Thanks. I understand the "timely; but smooth" application of appropriate 
control when fan up front stops (aka: panic).
Also substantiates the fact that the fan up front keeps the pilot cool as each 
time it has quit on me I start sweating immediately.
Dan C


On Jun 10, 2010, at 12:55 PM, William R. Bayne wrote:

> 
> Hi Dan,
> 
> Thanks for the kind words.  I have always regarded the Ercoupe as a fine 
> cross country machine if one understands its capabilities, limitations and 
> their own limitations.
> 
> A properly functioning mixture control is absolutely necessary to achieve 
> maximum possible engine performance and efficiency at higher altitudes.  The 
> procedure in the Ercoupe Instruction Manual works fine, except that I have 
> found benefit below 5,000' PA (where density altitude at 100ºF may be 
> 7,000').   
> 
> EGT and/or CHT instrumentation is inexpensive (I used a single-probe non-TSO 
> EGT).  One has access to much more important information with sensors on all 
> cylinders and a selector switch controlling a single indicator for nominal 
> additional investment.  I believe intelligent use of such by the pilot allow 
> him/her to best achieve that magic point where the "best power", "best 
> economy and "best airspeed" curves cross for a given coupe.  I believe an 
> engine so operated is more likely to achieve or exceed TBO because the 
> operator has the ability to be aware of, diagnose and remedy many common 
> engine problems before their adverse effects accumulate to the point of 
> failure.
> 
> With the relatively low power-to weight ratio of the Ercoupe (as compared to 
> most "modern" certificated designs) proper leaning can make the difference 
> between success and failure taking off and climbing out from high altitude 
> airports in the summer.  I should have mentioned that.
> 
> To illustrate the "difference" our mixture control makes, My wife and I once 
> returned from somewhere and decided to overfly our airport and continue to 
> one near the beach for something to eat.  That was sufficient "break" from 
> normal procedure that I forgot to return the mixture to Full Rich before or 
> during descent from "high lean cruise" position.  Engine performance seemed 
> normal until I reduced power for descent from pattern altitude to land and 
> the "fire went out" in the engine.  Even though the prop continued 
> "windmilling", that transition was definitely a "holy s**t" moment.
> 
> Of course the power smoothly returned upon my timely but smooth return of the 
> mixture control to "Full Rich" (without backfire), but it was a very clear 
> reminder of the fact that a properly operating Stromberg mixture control is 
> effective to the purpose intended and not to be ignored.  I have also never 
> forgotten to enrich in descent again ;<)
> 
> Regards,
> 
> William R. Bayne
> .____|-(o)-|____.
> (Copyright 2010)
> 
> -- 
> 
> On Jun 10, 2010, at 11:43, Caliendo Dan wrote:
> 
>> Good discussion, William, and I agree. My experience with mountain flying 
>> has all been in fuel injected engines
>> and I'm wondering if you can use the leaning the mixture (which gives you 
>> significantly more power at high density
>> altitude) in an Ercoupe with a carburetor. Seems the mixture leaning is a 
>> pretty slow process in my Ercoupe; but I've
>> not used it at altitude (shucks, have had the coupe for over 2 years and 
>> haven't been above 3,000 ft yet : >).
>> Dan C
>> 
>> 
>> On Jun 9, 2010, at 10:45 PM, William R. Bayne wrote:
>> 
>>> 
>>> Hi Dennis,
>>> 
>>> You don't say what prop you have, but I will assume it is the correct size 
>>> metal McCauley of "standard" pitch.
>>> 
>>> If so, several considerations.  You will have slightly better performance 
>>> (for a given temperature) than the 415-D figures (1) because you will be 80 
>>> lbs. lighter, because the metal prop has slightly better efficiency (which 
>>> slightly increases the resulting rate of climb) and because I am consulting 
>>> the take-off figures in the 415-E Flight Manual (because you have the 85hp  
>>> engine instead of the 75hp in the D).
>>> 
>>> I have crossed the Continental Divide several times each way flying from 
>>> Phoenix via Lordsburg (the southern route) or to Albuquerque (the northern 
>>> route.  Fly the mountains early, because afternoon thunderstorms build fast 
>>> and often in the afternoon heat...not a good time to be there, aside from 
>>> the turbulence.  
>>> 
>>> This was infinitely more challenging utilizing VOR and pilotage than GPS 
>>> today.  VOR coverage below 10,000' in that area is poor, so one had to 
>>> achieve accurate enough results with pilotage (despite iron deposits 
>>> influencing the compass) after leaving Phoenix VOR reception to intersect 
>>> the rather limited "circle of VOR coverage" of the few VORs en route to 
>>> Albuquerque.
>>> 
>>> With a normally healthy engine, the "book" (interpolated) suggests an E 
>>> model with a wood prop at 1400 lbs. and 100ºF will require  4513' of runway 
>>> before liftoff.  That isn't the "whole story", though.  You can lift off in 
>>> "ground effect" on a given day (few air masses are exactly the same) and 
>>> find the plane won't climb and loses altitude in the gentlest bank.  That 
>>> can put you in deep yogurt real quick, so carefully review conditions in 
>>> depth before deciding to take off and never attempt a takeoff in which 
>>> success is at all doubtful.  This is easier said than done.
>>> 
>>> Again, with reference to 415-E data, the chart interpoation suggest a climb 
>>> rate at 4500' PA and 100ºF of 282 FPM at best rate of climb.  I am NOT 
>>> bragging in revealing dodging a church steeple well away from the Lordsburg 
>>> airport because our rate of climb had essentially ceased at 90 mph and 100' 
>>> off the ground.  Instead of establishing my normal "cruise-climb" I should 
>>> have set the plane up for best rate of climb to get higher under those 
>>> conditions.  Another time, departing Albuquerque near noon I found terrain 
>>> rising more rapidly than we were in three possible directions.  A "trick" I 
>>> discovered that day is to look for buzzards and/or cumulus clouds.  These 
>>> mark rising air, and the boost in climb is free except for the time off 
>>> course and circling upward in a stationary thermal.  
>>> 
>>> It is not unusual to find an inversion over an airport, in which the air 
>>> temperature actually rises as you climb.  Such a "cap" of air is what traps 
>>> smog in the Los Angeles, CA basin.  Once through that "cap" with the 
>>> superheated air nearer the ground (which typically has less "lift" in it) 
>>> below you, climb performance is much better.  
>>> 
>>> Where there is rising air there is also sinking air.  Always approach 
>>> higher ground at a 45º angle so you can turn away with only a 90º turn 
>>> should you encounter a downdraft there to maintain good terrain clearance.  
>>> We had to search up and down a high mesa on our course to find more lift, 
>>> but eventually climbed to over over 10,000' that day en route to Dalhart, 
>>> TX and East.
>>> 
>>> It would suggest you plan your trip to arrive at the airports you speak of 
>>> late in the day and depart in the early morning.  That makes a big 
>>> difference because high altitude airports usually enjoy low humidity and 
>>> that gives you 60ºF early morning takeoff conditions before an afternoon 
>>> high of 100ºF.  Alternately, depart with just enough fuel to get to a lower 
>>> airport before filling the tanks.  If you calibrate your tanks, keep 
>>> records of your fuel consumption, and monitor it several times each leg 
>>> this is quite predictable and safe.  In good VFR conditions, half the nose 
>>> tank's usable fuel is plenty of reserve (unless you are simultaneously 
>>> learning use of the GPS on a given flight  ;<)
>>> 
>>> Taking off from lower but hotter airports in Arizona in the summer, I have 
>>> taken of with full fuel and left my wife on the ground to see how much 
>>> "lift" is in the air mass present.  Unfortunately after returning to get 
>>> her, the engine is thoroughly "heat soaked" and oil temperatures can get a 
>>> bit dicey before reaching cooler temperatures aloft.  Fortunately today's 
>>> oils continue to lubricate adequately at temperatures above redlines still 
>>> recommended for our little Continentals.
>>> 
>>> There are options available to the proficient and knowledgeable pilot that 
>>> can greatly increase the utility of relatively low performance aircraft.  
>>> At some point experience significantly reduces the big bag of luck that new 
>>> pilots dip into frequently. But knowledge and quick thinking is the best 
>>> "insurance". These are the words of a Private Pilot, not a CFI or 
>>> professional aviator. Results may vary.
>>> 
>>> Regards,
>>> 
>>> William R. Bayne
>>> .____|-(o)-|____.
>>> (Copyright 2010)
>>> 
>>> -- 
>>> 
>>> On Jun 9, 2010, at 13:03, Dennis wrote:
>>> 
>>>> My brother & I are planning a cross country trip (with my 85hp 415C) which 
>>>> will require one or two take offs at airports with altitudes 4000 to 4500 
>>>> feet and temperatures up to 100 degrees F.  Density altitude probably at 
>>>> about 6500 feet or possibly higher.  Runways are 6000 feet long and the 
>>>> Ercoupe will be loaded to maximum at 1320 pounds.  
>>>> 
>>>> Considering all the above information, the 415-D flight manual charts 
>>>> (pages 10 and 11) show that it will take 3950 feet to take off and we will 
>>>> climb at 330 feet per minute.  My problem is that I have never done this.  
>>>> My normal take off roll when I am alone and it's 70 degrees F. takes me 
>>>> 1000 feet or less.  What I really need is someone who is very experienced 
>>>> in these long take off rolls to help convince me that the Ercoupe will 
>>>> really take off at 3950 feet and then climb at 330 feet per minute.  Of 
>>>> course, if it isn't at take off speed at 3950 feet of the 6000 foot 
>>>> runway, I still have time to abort the take off.
>>>> 
>>>> I will really appreciate any information or advice you can provide.
>>>> Thanks, Dennis Hatfield
>>>> 
>>>> 
>>>> 
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