A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Piloting
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Less Gloom



 
 
Thread Tools Display Modes
  #21  
Old June 20th 07, 09:22 PM posted to rec.aviation.piloting
Peter Dohm
external usenet poster
 
Posts: 1,754
Default Less Gloom

"Jay Masino" wrote in message
. ..
Jay Honeck wrote:
Piper's "solutions" in the piston market have been so bloody obvious
to long-term Piper owners that we ALL wonder what their problem is.
They needed to do two things ten years ago:

- Add a pilot's-side door to the Cherokee line.


Since the current design is integral to the structural integrity of the
cockpit, adding a door would not be a trivial change. In fact, it
might not be possible at all, and retain the current type certificate.
Personally, I've never found myself wanting a door on that side.

- Build an O-540-powered Arrow

They have done neither, and have thus been getting their asses waxed
by Cirrus and Cessna.


Ah, but note that Cirrus uses a fixed gear design. Maybe there just
wasn't enough of a demand for a big engined Arrow.


Additionally, they could have made simple changes (like flush-rivets
and wing filets) to the airframe that would have at least given the
appearance of keeping up. Again, they have done precisely nothing,
beyond adding glass panels and upgrading interiors.


Again, I don't think switching to flush-rivets would be a "simple
change". There's definitely a difference in strength. Note that even
companies like Laminar Flow utilize fairings and... basically... Bondo
for their wing smoothing. If it was trivial to switch to flush rivets,
I suspect some enterprising company would already hold the STC for it.

Unfortunately, there are FAA imposed limitations to what you can change
and still comply with the existing type certificate. Or else you're
opening yourself up to certifying an entirely new airframe, and all the
associated engineering costs.

I agree that many little complanies will probably pop up to support our
Cherokees if Piper does stop producing parts.

--- Jay


I, for one, an not so sure about either the door or the flush rivets--which
I have been tole are actually stronger, although they are also more labor
intensive.

However, I believe that Jay Honeck's original gloom was correct, as was the
subsequent contributor who suggested that Piper might cease to manufacture
slow selling parts and simply sell the existing stocks as orders come in.
Automobile manufacturers do that all the time and the parts involved are
technically not safety related, although the case could be argued for some
parts like seat back positioning locks; but some really mundane things like
air conditioning thermostats and interior door handles can make it
difficult, or even impossible, to maintain a classic car in original
condition. OTOH, the automobile manufacturers continue to offer new
products which (sort of) fit the old market system.

Therefore, despite my preference for an American company, I am currently
betting on one of the foreign companies, such as Diamond, who include
trainers and entry level aircraft in their product mix, to take over Piper's
old place opposite Cessna.

Peter



  #22  
Old June 20th 07, 10:51 PM posted to rec.aviation.piloting
john smith[_2_]
external usenet poster
 
Posts: 393
Default Less Gloom

- Add a pilot's-side door to the Cherokee line.

Since the current design is integral to the structural integrity of the
cockpit, adding a door would not be a trivial change. In fact, it
might not be possible at all, and retain the current type certificate.
Personally, I've never found myself wanting a door on that side.


Piper knows how to build them (ie-Tomahawk).
It will add weight, as the framing required will require more AL.
Structurally, I don't see that there would be much difference. The
structure sits atop the wing. Will not the load be carried by monocoque
structure?

- Build an O-540-powered Arrow

They have done neither, and have thus been getting their asses waxed
by Cirrus and Cessna.


Ah, but note that Cirrus uses a fixed gear design. Maybe there just
wasn't enough of a demand for a big engined Arrow.


TIO-360C - 210 hp - 379 lbs
TIO-540W1A5 - 235 hp - 400 lbs

The Arrow is heavy enough without adding more weight to the nose.

Additionally, they could have made simple changes (like flush-rivets
and wing filets) to the airframe that would have at least given the
appearance of keeping up. Again, they have done precisely nothing,
beyond adding glass panels and upgrading interiors.


Look at how/where the fillets join the wing and fuselage.
While a fillet at the leading edge might pose a problem with removing
the cowl, the trailing edge fillet would interfere with the flap
operation.
The last redesign of the Cherokee series wing was 30-years ago when they
changed from the Hershey bar to the taper wing.
  #23  
Old June 21st 07, 05:54 AM posted to rec.aviation.piloting
Jay Honeck
external usenet poster
 
Posts: 3,573
Default Less Gloom

TIO-360C - 210 hp - 379 lbs
TIO-540W1A5 - 235 hp - 400 lbs

The Arrow is heavy enough without adding more weight to the nose.


Interestingly, I found out today that Piper built several O-540
powered Arrow prototypes, back in 1980 -- with 300 horsepower! (It
was supposed to be a trainer for some Banana Republic's air force.)

One is still in the registry -- registered to Piper under the
Experimental category.

Damn, I'll bet that thing moves right along!

Look at how/where the fillets join the wing and fuselage.
While a fillet at the leading edge might pose a problem with removing
the cowl, the trailing edge fillet would interfere with the flap
operation.


I've got the wing fillet mod on Atlas. It poses no problems with
either the cowling or the flaps.
--
Jay Honeck
Iowa City, IA
Pathfinder N56993
www.AlexisParkInn.com
"Your Aviation Destination"

  #24  
Old June 21st 07, 09:42 AM posted to rec.aviation.piloting
Thomas Borchert
external usenet poster
 
Posts: 1,749
Default Less Gloom

Peter,

Therefore, despite my preference for an American company, I am currently
betting on one of the foreign companies, such as Diamond, who include
trainers and entry level aircraft in their product mix, to take over Piper's
old place opposite Cessna.


They have, if you count sales of new airplanes. By that measure, Piper is dead
- and has been for quite a while.

--
Thomas Borchert (EDDH)

  #25  
Old June 21st 07, 04:40 PM posted to rec.aviation.piloting
Andrew Gideon
external usenet poster
 
Posts: 516
Default Less Gloom

On Wed, 20 Jun 2007 13:39:18 -0500, Jay Masino wrote:

Personally, I've never found myself wanting a door on that side.


I've never flown a Piper, but this is one of the issues that turns me off
of the line. Under normal circumstances, this means more work.
Following an emergency landing, that could be significant. I don't like
thinking about getting a kid out of the back seat away from the door.

But as I wrote, I've never tried it.

- Andrew

  #26  
Old June 21st 07, 09:07 PM posted to rec.aviation.piloting
xyzzy
external usenet poster
 
Posts: 193
Default Less Gloom

On Jun 21, 10:40 am, Andrew Gideon wrote:
On Wed, 20 Jun 2007 13:39:18 -0500, Jay Masino wrote:
Personally, I've never found myself wanting a door on that side.


I've never flown a Piper, but this is one of the issues that turns me off
of the line. Under normal circumstances, this means more work.
Following an emergency landing, that could be significant.


Or before an emergency landing, if "open the door so it doesn't get
jammed shut in the crash" is part of your pre-emergency landing
checklist. Not the time to need to reach across the cockpit to undo
two latches...

  #27  
Old June 22nd 07, 01:08 AM posted to rec.aviation.piloting
john smith
external usenet poster
 
Posts: 1,446
Default Less Gloom

Jay Honeck wrote:
Look at how/where the fillets join the wing and fuselage.
While a fillet at the leading edge might pose a problem with removing
the cowl, the trailing edge fillet would interfere with the flap
operation.


I've got the wing fillet mod on Atlas. It poses no problems with
either the cowling or the flaps.


I see a Knots 2U wing root fairing kit, but cannot a trailing edge
fairing kit.
To effectively do the job, you need both.
Peter Garrison had an excellent article on wing fairings in one of his
FLYING columns last year or the year before.
  #28  
Old June 23rd 07, 02:17 AM posted to rec.aviation.piloting
Gatt
external usenet poster
 
Posts: 123
Default Less Gloom


"Tom Guess" wrote in message
...
Jay Honeck wrote in news:1182317519.821816.6690
@q75g2000hsh.googlegroups.com:

Ah, spin control. Some day I want to have a "Chief Corporate
Spokesperson" in my company who will clarify and sanitize all the
stupid things *I* say... :-)


There aren't enough hours in the day or enough skilled communicators in
the
trade to handle that assignment.



*plonk*


 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
Gloom Jay Honeck Piloting 194 July 7th 07 06:12 AM


All times are GMT +1. The time now is 04:40 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.