TECNAM P92 EAGLET Checklist [Glass]

□ Left Wing sump: CHECK for water and contaminants □ Left fuel filler cap: CHECK visually for desired fuel level and secure cap. □ Gascolator: DRAIN Check fuel for color, water, and contaminants. Make sure valve is closed and not leaking. □ Right Wing sump: CHECK for water and contaminants □ Right side fuel filler cap: CHECK visually for desired fuel level and secure cap. Left Wing □ Pitot tube: Remove pitot tube cover and check that the pitot tube mounted on the left wing is unobstructed. Do not blow into pitot tube. □ Left leading edge, wing skin, and strut: CHECK □ Left tank vent: CHECK for obstructions □ Left aileron: CHECK for damage, freedom of movement □ Left flap and hinges: CHECK security □ Left gear bolts: Grab gear strut and vigorously rock plane fore and aft checking gear attachment □ Left main landing gear: CHECK inflation 38 PSI, tire condition, alignment, brake condition, hydraulic leaks, and wheel bearing for damage. Fuselage: □ Antennas: Check Tail: □ Horizontal tail and tab: CHECK for damage, freedom of movement, side-to-side wiggle □ Vertical tail and rudder: CHECK for damage, freedom of movement (NOTE: do not move rudder unless nosewheel is lifted off the ground, do not touch trim tab) 06-2020 Right Wing: □ Right gear bolts: Grab gear strut and vigorously rock plane fore and aft checking gear attachment □ Right main landing gear: CHECK inflation 38 PSI, tire condition, alignment, brake condition, hydraulic leaks, and wheel bearing for damage. □ Right flap and hinges: CHECK security □ Right aileron: CHECK for damage, freedom of movement. □ Right tank vent: check for obstructions. □ Right leading edge, wing skin, and strut: CHECK Nose: □ Nose wheel strut and tire: CHECK inflation 32 PSI, tire condition, and straightness of nosewheel forks. Check wheel bearings. □ Static ports: CHECK □ Propeller and spinner condition: CHECK for nicks and security □ Oil Cooler, Radiator, Ram Air Intake: CHECK Engine: □ Foreign Objects or Leaks (oil/fuel/coolant lines): CHECK □ Coolant Reservoir Level: CHECK □ Oil Level: CHECK, Cap Secure □ Carburetor Filters: CHECK □ Engine Mounts: CHECK □ 8 Muffler Springs: CHECK □ All parts, hoses, wires secure: CHECK □ Engine Cowlings: CLOSE and LATCH □ Tow bar, chocks if any: REMOVE Starting: □ Seat position and safety belts: ADJUST □ Parking brake: SET □ Seat: WIGGLE until pins lock □ Passenger Briefing o Seat Belt use o Door Release o Emergency Equipment o Motion Sickness o Sterile Cockpit o Propeller Safety o Cockpit Resource Management Briefing (CRM) o LSA Airworthiness Certification □ Strobe lights: ON □ Fuel valves: BOTH ON □ Master switch: ON □ Fuel quantity: CHECK NOTE Compare the fuel levels read by the fuel quantity indicators with the quantity present in the tanks □ Throttle: IDLE □ Friction lock: ADJUST □ Choke: AS NEEDED □ Propeller area: “CLEAR” □ Ignition Switch: START □ Choke: OFF □ Oil Pressure: CHECK Shut engine down if oil pressure does not rise in 10 sec. □ Engine RPM: 2000 – 2500 RPM □ Avionics Master: ON □ EFIS/EMS Displays SET, as desired using Button □ Circuit Breakers: Check □ Instruments: □ Oil Pressure CHECK □ Oil temperature CHECK □ Cylinder head temp. CHECK □ Voltmeter CHECK □ Ammeter CHECK □ Fuel Pressure CHECK 06-2020 PRE-TAXI: □ Transponder (Check Code) ALT □ AWOS / ASOS / ATIS: OBTAIN □ Altimeter: SET □ Attitude Indicator: CHECK □ Directional Indicator: Compare to Magnetic Compass □ GPS: SET □ Radio: CHECK WITH UNICOM □ Briefing: Brief self or passenger on taxiways that will be used to reach the runway TAXI: □ Parking Brake: OFF □ Brakes: CHECK □ Turn Coordinator / Ball: CHECK BEFORE TAKEOFF: □ Parking Brake: ON □ Oil Temp: At least 122° F □ Throttle: 4000 RPM □ Engine instruments: CHECK • Oil Pressure 29 – 72.5 PSI • Oil temperature 122 - 230° F • Cylinder head temp. 122 - 275° F • Fuel Pressure 2.2 – 5.9 PSI • Voltmeter 13+ Volts • Ammeter Positive Charge □ Test ignition systems: • Maximum RPM drop with only one ignition 300 rpm • Max difference between LEFT or RIGHT 120 rpm □ Throttle: FULL IDLE (check for roughness) □ Throttle: 2000 RPM □ Flight controls: CHECK □ Seat belts: FASTENED □ Briefing: Brief self or passenger loss of engine contingencies (see front of checklist) HOLD SHORT LINE □ Flaps: T/O (15°) □ Fuel Pump: ON, Check Pressure □ Trim: CENTERED □ Strobe and Landing Lights: ON □ Doors: CLOSED □ Takeoff Brief: Complete □ Pattern: CHECK □ Radio: CALL □ Parking brake: OFF 06-2020 TAKE OFF: □ Taxi to line-up, □ Mag Compass and D.G.: CHECK □ Throttle: FULL NOTE Static RPM is approximately 4900 rpm □ Engine instruments: CHECK Airspeed Indicator Alive/RPM up -if not abort. □ Vr (Rotation speed): ~ 48 KIAS NOTE Rotate to takeoff attitude and accelerate to a climb speed of 60 knots with 15° Flaps □ Flaps: RETRACT (Safely airborne/300 ft □ Vy 68 KIAS CLIMB: □ Landing light: OFF □ Fuel pump: OFF □ Trim: ADJUST □ Cruise climb: 75 – 80 KNOTS CRUISE: □ Throttle: SET (5100min - 5500 RPM Max) □ Engine instruments: CHECK □ Engine instruments: CHECK • Oil Pressure 29 – 72.5 PSI • Oil temperature 122 - 230° F • Cylinder head temp. 122 - 275° F • Fuel Pressure 2.2 – 5.8 PSI • Voltmeter 13+ Volts • Ammeter Positive Charge CAUTION Normal position of the fuel selectors is both on. Check fuel balance and fuel pressure. If necessary, shut off the lower reading tank using the appropriate fuel shutoff valve. Check fuel pressure again. BE SURE THAT ONE TANK IS FEEDING THE ENGINE AT ALL TIMES! NOTE Check fuel gauges frequently with one tank shut off to prevent fuel starvation. PRE-MANEUVERS LIST: □ Clearing Turns □ Select emergency landing area □ Va – 93 KIAS EXTENDED DESCENT: □ Minimum 3000RPM □ Speed - 65-75Kt □ Engine Instruments – Monitor LANDING LIST: Check safety belts tight □ Landing light: ON □ Fuel valves: BOTH ON □ Fuel pump: ON □ Brake: OFF / Check Pressure □ Flaps: AS DESIRED GO-AROUND: □ Throttle: FULL POWER □ Pitch: Climb Attitude □ Flaps: Retract to 15 degrees - 60 KIAS Above 300 feet: □ Flaps: UP, Climb Speed – 68 KIAS □ Trim: Adjust □ Maneuver to the non-pattern side of runway 06-2020 AFTER LANDING: □ Clear Runway: RADIO CALL □ Landing Light: OFF □ Flaps: UP □ Fuel Pump: OFF □ Trim: CENTERED PARKING: □ Parking Brake: ON □ Strobe Lights: ON □ Other Lights: OFF □ Flaps: UP □ Total Hours: RECORD □ Avionics Master switch: OFF □ Fuel Pump: OFF □ Ignition Switch: OFF □ Master switch: OFF □ One or Both Fuel Valves: OFF □ Trash - Remove □ Chocks : INSTALL □ Parking brake: OFF (for extended parking) □ Pitot tube cover: INSTALL □ Control locks: INSTALL □ Aircraft: TIED DOWN □ Checklist in Airplane □ Doors: CLOSED □ Key Returned to Box. CLOSED PATTERN OPS CHECK LISTS HOLD SHORT LINE □ Engine Instruments: CHECK □ Fuel quantity CHECK □ Trim: Centered □ Fuel Valves: BOTH ON □ Fuel Pump: ON □ Flaps: T/O (15°) □ Doors: CLOSED □ Takeoff Brief: REVIEW □ Pattern: CHECK □ Radio: CALL CLIMB: □ Rotate 48 KIAS □ Accelerate 60 KIAS □ Flaps: RETRACT (300 ft) □ Establish Vy clean: 68 KIAS □ Trim: ADJUST LANDING: Check safety belts tight □ Fuel Valves: BOTH ON □ Fuel Pump: ON □ Brake: OFF / check pressure □ Flaps: AS DESIRED AFTER LANDING: □ Clear Runway: RADIO CALL □ Flaps: T/O (15°) □ Trim: CENTERED 06-2020 EMERGENCY PROCEDURES: ENGINE FIRE DURING START □ Continue Cranking with Starter □ Choke PUSH OFF □ Throttle FULL OPEN If fire extinguished, shut down and inspect. If Fire Persists: □ Fuel valves: OFF □ Electric fuel pump: OFF □ Ignition Switch: OFF □ Master switch: OFF □ Parking brake: SET □ Escape rapidly from the aircraft ENGINE FAILURE DURING TAKEOFF RUN □ Throttle: IDLE □ Brakes: APPLY AS NEEDED After stopped □ Ignition Switch: OFF □ Master switch: OFF □ Fuel selector valves: OFF ENGINE FIRE DURING TAKEOFF RUN □ Throttle: IDLE □ Brakes: AS NEEDED After stopped □ Fuel Valves: OFF □ Electric fuel pump: OFF □ Cabin heating: OFF □ Ignition Switch: OFF □ Master switch: OFF □ Parking brake: SET □ Escape rapidly from the aircraft ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF □ NOSE DOWN/Pitch for best glide 68 kts □ Find a suitable place on the ground to land safely. The landing should be planned straight ahead with only small changes in direction not exceeding 45° to the left or 45° to the right □ Flaps: AS REQUIRED □ Ignition Switch: OFF □ Fuel selector valves: OFF When airspeed no longer needed □ Master switch: OFF ENGINE FAILURE INFLIGHT □ Pitch for best glide speed: 68 KIAS □ Fuel Valves: BOTH ON □ Electric Fuel Pump: ON □ In-flight Engine re-start or forced landing NOTE Glide ratio is 12.8 therefore with 1000 ft of altitude; it is possible to cover ~2 nautical miles in zero wind conditions. IN-FLIGHT ENGINE RESTART – IF TIME PERMITS □ Fuel Valves: BOTH ON □ Electric Fuel Pump: ON □ Throttle: MIDDLE POSITION □ Master Switch: ON □ Ignition switch: START, then both □ If the restart fails: Procedure for a Forced Landing Without Engine Power: APPLY □ If engine starts: Land as soon as possible. FORCED LANDING WITHOUT ENGINE POWER □ Establish: 68 KIAS □ Locate suitable terrain, land into wind □ Radio / Transponder: 121.5 / 7700 □ ELT: Activate near ground □ Fuel selector valves: OFF □ Electric fuel pump: OFF □ Ignition Switch: OFF □ Safety belts: TIGHTEN □ Doors: UNLATCHED □ Flaps: AS NECESSARY When airspeed no longer needed □ Master switch: OFF 06-2020 DITCHING □ Seats belts: TIGHTEN □ MAYDAY 121.5 / 7700 □ Flaps: FULL DOWN □ Fuel selector: BOTH OFF □ Electrical fuel pump: OFF □ Ignition: BOTH OFF □ Doors: PROP OPEN When airspeed no longer required □ Master switch: OFF □ Ditch with nose high attitude ENGINE FIRE IN-FLIGHT □ Cabin heat: OFF □ Fuel Valves: OFF □ Electric fuel pump: OFF □ Throttle: FULL IN until the engine stops running □ Cabin vents: OPEN □ Pitch for 130 KIAS to snuff out flames □ Employ slip to keep flames away from firewall Do not attempt an in-flight restart □ Procedure for a Forced Landing Without Engine Power: APPLY ELECTRICAL FIRE IN CABIN IN FLIGHT □ Master switch: OFF □ Cabin vents: OPEN □ Emergency descent and Procedure for a Power-On Forced Landing. □ If flaps needed, Master switch: ON □ Flaps: AS REQUIRED □ Master switch: OFF CABIN FIRE DURING FLIGHT □ Cabin heat: OFF □ Cabin vents: OPEN □ Doors: OPEN, if necessary □ Master switch: OFF □ Emergency descent and Procedure for a Power-On Forced Landing. □ If flaps or airspeed needed, Master switch: ON □ Flaps: AS REQUIRED □ Master switch: OFF POWER-ON FORCED LANDING □ Descent: ESTABLISH □ Airspeed: 68 KIAS □ Landing area: SELECT □ Safety belts: TIGHTEN □ Doors: UNLATCH Landing assured: □ Flaps: AS REQUIRED □ Fuel selector valves: OFF □ Electric fuel pump: OFF □ Ignition Switch: OFF When airspeed no longer required □ Master switch: OFF IRREGULAR ENGINE RPM □ Throttle: CHECK □ Engine gauges: CHECK □ Fuel quantity indicators: CHECK □ Electric fuel pump: ON □ Fuel Valves: BOTH ON If the engine continues to run irregularly, land as soon as possible. LOW FUEL PRESSURE (below red line limit) □ Fuel quantity indicators: CHECK □ Electric fuel pump: ON □ Fuel Valves: BOTH ON If the fuel pressure continues to be low, land as soon as possible. 06-2020 LOW OIL PRESSURE □ Oil temperature: CHECK □ If oil temperature is stable within the green arc: LAND as soon as possible □ If oil temp is increasing: LAND as soon as possible and be alert for impending engine failure TRIM SYSTEM FAILURE In case the trim control should not respond: □ LH/RH switch: CHECK for correct position □ Circuit breakers: CHECK, reset one time □ Airspeed: Adjust speed to control aircraft without excessive stick force □ Land aircraft as soon as possible, flaps up. Note: If trim should fail in cruise position, deploying flaps after slowing the plane may reduce trim pressure. LANDING WITH A FLAT TIRE □ Apply rudder and brakes to stay on runway □ Make radio call to UNICOM and inbound traffic about closed runway □ Push plane off runway UNINTENTIONAL FLIGHT INTO ICING CONDITIONS □ Get away from icing conditions by changing altitude or direction of flight in order to reach an area with warmer external temperature. □ Increase rpm to avoid ice formation on propeller blades. □ Pitot heat: ON □ Cabin heat: ON □ Land as soon as practical □ Do NOT use flaps WARNING In case of ice formation on wing leading edge, stall speed may increase. NOTE It may be necessary to slip the plane on landing to see out. RECOVERY FROM UNINTENTIONAL SPIN □ Reduce the power to idle □ Position the ailerons to neutral □ Apply full opposite rudder against the rotation □ Apply positive, brisk, forward stick (forward of neutral) to break stall. □ After spin rotation stops, neutralize the rudder. □ Begin applying back-elevator pressure to raise the nose to level flight. LOST PROCEDURES □ Climb and Circle to better see prominent landmarks □ Conserve fuel □ Communicate with ATC (121.5) □ Comply with ATC instructions