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Accident Prevention

 
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sdthatcher



Joined: 13 Mar 2008
Posts: 91
Location: Port Saint Lucie

PostPosted: Thu Mar 20, 2008 6:05 am    Post subject: Accident Prevention Reply with quote

Just for the record, be sure when making your 45 to downwind on a gusty day
you don't try the bank and yank approach (60-70 degree hard bank maintaining
level flight) then level out abeam the numbers on downwind. You just might
find that you've exceeded 6 g's in your aircraft as you watch your wings
embrace your cabin!

Scott Thatcher, Palm Beach Gardens, FL
601XL with Corvair, Registered as E-LSA
N601EL


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Scott Thatcher, Port Saint Lucie, FL
601XL with Corvair, Registered as E-LSA
N601EL, EAA203 140 hours and not flying currently.
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cscsail(at)gmavt.net
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PostPosted: Thu Mar 20, 2008 8:13 am    Post subject: Accident Prevention Reply with quote

I'm not a 601 driver, but I would thing that the approach speed would we
below the maneuvering speed (Va). Below this speed the wing can not produce
enough lift to overstress the aircraft.
Gordon

---


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david_a_g_johnson(at)btin
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PostPosted: Thu Mar 20, 2008 9:03 am    Post subject: Accident Prevention Reply with quote

This is not quite true - a rapid reversal of the controls can over-stress
the airframe. This is thought to have caused the crash of a PA28 near my
home. A large section of one wing broke off (about 1/3rd. I think)

You can read the full AAIB report at:-

http://www.aaib.dft.gov.uk/cms_resources/dft_avsafety_pdf_025533.pdf

Dave Johnson
do not archive

---


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notsew_evets(at)frontiern
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PostPosted: Thu Mar 20, 2008 9:50 am    Post subject: Accident Prevention Reply with quote

Amazing. I owned a Cherokee and "thought" is was built like a tank.. Guess
not.
SW
---


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ernieth(at)gmail.com
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PostPosted: Thu Mar 20, 2008 10:15 am    Post subject: Accident Prevention Reply with quote

Thanks,
Very interesting.

It does they state " the aircraft was flying at or just below VA of 118kt",


Looks like Va, is more of a guideline than a grantee in some cases.

The recommedation.....

training syllabus for private pilot should be reviewed...

e.

do not archive

On Thu, Mar 20, 2008 at 9:59 AM, Dave Johnson <david_a_g_johnson(at)btinternet.com (david_a_g_johnson(at)btinternet.com)> wrote:
[quote]--> Zenith-List message posted by: "Dave Johnson" <david_a_g_johnson(at)btinternet.com (david_a_g_johnson(at)btinternet.com)>

This is not quite true - a rapid reversal of the controls can over-stress
the airframe. This is thought to have caused the crash of a PA28 near my
home. A large section of one wing broke off (about 1/3rd. I think)

You can read the full AAIB report at:-

http://www.aaib.dft.gov.uk/cms_resources/dft_avsafety_pdf_025533.pdf

Dave Johnson
do not archive

---


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rtdin



Joined: 16 Mar 2008
Posts: 46
Location: Florida panhandle

PostPosted: Thu Mar 20, 2008 12:04 pm    Post subject: Accident Prevention Reply with quote

Lets slow down here and take a breath. First, these bank angles at pattern altitude would be seriously bad judgment. Second, If the pilot's wife were on board, he might get slapped real hard. What we do know is that an aircraft with the wing and power loading of a CH601XL would barely be able maintain altitude beyond 60 degrees of bank. A bank angle of 40 Deg = 1.3 G, 60 Deg = 2 G, 70 Deg = about 3.2.
http://pilotsweb.com/principle/load.htm We always slow down in the pattern, do we not?
The more likely scenario would be that a greenhorn would let the ball slip out, stall and not recognize the spin entry. Few pilots have training in spins any more. Even CFI candidates don't have to demonstrate them anymore. A log book entry will do. BTW, some bank angles of more that 60 degrees can be done one handed while pouring a drink with the other hand. Watch this. http://youtube.com/watch?v=Xp2Uc9XvmjY Slightly more than 1 G. Bob Hoover has always been my hero.
Bob Dingley
XL/Lyc Do not archive
**************
Create a Home Theater Like the Pros. Watch the video on AOL Home.
(http://home.aol.com/diy/home-improvement-eric-stromer?video=15?ncid=aolhom00030000000001) [quote][b]


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bryanmmartin



Joined: 10 Jan 2006
Posts: 1018

PostPosted: Thu Mar 20, 2008 12:53 pm    Post subject: Accident Prevention Reply with quote

A 6G coordinated turn at a constant altitude would require slightly
more than 80 Degrees of bank. It takes 76 degrees of bank to exceed
the flight load limit of 4Gs.

Quote:


>

Just for the record, be sure when making your 45 to downwind on a
gusty day you don't try the bank and yank approach (60-70 degree
hard bank maintaining level flight) then level out abeam the numbers
on downwind. You just might find that you've exceeded 6 g's in your
aircraft as you watch your wings embrace your cabin!



--
Bryan Martin
N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.


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--
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
do not archive.
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bryanmmartin



Joined: 10 Jan 2006
Posts: 1018

PostPosted: Thu Mar 20, 2008 1:05 pm    Post subject: Accident Prevention Reply with quote

The published Va for most aircraft is only valid at the aircraft's
gross weight. You can exceed the airplane's flight load limit at lower
weights at the published Va without stalling the airplane. At the
lower weight, you probably won't over-stress the wing root attachment
but you may over-stress other parts of the structure. Va should be
decreased for weights less than gross weight.

On Mar 20, 2008, at 1:55 PM, ernie wrote:

Quote:
Thanks,
Very interesting.

It does they state " the aircraft was flying at or just below VA of
118kt",
Looks like Va, is more of a guideline than a grantee in some cases.

The recommedation.....

training syllabus for private pilot should be
reviewed...



--
Bryan Martin
N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.


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_________________
--
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
do not archive.
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ashontz



Joined: 27 Dec 2006
Posts: 723

PostPosted: Thu Mar 20, 2008 1:41 pm    Post subject: Re: Accident Prevention Reply with quote

Maybe this is the real problem. The 'in the pattern' accidents were the one's that disturbed me the most.

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n801bh(at)netzero.com
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PostPosted: Thu Mar 20, 2008 3:24 pm    Post subject: Accident Prevention Reply with quote

I saw Bob Hoover fly when I lived in Fla back in the 80's.. That video you gave a link to was a testimony to how damn good Bob Hoover really is. If you look up the word smooth in the dictionary there will be a color picture of him under the defination...
Ben.
do not archive

t get slapped real hard. What we do know is that an aircraft with the wing and power loading of a CH601XL would barely be able maintain altitude beyond 60 degrees of bank. A bank angle of 40 Deg = 1.3 G, 60 Deg = 2 G, 70 Deg = about 3.2.
http://pilotsweb.com/principle/load.htm We always slow down in the pattern, do we not?
The more likely scenario would be that a greenhorn would let the ball slip out, stall and not recognize the spin entry. Few pilots have training in spins any more. Even CFI candidates don't have to demonstrate them anymore. A log book entry will do. BTW, some bank angles of more that 60 degrees can be done one handed while pouring a drink with the other hand. Watch this. http://youtube.com/watch?v=Xp2Uc9XvmjY Slightly more than 1 G. Bob Hoover has always been my hero.
Bob Dingley
XL/Lyc Do not archive
**************
Create a Home Theater Like the Pros. Watch the video on AOL Home.
(http://home.aol.com/diy/home-improvement-eric-stromer?video=15?ncid=aolhom00030000000001)
Quote:


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Tim Juhl



Joined: 21 Mar 2006
Posts: 488
Location: "Thumb" of Michigan

PostPosted: Thu Mar 20, 2008 3:33 pm    Post subject: Re: Accident Prevention Reply with quote

I've been flying 33 years and doubt if I've ever pulled much more than 3 g's in any maneuvers, including steep turns. This is true even with all the students I've flown with. If it was routine to pull that many g's we'd have broken airplanes all over the place.

Tim

do not archive


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______________
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Champ L16A flying
Zodiac XL - Jabiru 3300A
Almost done! It'll fly in spring!
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PostPosted: Thu Mar 20, 2008 4:09 pm    Post subject: Accident Prevention Reply with quote

Yep
I assumed this was calc , they did finite analyis on the wingwhy would
the miss that

Do not archive

On 3/20/08, Bryan Martin <bryanmmartin(at)comcast.net> wrote:
Quote:


The published Va for most aircraft is only valid at the aircraft's
gross weight. You can exceed the airplane's flight load limit at lower
weights at the published Va without stalling the airplane. At the
lower weight, you probably won't over-stress the wing root attachment
but you may over-stress other parts of the structure. Va should be
decreased for weights less than gross weight.

On Mar 20, 2008, at 1:55 PM, ernie wrote:

> Thanks,
> Very interesting.
>
> It does they state " the aircraft was flying at or just below VA of
> 118kt",
>
>
> Looks like Va, is more of a guideline than a grantee in some cases.
>
> The recommedation.....
>
> training syllabus for private pilot should be
> reviewed...
>
--
Bryan Martin
N61BM, CH 601 XL,
RAM Subaru, Stratus redrive.
do not archive.



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planecrazydld(at)yahoo.co
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PostPosted: Thu Mar 20, 2008 5:32 pm    Post subject: Accident Prevention Reply with quote

very common thought - but untrue. It is theoretically impossible to overstress the airframe structure by deflection of the controls to limit at or below maneuvering speed. This does not address gust loading, vertical wind shear, and other transients that are frequently encountered during flight.

Gordon <cscsail(at)gmavt.net> wrote:[quote] --> Zenith-List message posted by: "Gordon"

I'm not a 601 driver, but I would thing that the approach speed would we
below the maneuvering speed (Va). Below this speed the wing can not produce
enough lift to overstress the aircraft.
Gordon

---


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PostPosted: Thu Mar 20, 2008 6:14 pm    Post subject: Accident Prevention Reply with quote

Dave
This report did a detailed investgation on how a aircraft could be
damage at or below va with the right/wrong control inputs


On 3/20/08, David Downey <planecrazydld(at)yahoo.com> wrote:
[quote] very common thought - but untrue. It is theoretically impossible to
overstress the airframe structure by deflection of the controls to limit at
or below maneuvering speed. This does not address gust loading, vertical
wind shear, and other transients that are frequently encountered during
flight.

Gordon <cscsail(at)gmavt.net> wrote:
"Gordon"

I'm not a 601 driver, but I would thing that the approach speed would we
below the maneuvering speed (Va). Below this speed the wing can not produce
enough lift to overstress the aircraft.
Gordon

---


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dredmoody(at)cox.net
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PostPosted: Fri Mar 21, 2008 7:27 am    Post subject: Accident Prevention Reply with quote

I second that motion Tim. I have flown several times with friends in their aerobatic planes (Citabria Decathalon, Christen Eagle, Steen Skybolt, Extra 300) and have found that the 4G entry / exit from an inside loop is way, way more G load than I would ever confidently put my 601XL through (once it is finished that is). Other pilots mileage may vary but nobody needs to worry about me overstressing my XL. Hell, Bill of Georgia flies even lighter touch than me so take us both off the worry list.

Dred
[quote][b]


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sdthatcher



Joined: 13 Mar 2008
Posts: 91
Location: Port Saint Lucie

PostPosted: Fri Mar 21, 2008 3:21 pm    Post subject: Accident Prevention Reply with quote

OK Jerry, I admit that being careful doesn't sound fun but if you're 67, you
have obviously either been lucky or not as bold as you think. Doing rolls,
immelmans, etc., are not yank and bank flying! Imagine decending to pattern
altitude... the speed slowly builds up while you're watching one aircraft
turn x-wind to join the downwind and another overflying the field. You bank
hard right at 60-70 degrees to miss the aircraft overflying the field (to
get an instrument rating I believe you've got to hold a 720, 60 degree bank
without losing altitude, so this isn't too hard on the plane). But Winds
are gusting to 25 kts and suddenly you go vertical and pull back on the
stick simultaneously while never noticing that you had exceeded maneuvering
speed. Easily a 4-6 g maneuver. All I'm saying is that it can happen. Not
often. Maybe never. But think about it when you are in the pattern.

Another common error was mentioned previously regarding stalling the
aircraft in a tight turn. I was doing some spot landings in a Mooney and
while tuning base to final (and decending), I banked it hard over to at
least 70 degrees. Engine was at idle. I knew I was going to hit the spot on
the runway, so I leveled off... except the plane would not level off! It
continued the left turn and those famous words, "Oh S..t" were stated
loudly. The wing had stalled and the controls were useless. I added power,
nosed over (all this within about 50 feet of the ground) and the plane
immdiately leveled off, I dropped the gear and missed the mark entirely!
Moral of the story. Never make hard turns in the pattern or anywhere else
unless absolutely necessary

DO NOT ARCHIVE

Scott Thatcher, Palm Beach Gardens, FL
601XL with Corvair, Registered as E-LSA
N601EL

Message from Jerry Hey

<<Surviving and living are not at all the same. Putting around making
gentle turns may extend your life but it is not living. Yanking and
banking are the important fun part of flying, much more so than
sitting still in the left seat, afraid to twitch. I love to fly.
One of my old friends, flying a Tailwind, can't go from point to point
without tossing in a roll ever so often. One night, in pitch black,
we did roll after roll as we cork screwed along, only the lights on
the ground to pronounce right side up and our laughter filling the
cabin. That was living! I would not have a plane that cannot
handle a little fun. Jerry age 67 (701 scratch )>>


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_________________
Scott Thatcher, Port Saint Lucie, FL
601XL with Corvair, Registered as E-LSA
N601EL, EAA203 140 hours and not flying currently.
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