Jim Miller said:I would never dispute the advantages offered for the jack screw trim. I have also heard from people with trim tabs that they work reasonably well. I am going with a trim tab on my exp Cub/SuperCub just because it
is much simpilar to fabricate and install. It gets rid of a lot of pullies and the trim cable. For the kind of flying I will be doing I expect it to work ok for me.
Indabush said:Does anyone know why did Piper went with the Jackscrew instead of a trim tab?
Jim Miller said:Hydrocub
My goal is to fit it into the 1320 gross wt LSA category. I will be flying solo 99% of the time with no more extra wt than a small bag. If I do carry passengers it will just be my wife and myself which together is about 270 total.
Jim Miller said:Hydrocub
My goal is to fit it into the 1320 gross wt LSA category. I will be flying solo 99% of the time with no more extra wt than a small bag. If I do carry passengers it will just be my wife and myself which together is about 270 total.
cubdriver2 said:Jim Miller said:Hydrocub
My goal is to fit it into the 1320 gross wt LSA category. I will be flying solo 99% of the time with no more extra wt than a small bag. If I do carry passengers it will just be my wife and myself which together is about 270 total.
This makes no sence, some of the lightest certified 2 place aircraft ever built had jackscrews, E2 Cub, J2 Cub, J3 Cub, it gives you the ability to trim for ANY given speed and STILL have full elevator travel which gives you the safest and most comfortable range of tail authority.
Glenn
It only makes sense if taken in context. I was responding to a post about problems at or near gross wt. My point was that a 1600 lb true gross wt
arbitrarily limited to 1320 will have no such concerns.
Mvinion
I have moded a PA22 balanced elevator with a Wag aero trim tab kit. I am using a Van's two lever throttle with the second lever to be trim. All I need to do is connect with a marine cable to trim tab and I am done. Think of all the pullies, trim crank, trim cable, etc eliminated. The trim will be ground adjusted with washers, flown, readjusted, etc until it flies straight and level with trim tab flush with elevator.
Jim Miller said:cubdriver2 said:Jim Miller said:Hydrocub
My goal is to fit it into the 1320 gross wt LSA category. I will be flying solo 99% of the time with no more extra wt than a small bag. If I do carry passengers it will just be my wife and myself which together is about 270 total.
Mvinion
I have moded a PA22 balanced elevator with a Wag aero trim tab kit. I am using a Van's two lever throttle with the second lever to be trim. All I need to do is connect with a marine cable to trim tab and I am done. Think of all the pullies, trim crank, trim cable, etc eliminated. The trim will be ground adjusted with washers, flown, readjusted, etc until it flies straight and level with trim tab flush with elevator.
Jim-
I have to be blunt. This is a poor design. The failure mode with a single cable system has a high potential of full loss of control. If your marine cable fails (they do) you will have a runaway trim tab. You might want to study up on this.
Tim
Jim Miller said:The marine cable idea was something I saw on this site. If a bad idea I will use something else. There are a lot of airplanes flying safely with trim tabs and I need to take a look at some of those. How are the cessna's, husky and other aircraft constructed trim tab wise. Are they a single cable push/pull or do they have a better set-up. Van's is another 200mph aircraft with trim tabs. Does anyone know how van's trim tabs are connected. My first post on this thread said that I in no way was disputing the superiority of the Piper jack screw tail system. I have flown my Colt for 15 years with the jack screw trim.
Carey Gray said:This is kinda like the old days, where guys declared themselves experts and then gave advice on things they know nothing about. I miss the old days.