<p> Flight Test- Engine</p><p>Runup: Cruise: Static RPM: ALT: RPM drop MAP: Primary injectors off: RPM: Secondary injectors off: IAS: Leading coils off: TAS: Trailing coils off: OAT: MAP: Fuel pressure: RPM: Coolant temp: OAT: Coolant pressure: Fuel pressure: Oil temp: Coolant temp: Oil Pressure Coolant pressure: GPM: Oil temp: Oil Pressure: Cruise: ALT: Take off: MAP: MAP: RPM: RPM: IAS: IAS: TAS: OAT: OAT: Fuel pressure Fuel pressure: Coolant temp: Coolant temp: Coolant pressure: Coolant pressure: Oil temp: Oil temp: Oil Pressure: Oil Pressure: GPM: Climb: MAP: Cruise: RPM: ALT: IAS: MAP: OAT: RPM: Fuel pressure IAS: Coolant temp: TAS: Coolant pressure: OAT: Oil temp: Fuel pressure: Oil Pressure Coolant temp: GPM: Coolant pressure: Oil temp: Cruise: Oil Pressure: ALT: GPM: MAP: RPM: Cruise: IAS: ALT: TAS: MAP: OAT: RPM: Fuel pressure IAS: Coolant temp: TAS: Coolant pressure: OAT: Oil temp: Fuel pressure: Oil Pressure: Coolant temp: GPM: Coolant pressure: Oil temp: Switch Tanks: Oil Pressure: GPM: Flight Test- Speeds, Controls, Slow Flight</p><p>Controls: ASI Calibration – 5000’ Yaw - 5 degrees yaw: OAT: Pitch - 3 degrees up/down pitch: 180 kts IAS Roll - 5 degrees: GPS track - 0 deg GPS Groundspeed: Roll - 20 degrees: GPS track - 90 deg Trim - Pitch trim response: GPS Groundspeed: GPS track - 180 deg Speeds: GPS Groundspeed: Canard Stall: GPS track - 270 deg Weight: GPS Groundspeed:</p><p>Throttle - Increase power to maintain 150 kts IAS altitude at nose bob speed. Note GPS track - 090 deg roll/yaw response during canard stall GPS Groundspeed: GPS track - 90 deg GPS Groundspeed: Approach – GPS track - 180 deg Downwind 90 kts GPS Groundspeed: Final 80 kts GPS track - 270 deg Touch down 70 kts. GPS Groundspeed:</p><p>Gear Retraction Test 120 kts IAS IAS - 105 kts GPS track - 0 deg Gear - Retract GPS Groundspeed: Note required pitch/roll trim changes GPS track - 90 deg Cycle 3 times – leave down GPS Groundspeed: IAS 80 kts – trim to s & l GPS track - 180 deg Throttle Full power GPS Groundspeed: Climb 90 kts GPS track - 270 deg Gear: Retract GPS Groundspeed: Note pitch/roll changes Cycle 3 times – leave up 90 kts IAS Level – 90kts GPS track - 0 deg Manually lower gear GPS Groundspeed: IAS: GPS track - 90 deg GPS Groundspeed: Landing BrakeTest GPS track - 180 deg Coolant temp: GPS Groundspeed: Oil temp: GPS track - 270 deg IAS - 90 kts GPS Groundspeed: LB - Lower IAS: 70 kts IAS Coolant Temp: GPS track - 0 deg Oil temp: GPS Groundspeed: IAS 80 kts – trim to s & l GPS track - 90 deg Throttle Full power GPS Groundspeed: Climb 90 kts GPS track - 180 deg Gear: Retract GPS Groundspeed: LB: retract GPS track - 270 deg Note pitch/roll changes GPS Groundspeed: Level – 90kts Manually lower gear Compass Deviation Rudders N: E: S: W: Both Rudders deploy All electrics on: Sideslip test N: E: S: W: IAS Stability & Control</p><p>Static Longitudinal Stability: pull, pull more Dynamic Longitudinal Stability: pull, push, return Lateral Directional Stability: sideslip, Release aiIerons Static Directional Stability: yaw left & right, release rudders Spiral Stability: Bank, release</p><p>Accelerated Stall: Constant bank, reduce speed</p><p>Weight: 30 degree: IAS 45 degree: IAS 60 degree: IAS</p><p>Flutter & VNE</p><p>Tap controls, aileron, elevator, rudder</p><p>IAS: TAS IAS: Alt: TAS Alt: IAS: TAS IAS: Alt: TAS Alt: IAS: TAS IAS: Alt: TAS Alt: IAS: TAS IAS: Alt: TAS Alt: IAS: TAS IAS: Alt: TAS Alt: IAS: TAS IAS: Alt: TAS Alt: IAS: TAS IAS: Alt: TAS Alt: IAS: TAS IAS: Alt: TAS Alt: Rate of Climb / Angle of Climb</p><p>C of G Weight IAS Start End OAT Time ROC</p><p>Service Ceiling:</p><p>Alt: 10000: ROC: Alt: 12000: ROC: Alt: 14000: ROC: Alt: 16000: ROC:</p><p>Night Flight: Taxi: 30 mins Electrical load: Cockpit lighting Taxi light Landing lights Strobes Nav lights</p>