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WING ATTACHMENT WIRING FLIGHT CONTROL  MISCELLANEA CANOPY INSTALLTION LANDING GEAR FUEL COWLING OPTION'S  BUILDERS LOG
Page 32.14: FLIGHT CONTROLS
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Step 01: Route the F-1247B Aft Stabilator Cables forward through the holes in the F-1207B and F1206A Bulkheads; see Figure 1. The cable from the top stabilator horn passes through the top hole  
Step 02: Route the F-1257A Forward Stabilator Cables aft through the holes in the F-120A & D Bulkheads; see Figure 1. The cable from the right pulley passes through the upper hole.  
Step 03: Reach through the access holes in the bottom of the fuselage and connect the F-1247A & B Stabilator Control Cables as shown in Figure 2. A wire tool can be made that is inserted into the holes in the cable ends, this will hold them stationary as the barrel is rotated.
Step 04: Place a small weight on the stabilator to hold the traiing edge down. Remove the slack from the upper cable by tightening the upper cable  
Step 05:  
Step 06:  
Step 07: Remove the clamp and stick from the control stick and the weight from the stabilator.
Move the control stick between the forward and aft pitch stops. The stabilator should reach its travel stops just before the corresponding control sticks are reached. If not adjust the turnbuckles an equal and opposite number of turns until it is achieved.
 
Step 08: Once the proper tension is achieved, and no more than three threads are exposed from the ends of the barrels, align the V-notch in the ends of the barrel with the groove in the cable ends and then insert the lock clips as shown in Figure 3. the hook end of the lock clips are inserted into the hole in the center of the barrel and must be completely  pressed in until the hook springs open inside the barrel  
   
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CENTER SECTION MID FUSE LOWER FUSE  SIDE SKINS ROLLOVER TAIL ATTCH  SEATS PEDALS FUEL FWD FUSE  BUILDERS LOG
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