Limitaciones y Emergencias Tecnam P2012 TRAVELLER

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ED 1 ABR 2026 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” “TECNAM P2012, TRAVELLER” “CC–DAP AEROVÍAS DAP” A.- OPERATING LIMITATIONS 2.- Fuel (U.S. GAL) Type to Use Total Capacity Usable Fuel Maximum Fuel Unbalance 1.- Limitations (KIAS) Va Vne Vno Vfe (flap T/O) Vfe (flap LAND) Vmc (flap T/O) Vmc (flap LAND) Vx (flap UP) Vx (flap T/O) Vy (flap UP) Vy (flap T/O) Vsse Vxse Vyse Vref LAND Max Cross Wind 3.- Weights (LBS) Maximum TAKE-OFF Máximum Landing Maximum Baggage NOSE Maximum Baggage REAR Engine Operating Limitations Reason HP o BHP Maximum RPM Cylinder Head Temperature (°F) Maximum Normal Oil Temperature (°F) Maximum Normal Oil Pressure (PSI) Maximum Minimum ED 1 ABR 2026 B.- EMERGENCIES PROCEDURES 1. SMOKE OR FIRE 1.1 Engine Fire on the Ground 1. Parking brake 2. Cabin air system 3. Fuel selectors 4. Fuel pumps 5. Throttle Levers 6. Mixture levers 7. Ignition switches 8. All electric / light switches 9. Emergency evacuation 1.2 Engine Fire during Take-Off Run If engine fire occurs before rotation: ABORT TAKE OFF 1. Throttle Levers 2. Rudder 3. Brakes With aircraft stopped: 4. Parking brake 5. Cabin air system 6. Fuel selectors 7. Fuel pumps 8. Throttle Levers 9. Mixture Levers 10. Ignition switches 11. All electric / light switches 12. Emergency evacuation ED 1 ABR 2026 1.3 Engine Fire after Take-Off If engine fire occurs immediately after becoming airborne: 1. Abort on the runway if possible When aircraft is safely stopped: 2. Perform “Engine Fire on the ground” procedure If the decision is taken to continue take-off, take into account the time and height loss to feather the propeller. If engine fire occurs after rotation: 1. Throttle Levers 2. Propeller Levers 3. Mixture Levers 4. Heading 5. Attitude 6. Cabin air system 7. Affected engine If affected engine is inoperative: a. Inoperative Engine Throttle Lever b. Inoperative Propeller Lever At safe altitude an airspeed: 8. Flaps 9. Affected Engine 10. Airspeed 11. Land as soon as possible applying one engine inoperative landing procedure. ED 1 ABR 2026 1.4 Engine Fire in Flight 1. Attitude 2. Affected engine 3. Heading 4. Cabin air system 5. Land as soon as possible applying one engine inoperative landing procedure. 1.5 Electrical Smoke in Cabin on the Ground 1. All electric / light switches 2. Cabin air system 3. Fuel selectors 4. Fuel pumps 5. Throttle levers 6. Mixture levers 7. Ignition switches 8. Parking brake 9. Emergency evacuation 1.6 Electrical Smoke or Fire in Cabin during Flight 1. Cockpit ventilation 2. Cabin air system 3. Attain VMC conditions as soon as possible In case of visible fire: 4. Direct the fire extinguisher toward the base of flame ED 1 ABR 2026 2. EMERGENCY EVACUATION 2.1 On Ground Check: 1. Parking brake 2. Throttle Levers 3. Mixture Levers 4. Fuel selectors 5. Fuel pumps 6. Ignition switches 7. All electric / light switches Once aircraft is secured, perform the following actions: 8. Seat belts 9. Headphones 10. Emergency doors (use the emergency door opening system) 11. Escape away from flames/hot engine compartment/spilling fuel tanks/hot brakes/propellers 3. IN FLIGHT INOPERATIVE ENGINE SECUING PROCEDURES At safe airspeed and keeping control using rudder and ailerons: 1. Throttle lever 2. Propeller lever 3. Mixture lever 4. Fuel selector 5. Fuel pump 6. Ignition switches 7. FIELD switch 8. Perform load shedding following information and procedure of §§3.1-3.2, as possible. ED 1 ABR 2026 4. ONE ENGINE INOPERATIVE PROCEDURES 4.1 Engine Failure during Take-Off Run If engine fails before rotation: ABORT TAKE OFF 1. Throttle levers 2. Rudder 3. Brakes 4.2 Engine Failure after Take-Off If engine fails immediately after becoming airborne: 1. Abort on the runway if possible. If the decision is taken to continue the take-off, take into account the time and height loss to feather the propeller. If takeoff is continued: 1. Throttle Levers 2. Propeller Levers 3. Mixture Levers 4. Heading 5. Attitude 6. Affected engine 7. Affected engine ED 1 ABR 2026 At safe altitude and airspeed: 8. Affected Engine Throttle lever 9. Affected Engine Propeller lever 10. Flaps 11. Airspeed 12. Affected engine 13. Land as soon as possible applying one engine inoperative landing procedure. 4.3 Engine Failure in Flight 1. Heading 2. Attitude 3. Affected engine 4. Affected engine 5. RECOVERY FROM UNINTENTIONAL SPIN 1. Throttle levers 2. Rudder 3. Ailerons 4. Control wheel As rotation stops: 5. Flaps 6. Rudder 7. Attitude 8. Throttle levers ED 1 ABR 2026 6. STALL RECOVERY At the first indication of stall, as for example uncommanded lateral motion or pitch down, buffeting, artificial stall waring (aural or CAS message): 1. Autopilot 2. Pitch 3. Power 4. Attitude 5. Return to the desired flight path. 7. Autopilot Emergency Procedures 7.1 Autopilot Hardover Or Failure To Hold The Selected Heading In case of A/P hardover or failure to hold selected heading, apply following procedure: Accomplish items 1 and 2 simultaneously: 1. Airplane control wheel 2. AP DISC switch 3. AP MASTER switch 4. AP circuit breaker 7.2 Electrical Trim Malfunction In case of Electric Trim malfunction (either in AP Autotrim mode ore when manually operated through the Manual Electric Trim Switch), apply following procedure: 1. AP DISC switch 2. TRIM DESC switch 3. TRIM circuit breaker 4. AP DISC switch ED 1 ABR 2026 7.3 Engine Failure During Autopilot Operation 1. Control wheel/Rudder pedals 2. AP DISC switch 3. AP MASTER switch 4. Engine failure in flight procedure