This has been nagging at me, also.  But, for a different reason.  It seems
to me that if you can actually turn downwind in such a way as to lose
airspeed, causing the nose to pitch down, then you have, by definition,
stalled the aircraft.
 
We had an accident report back in the 70's concluding that a T-28 had done
that.  We were all cautioned to be wary of downwind turns in the pattern.
 
But...I am not convinced that it is even possible to make such a turn and
lose that much airspeed.
 
I am able to be convinced, however, if somebody can confirm or explain it.
 
Dave Winters
2797H

-----Original Message-----
From: [email protected] [mailto:[EMAIL PROTECTED] On
Behalf Of robertbartunek
Sent: Wednesday, June 18, 2008 8:05 AM
To: [email protected]
Subject: [ercoupe-tech] Re: July Flying Mag



The following quote from the article puzzles me.
"Pilots thought nothing of flying Ercoupes very slowly. When they 
would, say during a forced landing fly from a headwind condition to a 
no wind condition,the airplane would pitch nose down to try to 
maintain airspeed."
How do you get the nose to "pitch down" in an Ercoupe? With full aft 
elevator control input, mine (a CD) just mushes straight ahead with a 
slightly positive deck angle at about 300 fpm at about 47 mph IAS. 
Bart

--- In ercoupe-tech@ <mailto:ercoupe-tech%40yahoogroups.com>
yahoogroups.com, [EMAIL PROTECTED] wrote:
>
> Ed: Thanks for your comments. The author of the article made a 
similar 
> observation: " The bad Ercoupe record had more to do with pilots 
thinking it was 
> 'safe' than it did with the airplane itself" He goes on to 
say: "Pilots thought 
> nothing of flying Ercoupes very slowly. When they would, say 
during a 
> forced landing fly from a headwind condition to a no wind 
condition,the airplane 
> would pitch nose down to try to maintain airspeed. And it would hit 
the ground 
> nose down,just as if it had stalled. It couldn't stall because of 
restricted 
> up-elevator travel but it could sure hit the ground hard and nose 
down." He 
> concludes that the high vertical loading of such an impact is the 
reason low 
> speed loss of control accidents have a much higher incidence of 
injury and 
> death. My own experience suggests that even before pitching nose 
down in a 
> stall/mush condition the sink rate itself could be the cause of 
serious injury or 
> death if sufficient airspeed is not maintained in a forced landing.
> I think the risk of being trapped upside down is inherent in most 
all 
> tricycle gear low wing aircraft. I'm surprised that there is 
little discussion of 
> how to mitigate that risk. My engine out emergency checklist 
includes 
> lowering the side windows but I'm not sure if I could get out even 
with them open. I 
> have seen articles about practicing exit from a submerged aircraft 
but never 
> about escape techniques on dry land. 
> 
> Jim Graham
> 
> 
> 
> **************Gas prices getting you down? Search AOL Autos for 
> fuel-efficient used cars. (http://autos. <http://autos.aol.com/used?>
aol.com/used?
ncid=aolaut00050000000007)
>



 

Reply via email to