20 February 2005

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20/2/05
Sanded flap servo mount. Flap drive assembly and wiring completed and tested successfully.
Trial fit of aileron cable using wedge and R-clamp.
Lower front seat belt lugs and reinforcing installed except for flock.
Battery box riveted to firewall. Hole for main wiring harness drilled in firewall.
Right door installation commenced. Left back door hinge recesses cut with 2 inch hole saw.
Left hand side compression gussets cut and fitted but not epoxied.
Time: 5 hours
Total Time: 116 hours

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