AN365-1032A

  • Circuit Breaker Mounting

    Circuit Breaker Mounting

    Bolted Ram mount base to RH panel cover using AN3 hardware. Cut copper bus bars to size and drilled circuit breaker holes at 0.8 inch spacing. Installed circuit breakers into RH panel cover then secured bus bar onto bottom terminals of circuit breakers with 6R4 screws. Used two separate bus bars for circuit breakers; one…

  • FWF Wiring – Part 2

    FWF Wiring – Part 2

    Replaced temporary bolts in starter solenoid with proper length bolts. Added extra bit of wire to alternator wires with solder splices and finished wiring and mounting voltage regulator and capacitor (minus the reset button). Drilled LH and RH grommet holes through firewall and clecoed gromet covers into place; will rivet when wiring is completed. Made…

  • Canopy Installation – Part 3

    Canopy Installation – Part 3

    Reattached canopy to fuselage with hinge pin and verified fitment along front and rear edges along with latch operation. Installed canopy retaining strap and tested operation. Located hole for canopy latch pin and drilled into upper longeron. Will remove plastic from inside and outside of canopy once aircraft is complete. Canopy task now complete! Hours…

  • Canopy Trimming – Part 3

    Canopy Trimming – Part 3

    Continued to trim and fit canopy. Matched drilled final holes in LH side of forward and aft canopy bows and realized that canopy was pulling up the frame in the front by about 1/4″. Unbolted front left corner of canopy frame and added 1/8″ spacer to lengthen the front bow area. Also added rubber washers…

  • Windshield Installation – Part 6

    Windshield Installation – Part 6

    Finished installing windshield onto fuselage by installing screws from front to back, skipping last bottom screw on each side. Aligned windshield bow with top center screw and installed sandwiching strap in between. Needed to run tap through each screw hole to clean paint out of threads; should have done before installing bow, however. Worked from…

  • Windshield Installation – Part 5

    Windshield Installation – Part 5

    Using two people, reinstalled bolts in upper longerons, windshield skirt, and upper motor mounts. Applied torque check to bolts to monitor torque. Slid windshield into place and began installing bolts starting from forward center and working backwards. Used a piece of tape on wrench to prevent nut from falling out. Hours Worked: 1.95

  • Canopy Components – Part 3

    Canopy Components – Part 3

    Clamped canopy frame components together and checked fitment on fuselage. Forward windshield flange might need a bit of trimming but overall fit good. Pilot drilled then updrilled forward and aft canopy bows to side rails. Cut canopy hinge pieces from P5 piano hinge stock then pilot drilled per plans. Modified hinge pin per plans and…

  • Control Stick Assembly – Part 3

    Control Stick Assembly – Part 3

    Disassembled dual stick assembly and deburred stick holes. Lubricated control stick horns with lithium grease and deburred taper pin holes. Reassembled left and right control sticks and attached link rod with hardware. C04 complete! Hours Worked: 0.70

  • Tail Installation – Part 3

    Tail Installation – Part 3

    Mocked up ELT location on rear shear web and marked vertical stabilizer on where skin needs to be trimmed. Removed vertical stabilizer and marked out mounting hole location on shear web. Trimmed vertical stabilizer skin and riveted ELT mount and clamps to fuselage. Painted elevator horn with spray paint. Reattached vertical stabilizer with AN3 and…

  • Rear Spar Carry Through Assembly

    Rear Spar Carry Through Assembly

    Created F03-02, F03-05L/R, F03-08 and -04/-07 spacers from legacy plans using angle and channel stock on hand. Clecoed together -01 rear spar carry through assembly together then updrilled all holes. Disassembled part and prepped parts for final assembly. Assembled all parts with rivets and AN3 hardware. F03 complete! Hours Worked: 6.65

  • Fuel Tank Installation

    Fuel Tank Installation

    Rinsed tank out with water to clear out debris from inside. Re-fit tank to fuselage and trimmed fuel bay area slightly more to accommodate vent fitting. Clecoed tank stop into place and confirmed tank was sitting full forward. Installed fuel tank straps and lightly tightened straps until they were touching the tank fully. Used AN3-7A…

  • Aft Forward Fuselage Assembly – Part 3

    Aft Forward Fuselage Assembly – Part 3

    Used rivet stems and clamps to hold center seatbelt channels into place while locating and pilot drilling seat ribs and channels to forward floor. Clecoed -14L/R angles into place. Located idler assembly and pilot drilled to lower cross member and seat belt attach assembly. Updrilled all holes in fuselage floor then removed floor for better…