Wings

Ailerons mounted  ( 1 hr )

Mounted LH and RH Ailerons to Wings and Pushrods.   Some adjustment required using washer positions (reversed location of 2 washers vs 1 ) to center aileron between hinge supports to avoid contact with rivet heads on hinge brackets.  Documented in instructions so I can repeat after dis-assembly, etc.   NOT tightening locknuts at this time since expecting some adjustments will be required to neutralize position.  Also, will be removing pushrods and Ailerons when I rivet on bottom skins...so I know they're coming off soon.

 

Wings

Pushrods Installed ( 3 hrs )

Sect 23-09:  Installed Pushrods between Torq Tubes and Bellcranks for both wings.  (I discovered Vans failed to provide W-730 template used to align bellcranks in neutral position.  When I contacted them, they emailed a dimensioned drawing (and sent the actual one in the mail I plan to use to confirm alignment).  I determined only 1 dimension was critical and some of the shapes were unnecessary - so making the template was relatively easy vs the all the dimensions w/o tolerances shown to .001".... Their engrg dwgs need to be properly dimensioned !

I left fasteners loose to allow final adjustments.   Really like having the Washer Wrenches from Cleaveland Tools...one is shown in pic at inboard rib area near Torq Tube.   These make slipping in small washers much easier - with so much less cussing.

RH Wing...pushrod connected

Very pleased with the silky smooth operation of the control linkages - extra time spent getting the brass bushing fit just right at Bellcranks seems to be paying off.

LH Wing...note fastener not tighted...yet.

RH Wing Bellcrank w/ W730 template holding neutral position

   Autopilot support bracket installed...pending Servo install.

LH Wing Bellcrank..  Loose nuts until final adjustments.

Wings

Bellcranks Installation ( 3 hrs )

Switched schrader air valve to RH tank along with cap for air line so I can test for leaks.   Holding air in balloon long time, but didn't get around to checking with soapy water (optimistic though !).
















Meanwhile I determined center of travel of Electric Aileron Trim Actuator using 9V battery to exercise through full travel.   Ready to install next.  

Since I received the backordered Bellcranks from Vans Monday, I now could do Sect 23-05 - installing Bellcranks. The long brass bushing required much more than simple deburring of ends to insure easy & smooth rotation of bellcranks.  I spent a LOT of time gently (no undo option !) reducing brass diameter and smoothing insider of Pivot Tubes.  Seemed weldment onto Pivot tubes may have caused distortion.

showing brass bushings...partially installed in pivot tubes

Finally achieved free and easy rotation.  Installed LH and RH Bellcranks into Wings. Yay !

Wings

Cont'd Electric Aileron Trim  ( 2 hrs )

Electric Aileron Trim assembly continued at Steps 3-6 Sect OP38-02 and  -03 Step 1 & 2.  Drilled #30 holes, deburred edges, cleaned, primed.  Mounted Ray Allen servo and linkage.

Wings

Tank Leak Test, Autopilot installation  ( 3 hrs )

LH tank testing:  Only place I've been identifying leaks was at the balloon attached to the tank.   Replaced balloon, applying thread sealant prior to slipping onto fitting.  Used band of strong tape, followed by safety wire twisted tight (thanks Vans Air Force for tip to use safety wire/pliers !).  Finally....no bubbles at balloon attach !    Now I can concentrate on confirming no other leaks.  So far all I could reach showed no signs of bubbles w/ generous applications of soap suds.

 

Started Optional Sect 56 - Garmin Autopilot Servo install kit.   Bolted on Roll Servo Brace in right wing, built 1 Pushrod for Pitch servo, and 1 Pushrod for Roll Servo (1/8" longer).  That all I can do in the wing until I purchase the Garmin Servo - which I probably won't buy until I purchase the Garmin G3X avionics (displays, etc).

Powder coated white brace added to bellcrank mount on Right Wing Spar

Looks simple, but alum tubes required drilling and taping for 1/4-28 threads.

Getting started on the Optional Sect 38 -  Electric Aileron Trim.  Drilled #30 holes & deburred mounting brackets.

Wings

Install Torq Tubes  ( 2hrs )

Installed Torq Tube Assemblies in LH and RH Wings per Sect 23-08 Steps 1-4.   LH filled gap perfectly, needing no washers.   RH needed just two thin washers, NAS11490432 to fill gap   (avoids overloading bearings when ends are tightened).    Impressive smooth operation.   Not yet torqued, since not sure if final installation.

 Spent time reviewing remaining tasks, and re-checking LH tank for leaks.  No bubbles as soaping rivets and joints.   Seems only one I can find is where balloon attaches to fitting !  Originally wrapped with tape.  Tried tightening wire around "nipple", but still leaks.  Gotta research Vans Air Force site to see what others have done to "seal" balloon.  I want confirmation no leaks in areas I can't reach due to tank installed onto wing.

Wings

Torque Tubes  ( 1 hr )

Drilled final holes to complete assly of LH & RH Torque Tubes.  Sect 23-07 Steps 1-4.  Used shotgun cleaning rod again, but this time as perfect "gage" to measure actual gap between bearings for Left Wing and Right Wing.  Since plus/minus 1/64 inch required for final length of Torque Tubes, this will insure fit.

Trusted "gage" more than measuring to 1/64".  But checked both ways

Ready to dis-assemble to deburr.

Emailed Vans again - only 4 of 8 required AN13A bolts provided.  Seems they've missed again that QB has two wings! in inventory list.