G1-1: The latest "Read Me", firmware and configuration files were downloaded. ******PENDING****** ELT TEST The avionics cooling fans were confirmed to be circulating air, the left fan pushes air upward and the right fan pushes it downward. Both fuel pumps were confirmed to be able to turn on. The EFIS display comes on and the battery was charged up to 13.6. ******PENDING****** UPLOAD TAILNUMBER
G1-3 Trim speed knob was set to MAX. GPS source functioning COM Radio powers up, tx and rx confirmed. Intercom working. Transponder powers up. Transponder indication on EFIS. ADS-B functioning. Stall Warning is louder than AOA tones. AOA tones are louder than EFIS warnings. Dimmer control works for both lights and and EFIS. Nav lights turn on on NAV, red on left, green on right. STROBE turns white strobes on on both wings. Dimmer controls the cabin light.
G1-4 Landing light turns on on STEADY. Landing light pulses on PULSE.
--- OTHER APPROPRIATE SYSTEMS ---
The canopy was latched. Canopy warning shown on EFIS.
--- LANDING GEAR & BRAKES --- The gear access covers were removed. The gear attach nuts are properly torqued. Brake system has been filled with a MIL-H-5606 equivalent (MIL-PRF-83282) The brakes on the pilot seat were pressed and held for 30 seconds and feel firm. No leaks on brake lines. The aircraft was pushed while holding the brakes and it was confirmed that it does not move when pressing them Brake pedals on passenger seat were tested as it was done on the pilot's seat. It passed all tests. No leaks were found. All tires were pressure checked (28psi on main wheels and 22psi on landing wheel). There is enough gap between the tires and fairings.
FLIGHT CONTROLS CHECK
--- FLIGHT CONTROLS ---
G2-1 Nose up trim switch was actuated. Holding the trim switch stops after 6 seconds. The trim reached full Nose Up. The tab was trailing edge down from the stabilator. Nose down took 12 seconds to reach full travel.
