It is sometimes necessary to dig further into apparently "simple  
truths" to reach maximum enlightenment  ;<)

When additional horsepower increases elevator effectiveness,  
precisely how could trim authority not concurrently and similarly  
increase?  After all, what we are talking about is an increase in  
airflow over the "...angle the elevator makes with the elevator chord  
line (see Ercoupe Service Memorandum No. 25)...".

If the efficiency of either type trim system is increased, it would  
logically follow that less "trim input" under power is necessary for  
a given result.  There is NO data of which I am aware that  
establishes any power-on difference in actual trim effectiveness that  
even suggests the separate tab design is sufficiently more effective  
than the earlier "trimmed elevator" that a change from one system to  
the other is logical or desirable.

We also need to consider the actual difference in horsepower  
available in flight between the 75 hp and the 85 hp configurations.    
Ercoupe Service Memorandum No. 37 and 37A present propeller  
performance data between the standard wood Sensenich 74FC48T and the  
McCauley 1-A-90 that is most common today.

"A typical production Ercoupe was used loaded to a gross weight of  
1260 lb. for all of the tests.  The instruments were calibrated, and  
the air conditions were very close to standard for the duration of  
the tests."  The "typical production Ercoupe had 75 hp.  The"74"  
Sensenich was turning at 2600 R.P.M. at a maximum speed of 121 MPH.   
The 73" McCauley was turning at 2500 R.P.M. at a maximum speed of 121  
MPH.

If one goes to the Continental Owners Manual and the Altitude  
Performance Curve for (both) the C75 & C85, it is quite clear that at  
2600 R.P.M. more than 85 hp is being produced by the 75 hp engine.   
At 2500 R.P.M. approximately 83 hp is being produced.  There would  
likely be a 2 hp variation in the maximum power output between  
production engines!  This is the first indication that the 85 hp  
"improvement" in performance is a myth.

Fred Weick wrote the book on propeller design in the thirties, and I  
happen to own the copy that was once in the Technical Information  
Center of the Lockheed-California Company in Burbank, California.  It  
explains in detail why the longer 73" and 74" fixed pitch props are  
MORE EFFICIENT than the shorter ones specified in the Type  
Certificate for the C85.

Ercoupers today mostly have the shorter props and 85 hp  
modifications.  It is understandable that they are reluctant to  
believe original ERCO performance figures, because to do so they  
would have to accept that the reduced performance of their present  
configuration is the result of following Continental's requirements  
in order to modify the 75 hp Continental to an "official" 85 hp.   
They have been persuaded give up the steak for the "sizzle"!

The ERCO discussions of the trim systems largely concern themselves  
with glide performance and not with full power performance.

Don's trim system is discussed at length in Ercoupe Service  
Memorandum No. 19 of 4/26/46 (date from ESM No. 38).  It says:   
"...the natural trim speed in a glide with the controls and trim  
device disconnected is now approximately 70 mph, a speed at which the  
airplane can be maneuvered to a satisfactory landing by throttle  
alone".  "The use of a movable trim tab will not affect the feel of  
the controls".  "Flight check should show a glide speed of 68-70 mph  
with trim unit set at "nose up".

Ercoupe Service Memorandum No. 25  pertains to the "new" trim system  
with the separate trim tab installed on Ercoupes Serial Nos. 1623 and  
up with the 75 hp engine.  It states:  "...the angle the elevator  
makes with the elevator chord line trims the ship for a glide, power  
off, at 58 mph and a 55 mph climb with power on."

Accordingly, it would appear that any difference in "trim authority"  
at full power would be of little, if any, significance in normal  
use.  At full power, it is "nose down" trim that is needed.  Every  
trim system ever fitted had more "nose down" trim available than  
could be effectively used.

Regards,

William R. Bayne
.         |-(o)-|         .
(Copyright 2010)

-- 

On Aug 29, 2010, at 20:11, John Cooper wrote:

>   On 8/29/2010 5:19 PM, Donald wrote:
>> I suppose someone smarter than I decided upon it, but I fail to see
>> why the additional 10 hp requires a trim tab. I sure have not missed
>> having one so far, and am reluctant to install one..
> Additional Horsepower increases elevator effectiveness and thus  
> requires
> more trim authority to accomplish the same task.
>
> -- 
> John
> Skyport East
> www.skyportservices.net

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