- 6.5.2 – Rudder Pedals
- 6.7.1 – Spar Positioning
- 6.1.5 Keel Hardpoints
- 6.8.1 – Canard Reinforcements
- 6.1.3 Keel Access Holes
- 6.2.3 Front Seats
- 6.3.1 Assemble Rudder Pedals
- 6.3.1 Brake Lines
- 6.3.1 Brake lines
- 6.3.1 Brake Lines
- 6A.3.1 Toe Brakes
- 6A.3.1 Parking Brake
- 6.6.2 – Install Landing Gear Selector
- 6.2.2 Safety Harness Hardpoints
- 6.9 Overhead Fresh Air Plenum Modification
- 6.9 Overhead Fresh Air Plenum Installation
- 6.3.7 Keel Installation (prep)
- 6A.3.1 Rudder Pedal Assembly
- 6.3.7 Keel Installation
- 6.7.2 Main Spar Installation
- 6.7.3 Main Spar Triax Layups
- 6.2.1 Seat Hardpoints
- 6.1.2 Keel Access Cover Flanges
- 6A.3.1 Rudder Pedal Installation
- 6.6.2 Install Instrument Panel
- 6.2 Assemble Seats
- 6.8 Doghouse Edge Finishing
- 6.8 Canard Reinforcements
- 6.8.2 Doghouse Attach Points
- 6.5.4 Install Nylaflow Tubing for Rudder Cables
- 6.3.7 Install Aft Keel Section
- 6.9 Overhead Plenum Lights
- 6.0 Aft Carbon Beam (Remediation)
- 6.9 Overhead Fresh Air Plenum
- 6.9 Overhead Fresh Air Plenum Painting
- 6.0 A-Pillar Beam (Overhead Switch Panel)
- 6.3.2 Front Seat Assembly
- 6.3.2 Front Seat Rails
- 6.3.2 Seating modifications
- 6.2.2 Safety Harness Replacement
- 6.2.2 Safety Harness Replacement
- 6.3.2 Seat rails and hardpoints
The last task for the day was to create a rectangular opening just forward of the firewall on each side of the fuselage for the main spar. The spar is the primary mounting point for the main wings.
Here are the lines that mark the opening on the left side.
And then, after cutting the opening.
