2650 - 2670 during the roll. I apply throttle slowly. The propeller never gets to 2700 RPM except for the brief surge. At rotation and during climb fuel flow settles in at 17 - 17.5 gals/hr and MP at 29. The data would indicate the low pitch stop is set too low preventing the prop from achieving full RPM or is the governor is limiting the prop RPM? How do I determine which one?

I hesitate to do a tied down static test for all the reasons mentioned in this thread.

The Hartzell manual says "The propeller low pitch stop is set at Hartzell Propeller Inc. in accordance with the aircraft TC or STC Holder's requirements and should not require any additional adjustment".

From the Hartzell manual " Turning the low pitch stop in will increase blade pitch to reduce RPM, and turning the low pitch stop out will lower blade pitch and increase RPM. The low pitch stop has 24 threads per inch. a Turning the low pitch stop 3/4 of a turn equals 0.030 inch (0.76 mm) of linear travel, and will change the blade pitch by approximately one degree. One degree of blade pitch will change the engine RPM by approximately 140-150 RPM. Turning the low pitch stop screw one revolution equals 0.042 inch (1.06 mm) of linear travel, and results in approximately 1.4 degree blade angle change. A 1.4 degree blade angle change results in an RPM increase/decrease of approximately 200 RPM."

If the low pitch stop is limiting max RPM, then I should turn the low pitch stop OUT one third of a turn to increase RPM by 40 RPM.

Does this logic sound correct?
On initial power application, it takes a second for the oil pressure from the governor to ‘catch up’. During that time the mechanical fine pitch stop limits rpm. Yours is above 2700, suggesting you need to move that stop (adjust on the nose of the prop) slightly coarser, toward lower rpm. Once you’re going, the governor kicks in, and limits rpm to 2670, very slightly low. Adjust the governor stop for slightly more RPM. Re-do your test. Most prefer the mechanical stop to limit initial rpm to around 2650-2670, and the governor set to 2680 or so. That way on every takeoff you can verify the stop is set correctly (best glide in an engine out) and the governor works (it will kick in half way down the runway).
 
Bear with me as I get my mind around the low pitch stop setting and see if my logic is correct. I have a 0-360, Hartzell C2YK-1/7666A-4 Propeller and a MT P - 420 - 3 governor. On takeoff, my engine data shows RPM increasing to 2730 for 1 second then decreasing to 2650 - 2670 during the roll. I apply throttle slowly. The propeller never gets to 2700 RPM except for the brief surge. At rotation and during climb fuel flow settles in at 17 - 17.5 gals/hr and MP at 29. The data would indicate the low pitch stop is set too low preventing the prop from achieving full RPM or is the governor is limiting the prop RPM? How do I determine which one?
It sounds like you will want to adjust both the low pitch stop and the governor. The prop low pitch stop being too low is why you get the surge, you'd probably get more surge if you slammed the throttle. The governor being set too low is why the RPM is a bit low in climb, the low pitch stop isn't in play in this situation.
I hesitate to do a tied down static test for all the reasons mentioned in this thread.
Understandable. You can do this as a series of takeoffs as well, it will take more time; I'll outline this below.
The Hartzell manual says "The propeller low pitch stop is set at Hartzell Propeller Inc. in accordance with the aircraft TC or STC Holder's requirements and should not require any additional adjustment".
As mentioned, you have the ability, and responsibility, to determine this as the builder/integrator for your experimental aircraft.
From the Hartzell manual " Turning the low pitch stop in will increase blade pitch to reduce RPM, and turning the low pitch stop out will lower blade pitch and increase RPM. The low pitch stop has 24 threads per inch. a Turning the low pitch stop 3/4 of a turn equals 0.030 inch (0.76 mm) of linear travel, and will change the blade pitch by approximately one degree. One degree of blade pitch will change the engine RPM by approximately 140-150 RPM. Turning the low pitch stop screw one revolution equals 0.042 inch (1.06 mm) of linear travel, and results in approximately 1.4 degree blade angle change. A 1.4 degree blade angle change results in an RPM increase/decrease of approximately 200 RPM."

If the low pitch stop is limiting max RPM, then I should turn the low pitch stop OUT one third of a turn to increase RPM by 40 RPM.

Does this logic sound correct?
No. You want to turn the low pitch stop in, because it sounds like your pitch stop is set too low. Hard to know how much too low it is, because it's not currently limiting the RPM and the governor is catching it.

Given that you don't want to tie the aircraft down, or do this static on the brakes, here's what I would recommend:
  • Turn the low pitch stop in 1 full turn to increase the blade angle, thereby reducing the static RPM, following the procedures in the manual.
    • This should hopefully be enough adjustment that the blade angle is clearly limiting the RPM and keeping the governor out of the loop
    • Given that this may increase your takeoff distance somewhat, ensure you have adequate runway
      • Unlikely to be significant, but be safe
  • Perform a takeoff from a dead (not rolling) start. Advance the throttle quickly; it doesn't have to be a slam, but it should be authoritative and have full throttle before you've gained much airspeed.
  • Observe the RPM, and post flight use your EFIS to graph the change in RPM and the change in airspeed.
    • You should see a trend of increasing RPM with increasing airspeed until it reaches governing RPM at which point the governor takes over and the RPM should stay constant with increasing airspeed.
  • Be prepared for the aircraft to float more on approach and landing
  • Adjust the blade angle and repeat as necessary based on the previous results until you reach a setting you're satisfied with
Afterwards, you can adjust the governor per its instructions so you get 2700 RPM in climb. Given that it's currently a bit low, this means that the airspeed at which it latches will be a bit higher than your last low pitch adjustment had it occur.
 
You need to turn your low pitch stops CW IN, not out. It’s pretty obvious that your Governor is controlling your RPM right off the start.. that’s why you are getting a surge. Here’s what I would do if I were you.
Remove the spinner, marking its clocking location with a dot from a sharpie.
Put an Alen key in the center screw, loosen the 9/16 nut and while holding the nut, turn the Alen key clockwise 2 full turns. Retighten the 9/16 nut.
Put the spinner back on before you run it again. It’s possible (I’ve heard) that you could damage the little fillet pieces behind the blades if you run it without the spinner supporting them from swinging out.
Raise your governed RPM to 2700 by backing out the screw on your governor one turn per 30 RPM. You should achieve 2700 on climb out at 100 knots.
 
You need to turn your low pitch stops CW IN, not out. It’s pretty obvious that your Governor is controlling your RPM right off the start.. that’s why you are getting a surge. Here’s what I would do if I were you.
Remove the spinner, marking its clocking location with a dot from a sharpie.
Put an Alen key in the center screw, loosen the 9/16 nut and while holding the nut, turn the Alen key clockwise 2 full turns. Retighten the 9/16 nut.
Put the spinner back on before you run it again. It’s possible (I’ve heard) that you could damage the little fillet pieces behind the blades if you run it without the spinner supporting them from swinging out.
Raise your governed RPM to 2700 by backing out the screw on your governor one turn per 30 RPM. You should achieve 2700 on climb out at 100 knots.
Yep, this took several trials for me, even though Hartzell's docs tell you approximately how far to turn it in order to reduce RPM by a given amount. You have to loosen the nut, turn the pitch stop "a little", tighten the nut, and then go fly. Repeat until your RPM behaves correctly. It helped to mark on the spinner bulkhead with a magic marker how far I previously turned the stop, so I knew roughly how much more adjustment I needed.
 
Yep, this took several trials for me, even though Hartzell's docs tell you approximately how far to turn it in order to reduce RPM by a given amount. You have to loosen the nut, turn the pitch stop "a little", tighten the nut, and then go fly. Repeat until your RPM behaves correctly. It helped to mark on the spinner bulkhead with a magic marker how far I previously turned the stop, so I knew roughly how much more adjustment I needed.
That’s why I recommend 2 turns.. If you go only 90 degrees at a time, you’ll have to do it 8 or 9 tries. Most hartzell props need 2 and 1/3 turns.
 
This is timely because i've been wondering about doing the adjustment. On a WW 200RV there is nothing in the manual. I wondered if the WW factory just sets it right on a test stand and it doesn't need to be done. I had no idea how to adjust it. So, I appreciate the good pictures and description for the 200RV shown in this thread.

I don't get any surge on take-off, it comes right to 2700 and stays there. So I might be adjusted right already. But I do get substantial braking at idle with the prop, I fly downwind at 2200 rpm and abeam the numbers reduce to 1650 rpm, and that gives a really steep glide. So I think I'll do this test next fall. A shallower glide would be a good thing, especially with the Hartzell governor that won't control below 1500 rpm, so in case of power loss, I can't make the pitch very coarse to improve glide.
 
This is timely because i've been wondering about doing the adjustment. On a WW 200RV there is nothing in the manual. I wondered if the WW factory just sets it right on a test stand and it doesn't need to be done. I had no idea how to adjust it. So, I appreciate the good pictures and description for the 200RV shown in this thread.

I don't get any surge on take-off, it comes right to 2700 and stays there. So I might be adjusted right already. But I do get substantial braking at idle with the prop, I fly downwind at 2200 rpm and abeam the numbers reduce to 1650 rpm, and that gives a really steep glide. So I think I'll do this test next fall. A shallower glide would be a good thing, especially with the Hartzell governor that won't control below 1500 rpm, so in case of power loss, I can't make the pitch very coarse to improve glide.
If you get 2700 as soon as you firewall it, then it is NOT set correctly. You should be getting 2550-2650 statically. You say that you aren’t getting any surge, but could that be because you are applying power soft and gently (as you should) and that’s masking any surge? Try bringing it up to about 2000 then shoving the rest in quickly and see if there’s any surge, I bet it probably will.
 
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If you get 2700 as soon as you firewall it, then it is NOT set correctly. You should be getting 2550-2650 statically. You say that you aren’t getting any surge, but could that be because you are applying power soft and gently (as you should) and that’s masking any surge? Try bringing it up to about 2000 then shoving the rest in quickly and see if there’s any surge, I bet it problems will.
Nope, I can add power very fast and no overshoot.
I don't mind if the fine pitch stops limit to 2700 statically, and so would probably limit to 2750 or 2800 in flight. That is not much overspeed if the governor croaked. (heck, we turn them that fast on the race course). I'll do the test and report back.
 
Nope, I can add power very fast and no overshoot.
I don't mind if the fine pitch stops limit to 2700 statically, and so would probably limit to 2750 or 2800 in flight. That is not much overspeed if the governor croaked. (heck, we turn them that fast on the race course). I'll do the test and report back.
On my fixed pitch -4, I go from 2100 static to 2700+ at cruise. That’s a 600+ increase from zero knots to 170 knots. I’m pretty sure if a governor let go on any CS equipped RV in cruise, they are going to have a massive overspeed. I know about a -14 that had a governor failure on takeoff and his prop went to 3000+ at liftoff and had no thrust, so he chopped the throttle and landed straight ahead and melted his brake caliper O-rings. Thankfully, no fire. Since then, he sent the prop out for inspection, had the governor overhauled and corrected his low pitch stops.
 
On my fixed pitch -4, I go from 2100 static to 2700+ at cruise. That’s a 600+ increase from zero knots to 170 knots. I’m pretty sure if a governor let go on any CS equipped RV in cruise, they are going to have a massive overspeed. I know about a -14 that had a governor failure on takeoff and his prop went to 3000+ at liftoff and had no thrust, so he chopped the throttle and landed straight ahead and melted his brake caliper O-rings. Thankfully, no fire. Since then, he sent the prop out for inspection, had the governor overhauled and corrected his low pitch stops.
Yes you are right that if a governor failed at cruise it would be a serious overspeed. I don't think it would matter much if the pitch stops were set at 2600 or 2700 static rpm, its going to go well above 3000.
 
Actually going through this right now. Static is set at 2650. Flew first flight with new Harzell this morning and I can only get 2650 RPM on takeoff/cruise. Since I'm bottomed out on the governor stop right now, can I reposition the actuator arm on the shaft or do I have to unsafety the 6 retaining screws rotate the assembly a few degrees and re-safety? Is the assembly positions indented or friction lock by the retaining screws?
 

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