I inspected the Spar carry thru this morning. (it is clean as new) this aircraft is a 1975 has 1300 TT, a disassembled 0-360 180 horse (the original engine) was torn down all parts are there with yellow tags, but needs assembly. the prop is there, never overhauled, and no ADs apply. I've not see any of the other parts yet.Worth depends on a lot of things, but there are some ADs and SBs that need to be checked. There are some places that like to crack, and that spar carrythrough is very susceptible to corrosion. If it's bad enough it's an expensive fix--as much as the airplane might be worth. Cessna used CAT hose for the overhead vents, and it rots and the reinforcing wire contacts the spar as well as other stuff like the fuel vent crossover tubing, and they corrode. Moisture comes from condensation from the breath of the occupants. No primer was used in those ceilings or on the spar to protect the surfaces.
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What should I offer ??
Have discovered a 177-b that was in restoration when the owner A&P-IA Died, it has been setting for a few years.
Question is simple, what are they worth restored?
Do you plan to paint it? Install a 21st century interior? Panel?
That is the hazard of restoring. we get 100 grand tied up in a 50k aircraft.$80k+ for a 177B? Either it has $35k in radios in it or a guy is dreaming. 95% of tire kickers would end up with a 182 at that price.
this O-360 have the D2000/3000 magneto?
None of the 177/B/RG had optional factory extended range tanks, is that a baggage fuel tank?
Yes on the paint, it has been scotch brited, thus is scratched beyond polished.
What would you call a 21st century panel?
Are you sure? My POH for my 76 lists that as an option.None of the 177/B/RG had optional factory extended range tanks, is that a baggage fuel tank?
A lot of the better equipped ones are in the $70-$75k range.
Talk to me about fuel tanks ,, are they a bag? or integral ? or a tank?All of them are gonna need fuel tank sealant repairs someday. Right now that is basically impossible due to the extremely poor access. The only way IMHO is to add new access panels to the fuel tanks. I haven't seen anyone even entertaining the idea yet.
Talk to me about fuel tanks ,, are they a bag? or integral ? or a tank?
All 177s are integral, hence "sealant repairs".
I don't see a future for aftermarket bags like Mooney, I don't think there would be enough demand for such a conversion. Then of course increase in weight which no 177 needs.
Now a simple fuel tank access improvement kit, that would be worth the effort.
Wings are off, why not a sloshing sealer?
I've read a little on old tank sealers and found there are those that are compatible with auto fuels and there are those that aren'tWhy would you do that when the original widely used even today poly-sulfide sealants nearly 50 years?
My tanks are 48 years old and no leaks. Not ever going to slosh them. How can they be clean enough to even use such a product and guarantee adhesion with the increadibkt poor access into a 177 tank? I think you'd just make a bigger mess. http://generalaviationnews.com/2011/03/07/sealant-contributes-to-fatal-accident/
I've read a little on old tank sealers and found there are those that are compatible with auto fuels and there are those that aren't
My statement above was interference to the accident mentioned, You really must know which sealant to use for the fuel you will run.My 68 with plain old 150 horse has been running plain 87 octane ethanol-free gas for about 5 years via Peterson STC.
I don't believe any of the 177Bs are STC for autogas, even tho the O-360-A1F6 (and D) can run 91 <I think>
My statement above was interference to the accident mentioned, You really must know which sealant to use for the fuel you will run.
When I worked theTC-4C crew at NAS we would defuel, calk the lines then, then open the tanks and spray in the old red top coat using a garden sprayer with a long wand. that was the only thing that finally stopped the leaks.How do you prep it so it WONT peel?
Sloshing over old sealant sounds like shooting yourself in the foot too. How well is going to stick to the old sealant? How much prep does the bare aluminum tank walls need?
Proseal has adhesion promoters available, applied before the sealant is.
When I worked theTC-4C crew at NAS we would defuel, calk the lines then, then open the tanks and spray in the old red top coat using a garden sprayer with a long wand. that was the only thing that finally stopped the leaks.
The red top coat from pro-seal works in the moonies why would it not work in a Cessna wing? this stuff
http://www.aircraftspruce.com/pages/cs/fueltanksealants/bunan.php
There is the question of the day.How do you prep it so it WONT peel?.
There is the question of the day.
might work actually, except when you collapse the wingJust drain the tanks at annual and vacuum out what peeled off every year. (sarcasm)
might work actually, except when you collapse the wing
They use the same skin doubler twice on the 60 gallon tanks, that doubler is where the filler adapter is screwed on.
I don't see why a guy couldn't get approval to install additional holes in the same manner, one inboard and outboard of the filler adapter on standard range tanks, just one hole inboard of the filler on long range tanks. Maybe the ribs are too close together in the other bays for that doubler.
What would you use as a reference to gain field approval ? this is a stressed skin on a cantilever wing. I don't believe the FSDO would ever give their blessing, so the local DAR would have to bless it.
DAR does mostly issuing of airworthiness certificates like imports type work, you mean DER?
Simple, I'd starting contacting part 23 structural DERs on the FAA's list, with a brief description of the proposal with pictures, or ask the mothership first, Cessna.
There's no reason these have to be the most miserable (or nearly the most) fuel tanks to repair on a SEP airplane.
Yep - DER
That is how it starts, Some one must provide the engineering, Cessna has been very reluctant to do this.