T1-1 The engine was started according to POH. Brakes can succesfully stop the aircraft at 2500RPM. Brakes can bring aircraft to a full stop. Aircraft can be kept straight while the rudder is straight. Aircraft can be steered using only the rudder. The aircraft can be pivoted both left and right using the brakes. Canopy was latched. Brakes can succesfully stop the aircraft at 400RPM. Brakes can succesfully stop the aircraft at full throttle. ******PENDING****** PAD CONDITIONING ******PENDING****** MAGNETOMETER CALIBRATION Engine was shutdown according to the manual. ******PENDING****** BRAKE RELEASE
T1-2 Stall warning was held in the on position by using duct tape. Engine was re-started and everything was checked accoding to the POH. RPM was increased to 4000RPM. Stall warning is loud enough.
