That is how I see it too. but?If it ain't broke don't fix it...
This carb shows that the ADs have been complied with (V) (F) stamped on the data plate & SBs aren't required.Definitely need to run the entire list of SBs that cover that model carb, for every parts manufacturer, unless the logs show to be done. There are a number of them that are stacked on top of each other and several that supercede others and others that change compliance and requirements.
A quick look showed at least 3 dealing with the body bolts showing signs of leakage. All were issued by different companies, some with installation effectivites, some for parts installations and others for overhaul facilities. Then there are the float and venturi messes too.
The Marvel line of carbs has been made and sold as well as supported by a number of companies over the years, and it has become a very tangled web of data and inspection requirements.
And this is why answering any question you ask is a waste of everyone's time.This carb does have a discrepancy that should not pass annual.
With the history on the Marvels, anyone who doesn’t adhere to the SB’s is an idiot.
It would be apparent for anyone familiar to the carb.. and it has nothing about SBs.And this is why answering any question you ask is a waste of everyone's time.
Do your home work!With the history on the Marvels, anyone who doesn’t adhere to the SB’s is an idiot.
when you adhere to all Service Bulletins or replace the carb with new, the carb is no longer able to run auto fuel?With the history on the Marvels, anyone who doesn’t adhere to the SB’s is an idiot.
Can you please elaborate? My plane has the same carb, and while I'm aware of the venturi AD I don't know the history or the real world risk.Do your home work!
Anyone who is familiar with carb would know why the AD on the Venturi occurred and why Precision Airmotive no longer makes the carb.
Do you know why the MA3SPA uses 1-2 gallons more fuel than the early unmodified carbs? and why that is not good.
The world of CARBs is a long story, there were several companies involved, Marvel invented the carb many years ago and was doing fine until Precision Airmotive got involved, they used 7carb failures in 37 years invoke a emergency AD to place a 1 piece Venturi, this screwed up the flow rate in the carb, and it would not run correctly. After 4 re-rites the AD was modified so the original parts could be re-installed and checked each 100 hours for looseness of the Venturi.Can you please elaborate? My plane has the same carb, and while I'm aware of the venturi AD I don't know the history or the real world risk.
I wouldn't admitting it in this crowd
It wasn’t an admission. More of an observation.I wouldn't admitting it in this crowd
I thought you were bragging.It wasn’t an admission. More of an observation.
Lol. I am guilty from time to time but not exceptional in any regard. To clarify I wasn’t insulting anyone. Just enjoying the banter.I thought you were bragging.
pretty much, but when the aircraft is not assembled properly isn't that a discrepancy that should corrected?So, this is one of those "everything works perfectly well, but the airplane is not 'airworthy' because it does not exactly match what was written on a piece of paper in 1948" situations. And, you can't get what was written in 1948 because the part with the correct part number hasn't been produced for the last 70 years.
If that is the case, then I stand corrected.4 studs that hold the carb to the sump provide the cotter key hole
Actually a cotter key is to be used.
I'm not your Lycoming Guy. It's interesting.Lycoming long ago started using plain nuts, lockwashers and flat washers to mount their carbs. Studs weren't drilled.
pretty much, but when the aircraft is not assembled properly isn't that a discrepancy that should corrected?
When Continental requires a positive stoped nut shouldn't there a cotter key?
the 4 studs that hold the carb to the sump provide the cotter key hole, shouldn't they used?
The 0-300- shown here requires a castle nut and cotter key. not a MS210--- style in the picture.Depends on the installation. The current small Continental parts book shows a plain washer, lock washer and plain nut. Maybe in a previous version it was to be safety wired, but times do change. In the picture I didn't see an exposed cotter pin hole in the studs. Maybe Continental was having studs break in service, and changed to a solid stud. Might be a service bulletin on that.
Which small continental ? the 0-200/A-65/85/90 requires it to be located on the intake spider and a stat-o-seal separating the case and intake then a washer then a castle nut and key.Depends on the installation. The current small Continental parts book shows a plain washer, lock washer and plain nut.
Those Lock-O-Seals aren't sealing anything. They're acting as flexible washers to allow the manifold to rock a little on the studs. The Marvel Schebler carb has a bad habit of sloshing fuel out the bowl vent, which is in the carb bore behind the venturi, causing flooding and rough running. The weight of the carb and the torsional vibration of the O-200 worked together to make that carb do that at certain RPMs. Rough running and serious RPM drops can happen.The intake manifold (spider) is attached with items 1, 2, 3, 4, figure 12. The studs for the spider are not shown in figure 12. You have to go to figure 1, I think item 11. It is the manifold that requires castellated nuts and cotter pins, due to the lock seals that seal it - don't want to crush the seal with too much torque and allow the seals to shrink and expand.
T
The overhaul manual has an innocuous little paragraph about tightening those castellated nuts. You run them up finger tight and then to the first notch that lines up with the cotter pin hole in the stud and install the cotter pin. NO wrench is used. They want that manifold flexible, and the rubber connectors on the induction tubes will allow some movement. I spent a couple of weeks troubleshooting an unhappy O-200 in a 150 20+ years ago and finally read the stupid instructions. Did what they told me and the engine smartened right up. I found that the rebuilder had left the Lock-O-Seals out altogether and had the manifold rigid, and have found several others like that, too.
Those Lock-O-Seals aren't sealing anything. They're acting as flexible washers to allow the manifold to rock a little on the studs. The Marvel Schebler carb has a bad habit of sloshing fuel out the bowl vent, which is in the carb bore behind the venturi, causing flooding and rough running. The weight of the carb and the torsional vibration of the O-200 worked together to make that carb do that at certain RPMs. Rough running and serious RPM drops can happen.
The overhaul manual has an innocuous little paragraph about tightening those castellated nuts. You run them up finger tight and then to the first notch that lines up with the cotter pin hole in the stud and install the cotter pin. NO wrench is used. They want that manifold flexible, and the rubber connectors on the induction tubes will allow some movement. I spent a couple of weeks troubleshooting an unhappy O-200 in a 150 20+ years ago and finally read the stupid instructions. Did what they told me and the engine smartened right up. I found that the rebuilder had left the Lock-O-Seals out altogether and had the manifold rigid, and have found several others like that, too.