Taylorcraft Rebuild


A couple of years ago, I purchased this used Hanger Nine Talorcraft for $250, including Zenoah G-23, servos and Futaba receiver.  It had its rendezvous with the ground on the third flight.  A strong cross wind was blowing that made the base leg downwind and I slowed it too much and when the turn to final was initiated, it stalled.  The whole of the front of the fuselage was wiped out.  There was no damage to the emphanage.  The wing had some leading edge damage in a couple of places but minor.

The windscreen and all but one side window was totaled.  The cowl was badly mangled but not torn up and could have been repaired with a lot of effort.  The wreck was looked at a few times and left set aside.  A new windscreen and cowl were available for about $80.  Interest in the rebuild came about for two reasons, first I'd finished repairing everything else and had a new build waiting but wanted to clean out all waiting repairs first.  Sort of a motivation to make me get the plane rebuild.  Second, Hanger Nine introduced another version of the Talorcraft and I wondered if the cowl and windshield would fit.  When I compared prices,  $50 cheaper on the cowl and windscreen plus the cowl was painted (a big item to me because I hate having to try to match paints and fuel proof) and the windshield trimmed, I got to thinking that even if they were slightly different in size, being that the whole front end needed rebuilt, then it could be built to fit, so the parts were ordered.

The cowl is only slightly smaller, perhaps .5 - .75 inches narrower and about .5 inches shorter.  The windscreen however at 8 inches 1.125 inches narrower.  That however is the width at the aft wing saddle so a rebuild will then have the cockpit parallel typical to most models instead of the expanding width typical to the scale Taylorcraft.  It is likely that all the emphanage of the two models was the same and that the fuselage was redesigned with a parallel cockpit to better suit using a two piece wing and wing tube.  I can very well understand the thinking of the redesign as the wing on the earlier model was one piece and very large.  Another issue is that building the center section of the wing into the fuselage allows strengthening the mid section which is very weak because of the footwell windows.  There are only three small areas of wood on each side plus the belly pan, leaving the model weak in the middle. 

Here are some pics.


Obviously, Before the Crash


More obvious, after crash


After Some Debrieding


Fitting Enough Together To Get A Side Pattern


Separating the Emphanage

  Everything forward of the emphanage had to go so that the rebuild could be done with a parallel cockpit section.


Side Pattern

While it may look like the side is intact enough for a rebuild, it is actually a bunch of pieces glued back together enough to get the pattern.  Also, this was not the first crash of this plane and there are several mended breaks.


The firewall fitted to to the cowl


Middle cockpit bulkhead glued to side sections


Belly Pan glued in place... note: landing gear doubler was first glued in.


Forward cockpit bulkhead in place


Firewall glued in place


Bulkhead doubler and fuel tank tray installed


The wing hold down block will serve also to hold the two halves of the plane together


The wing hold down extends aft enough for triangle stock to lock the tail to the foreward section


Turtle deck formers, fuel tank bracing and firewall triangle stock are installed


Servo tray, basswood triangle joiner, lateral brace, fuel line acess and landing gear blind nuts installed.
Everything is ready for joining except finishing the turtle deck, and forward belly pan.


Forward belly pan fitted


Cowl fairing blocks being fitted


Test Joining


Tail section to the forward section


Cowl fairings shaped


Cowl fitted

As can be seen in the above picture, the forward deck sheeting hasn't been installed.  I've been waiting to decide what to do about the engine.  The model was previously powered by a G-23 but it is heavy.  While I can find no evidence that any tail weight was added,  my belief is that the rebuild is going to add forward weight as a few structural efforts were made to beef up the strength of the forward air frame plus I've rebuild with 3/16 luan instead of light ply and balsa doubler. 

About four ounces can be reduced by using another set of wheels on hand rather than the very large balloon tires.  Another option is a lighter motor such as an MLD 28 that would provide a full one pound savings, provide more power and hand starting.  Other advantages would be it would almost completely be contained in the cowl.  None of the issues are deal makers except I don't want to add weight anywhere.


Fitted together to test the balance

I'm very surprised to see the plane tail heavy.  I'd expected the rebuild of the front end to make it nose heavy but looking more carefully, I can see that more material is aft of the CG than forward.  It's now clear that the heavier G-23 is well suited and it's looking like the projected 15 pounds (equal to pre repairs) is about where the end result will be if the tail heavy condition can be solved without adding weight.  Used were 1/4 scale HiTec servos on rudder and elevator and they and the throttle servo weigh a whopping 9 oz and set in a tray at the aft end of cockpit.  Repositioning the servos forward was tested and solved the balance issue so the servo tray will be moved and linkages added to.


Servo tray needs moved forward to balance


A couple of narrowing effects can be seen.  The wing leading edge has to be filled (no problem) .
The gear strut is now too wide (I'll live with it as the wing struts are dependent upon it and they survived the crash).


Leading edge filler pieces and overhead window fillers have been fitted

Several steps have been completed.  The cowl is fitted and cutouts made for spark plug, and exhaust pipes.  The two sections have been glued together.  Servo tray has been moved forward and linkages adjusted.    This leaves the remaining repairs to the wing.  There is about one rib bay on the left wing near the tip that needs some repair and about three bays worth of leading edge repair on the right wing panel.  The wing incidence has not yet been verified, though I really don't know what else to do with it other than zero it.  At the moment, the trailing edge has to be pushed down about 1/4 inch, which may be forcing a slight bit of negative so it needs checked as likely the forward dowel holes need relieved slightly.

Wing incidence has been checked and matches horizontal stab perfect.  Wing bolt holes have been set. 

As the wind screen and cowl were for the new version, there was some concern about the trim stripes matching up and especially the angle of the windscreen installation being such that the horizontal striping didn't end up being angular.  It is looking like the trim is very close to being correct with the cowl trim. 

One issue that still has me concerned a bit is the installation of the side windows.  All but one were destroyed in the crash and a decision has to be made about how to replace.  The new structure is 3/16" thick rather than 1/4" and one option would be simply to glaze them inside rather than flush outside though doing so would not be very clean.  Another is to make a frame for each window, glaze the frame and then sand the window to the frame and insert flush.  Another is to make dies for the windows and heat and fold the windows... this is the method I'd like to try.

Well, the technique was tried and works great... wow!


Used was a discarded crock pot oven
First the male mold is placed in the bottom


15 thousandths polyethelene sheeting cut about 1/2" oversize around is laid on the male mold


The female mold is laid over top keeping gaps equal
The female mold is the exact size of the window and the male mold cut 1/16 undersize around


On top of the glazing, a piece of plywood to keep the pane flat and finally a weight
Heat on low for about ten minutes and the weight will force the female mold down to the male
Cut power and let cool


Window panel completed


Finished window panel after trimming excess


Window fits flush outside and lips inside as the stock windows did
They will be installed of course after covering


This rebuild has six side windows.  Fortunately the molds will work for both sides so only three sets need be made and they are not difficult to make.  The project was far easier than I'd first thought it would be.

Had to lay off the project for a couple of days.  This morning a final CG test was made with struts installed and everything else except the covering and side windows and a few small repairs yet to be finished on the leading edge of the wing on the right side and the wing tip on the left side.  None except the covering will add any weight aft and the CG is showing right on the 4 1/4 point prescribed in the manual.  That is the good news, now the bad.  Total current weight is 15 lbs 8 oz and over the weight the manual suggest.  It list the plane as 13-15 with the G-23 making it on the heavier end.  Wing loading will be 28 oz sq/ft so right about the range of the newer version of the Taylorcraft.   The plane looks like this at the moment.



It did give an opportunity to mark the position for the strut anchor points under the fuselage where it is planned to use blind nuts and nylon screws.

Next, finish repairs to the wing and then sand and cover.


False ribs replaced
Note: Leading edge angle back on each side


Forward rib cap strip in place


Upper sheeting to forward rib cap


The gear strut is soft and relies on bracing
1/16 cable is used


Wing tip repair

Repairs are almost completed.  The one remaining item is the leading edge over the rib cap sheet when the rest dries.

The only hurdle left is the recovering and there is one issue.  The lateral striping remaining on the tail section does not line up with the striping on the new cowl and windscreen as can be seen  above.  I don't yet know how it will be resolved.

The most recent effort has been to rebuild the carb on the G-23 and dial it in.  Tuning produced 8650 rpms with an APC 16x8 and 1650 idle with smooth transition.  One discovery is that low throttle will not kill the motor so a kill method has to be worked out... either an opto kill or micro switch and servo.

Having an abundance of servos and several micro switches in the junk box, that is the route taken. 
Note: the engine kill is set up on the radio so as to require the aux trim to be run up rather than a toggle switch that can accidentally be flipped and shut down the engine.


Micro switch for engine kill

Of some interest might be the servo tray.  As noted earlier, the aft cockpit servo tray had to be abandoned because of balance.  Moving the tray forward meant it had to be removable to allow fuel tank access.  Also, installing radio gear fairly deep in a model is frustrating for those of us with large hands so a decision was made for an easy pull out tray with all radio gear on it as seen below.   The  flight battery is fastened under the tray.  There are no forward tray hold down screws as the forward part of the tray simply slides into a slot provided under the fuel tank tray at the forward cockpit bulkhead.


Flight battery fastened under tray
Note that the switch harness with charge plug can be disconnected from the flight system for easy removal of the tray
Heavy duty extensions are used


Servo tray slot under fuel tank tray


Servo tray in position
Note the extensions to the linkages

The antenna routing is out the top of the plane aft of the cockpit and will be secured to the vertical stab.  This was chosen to keep it some distance from the pull/pull rudder cables and to make it easier to remove the flight system tray. 

The total weight of the flight tray is 20 oz and with the 6 1/2" forward shift represents a fairly major weight adjustment forward compared to the original installation though it had used a smaller 4.8v flight battery that has been replaced with a 6v pack.  I bought the plane used from a good builder and confess to not having checked the CG before flying it, which if it had an aft CG, could have been a contributor to its stall and crash though I don't remember thinking the plane sensitive on elevator.  We will see. 

The solution to the striping alignment is to recover the entire sides and raise the striping as illustrated on the later model Hanger 9 Taylorcraft.  As noted above, covering has begun as the bottom covering can be seen.


Covering process continues
Basic covering is on... trim is next


Fuselage trimmed


Taylorcraft rebuild completed

Observations:  The rebuild was good amount of work and as per first impression, most of it confined to the fueslage as the wing repairs took minimal time and effort.  The only issue encountered was the alignment of the prepainted trim on the cowl and windscreen, due to replacing those parts with parts for the Taylorcraft 20cc.  The solution was to live with a slight kink as can be seen in the trim striping as the cowl turns it down slightly.  The trim on the bottom of the windscreen had to be overlayed to realign but that was easy.

Perhaps the most rewarding part of the effort was how easy the side windows were to make after have fretted over what was to be done with them.  Also, the use of the lumberyard 3/16 plywood to rebuild worked well.

The most significant observation regards the CG and a growing opinion that the CG could have been too far aft and possibly the cause of the crash.  My reasons are that the heavy pilot seat was mostly aft of CG (it has been omitted) but much more of an issue were the servo tray and flight battery were in the aft cabin well behind the seat and they weighed very nearly a pound and in the rebuild were moved a minimum of 6.25 inches forward to obtain proper CG.  I just do not see that the rebuild changed much about the structure weight.  I'm tempted to conclude that the PO (previous owner) wrongly balanced the plane by marking balance points on the fuselage and taking the measurement from the forward bulkhead where the wing dowels seat as is very typical of most wings.  One reason for this conclusion is that I almost did it.  The wing however has a 2.5" leading edge offset forward of that bulkhead, which would cause a balance error of that amount.  Other observations are that the plane had been previously crashed and that it had been flown very little as the engine and muffler were almost spotless.  It's possible that it had not been flown after its first repairs.

Conclusion:  The rebuild has been rewarding both from a standpoint of enjoying the effort and financially.  A good deal was gotten on this plane as it was bought for $250 including engine, receiver and servos.  A new Slim Line Pitts muffler is $99 + freight alone.  The newly released version Taylorcraft is $549 for plane only.   The rebuild cost less than $100 and less than $75 if one considers that only a small strip was used from a $26 roll of checkered covering leaving the rest for another repair or another project.

Final Report after flight testing.

Well.... the flight test was interesting.  The engine had been tuned following rebuilding the carb and seemed dialed in.  It started fine, a range check revealed no range or receiver RF issues and the motor spooled up without any hesitations and seemed to be running fine as it had when dialing it in a week or so before (it was a long wait for a decent fly day).  Take off was not much of an issue.  The nose wanted to rotate over a little and just a little back stick settled it for a full run up and a slight bit more back stick had her flying.  She went right just a tad but otherwise climbed smoothly.  Two clicks of up and a click of left had her about trimmed out. 

After gaining altitude, power back to about half stick and checked for trim at mid throttle... seemed good.  Chopped the throttle (very high) and let her glide and she seemed to enjoy a predictable smooth glide.  Powered her back up and looped her and that was smooth and showed adequate power for a good size loop.  Pulled a real tight full elevator loop and she showed some tip stall character.... she'd have to be respected.  Up high at half throttle, she was put in a 45 deg down slope to test CG and she revealed only a hint of upturn indicating the CG was probably exactly where it should be.

She was flying well perhaps five minutes into the flight and very high down at one end of the field, the engine quit.  Fish tailing her back and forth didn't kill enough altitude and it wasn't long before she was in trouble with too much height and a runway that went over the hill and out of sight.  She passed me 150 feet in the air.  I should have dived her and made a very hot wheel landing.  Now, I had a decision to make with neither option good.  If I kept her straight, I'd be landing her over the hill and blind and on a fairly sharp downhill grade.  If she caught a wing tip she'd cartwheel or almost certainly without knowing when to pull the stick back, go hard over on her nose and summersault down the grade.    If I tried to turn back on the runway, she'd likely stall. 

I put the nose down and initiated a fairly hard turn to bring her around and she tip stalled and went in on her nose from about forty feet.  She of course broke in half where all those windows are.

I didn't have any real good choices but the best would have been to dive her hard and do a high speed wheel landing.  Probably the second choice should have been to land her blind and keep the wings level until she was out of sight and then just hope for the best and let her settle by herself.  I admittedly chose the poorest option but it is the one that I get away with on most of the models I fly.... this one however will not tolerate such behavior.

The Damage:  She doesn't look as bad as the previous crash where everything was destroyed from the aft cabin bulkhead forward.  There is very little damage forward of the forward cabin bulkhead and no damage whatsoever to the middle of the cabin and rearward.  While she broke completely in half, she did so completely in those two inches from the forward cabin bulkhead and into the windows.  The firewall, forward belly plan, windshield deck and landing gear blocking are all intact.  The only damage on the wing is to the two mounting dowels and one set of servo gears.  The servo tray is not damaged, nor are the wing struts.

Can it be rebuilt?  Of course.  How easy?  I don't know yet.  She might can be pieced back together rather than a major rebuild.  I don't know how well the luan plywood can be fit back into place.  She is a very pretty airplane and the guys at the field gave her a lot of chatter about how good she looked after the rebuild.  As can be seen in the above rebuild thread, it was a major effort but would be some easier to do again.  I've the pattern for sides for example and now know how to make the side windows with ease and have the molds for those.  The greater question, is she a plane I want taking up space in my garage or is she too tempermental for my laid back flying desires and skills?  My guess is that I'll give her one more strike but I'm not sure that I'll rebuild her now or lay her aside for a bit.

Why did the engine quit?  I've no clue.  I'd tuned it more than a week prior to the test and did so after rebuilding the carb.  A bench run had shown that the carb had a problem because the high speed needle was run in fully and wasn't leaning it out.  After the carb kit, it was run again and dialed in and the top end needle was effective and normal.  It was pulled back two hundred rpm from top and had no spooling or idle problems.  At the field, it started easily, spooled without hesitation and run full power without any sag.  It ran flawlessly until she quit while cruising at about half power.  Did it heat up?  I'd be surprised if overheating was the cause of why it quit.  The cowl was baffled and there was plenty of exit.  The most probable explanation was the temperature and humidity difference between the day it was tuned and the cooler very damp day.  I doubt the temperature difference was that big of an issue but combined with the humidity change, the difference could have caused the flame out.    



Repairs have begun and with luck, it will be a fit the parts back together effort with perhaps a doubler or two for added strength.  A new cowl and windscreen are ordered. 

Mid January, 2010

While the crashed damage above looks bad, the broken parts have been fit back together and repairs progress with only some doublers remaining to be installed and then recovering the front section.  Those lower window panels will get closed in with plywood doublers to add some mid plane strength.  New windscreen has arrived but cowl remains on back order. 

May, 2010

The cowl came recently so there is more impetus to finish the TCraft again.  I test ran the engine a couple of days ago and believe the cause of the dead stick and crash became evident.  While the motor started easily and seem to run fine, after about five minutes of run time it sagged power and quit, obviously overheated from starving for fuel.  After pulling and inspecting the carb it was noted that the pump diaphragm used in the rebuild was acetate and even though it had such little run time was deformed.  A bit of checking got some feed back that the acetate pumps are given to poor pumping capacity so another repair kit was obtained.  It had the option of a newer teflon pump, with much greater pumping capacity claimed.  No sign of over heating was noted with it.  In fact the crank case was comfortable to the hand after a ten minute run... a very different story than the day before when it got hot.

Now knowing the cause of the dead stick, I feel better about getting the plane finished and flying.

The Taylorcraft is flying again    July. 2010

Repairs were finished and the plane has flown and is enjoying the flight ready hanger.



Thanks for taking a look.  Rebuild progress will be added to this page as it takes place.