http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular
.nsf/1ab39b4ed563b08985256a35006d56af/e533bb05389c90e486256a54006e47b2/$FILE
/Chapter%201-8.pdf
If it wraps cut and paste it as required to make a link. It gives
general guidelines for installing tow hooks on tailwheel and tricyle
gear airplanes.
He also forwarded a document file which described Cessna's testing of
100 series aircraft for towing and how nearly all structurally handle
1,200 lbs x 150% at various tow angles. This document is probably
available on letterhead from Cessna's Structural Department. Allow at
least a couple of weeks if you need a copy. Mr. Pate also sent photos
of an installation he saw in Texas.
The best information he sent were some unofficial copies of the
Javelin Aircraft STC for the tow-hook installation. He said that David
Blanton Sr. who passed away a few years ago donated the tow-hook STC
to the SSA. The STC drawing shows how to fabricate a steel bracket
that connects to the tailwheel using longer versions of the original
through-bolts. It is a very clean installation. I have been told
Gasser Banner can supply the bracket and the Schweizer hook. I have
contacted the SSA about purchasing the STC and Gasser Banner about
getting the Bracket and Hook. Interesting that the Javelin STC uses a
nylon cord running from the hook along the outside of the fuselage
through the pilot side window tied to the "assist strap" with a
specified amount of slack. To release the tow line you pull on the
cord. Seems like a very elegant solution - especially if you only plan
on towing ocassionally.
I hope the SSA has its act together enough to market the STC.
Hope this will be helpful to someone else in the future.
Try this one: http://tinyurl.com/qe6d
Vaughn
AC 43.13 Part 2A figure 8.3 shows a 5:1 lever. This is what you need to get
leverage and ensure that the tow pilot can release. But then also with a
lever there are issues with ensuring pilot access to the lever in emergency.
So a lot of thought as to the lever design and location is required.
AC43.13 Part 2A para 132c talks about 1/16" steel cable minimum. Again over
a long length this is too stretchy. Use 1/8" aircraft cable.
Try for best modern practice, not just using old data because it is
available.
A search of r.a.s archives will probably turn up more useful commentary.
Roger Druce
"Stuart Grant" <smg...@bellsouth.net> wrote in message
news:121d239b.03100...@posting.google.com...
contact me if you want to talk to someone about the approval process.
Chip Fitzpatrick
Before useing a Schweizer tow rig give serious consideration to the
info on this website
http://home.att.net/~jdburch/index.htm
I too would reccommend a tost tow rig only. Far safer for both the tow
pilot and glider.
NTSB stats show on average one tow pilot death each year- upsets on
tow with no chance of recovery.
I think the FAA data is way out of date and should have been revisited
long ago.
Good luck
Rod
Note also that the BGA has a modification to the Schweizer hook, approved
by the U.K. C.A.A., to incorporate a roller bearing in the hook to make
release under heavy load much easier.
W.J. (Bill) Dean (U.K.).
Remove "ic" to reply.
>
> "Rod Pool" <rp...@midwestcc.net> wrote in message
> news:faaf6494.0310...@posting.google.com...
>
> Stuart
>
> Before using a Schweizer tow rig give serious consideration to the
> info on this website
>
> http://home.att.net/~jdburch/index.htm
>
> I too would recommend a tost tow rig only. Far safer for both the tow
Gasser Banner says they have not manufactured brackets and hooks for the
Cessna 180 under their STC for many, many years but will sell the
documents needed for fabrication for $75 - which is a modest cost
considering the hassle. I may purchase just to see how it compares with
the Javelin method.
I have gotten lots of e-mail recommending using a TOST hook or inverted
installation of the Schweizer hook. I have e-mailed TOST hoping to get
information on their E85 release - mainly so I can figure out how to mount
it on the 180 tailwheel (not a leaf spring) and rig a release. I am still
assembling material for review by my A&P/IA so I don't buy anything I
won't actually be able to get approved. None of the experts liked the idea
of pulling the rope for release and pointed out that the FAA Advisory
Circular recommends a lever with a 5:1 mechanical advantage.
Rod's link below shows 337-approved inverted installation of Schweizer
hook on a Pawnee leaf spring tailwheel.
Thanks for all the comments. I will post what I find out from TOST.
Stuart