TECNAM P2006T CHECK LIST

TECNAM P-2006T · Checklist

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Overview

The Tecnam P-2006T checklist provides a comprehensive guide for pre-flight and post-flight checks, ensuring the aircraft is in proper condition before and after each flight. It includes detailed inspection procedures for various aircraft components and systems.

Complete aircraft check required before each flight.
Includes external and cockpit inspections.
Check for integrity of doors, landing gear, and propellers.
Verify fluid levels and check for leaks.
Perform visual inspections of wings, lights, and antennas.
Ensure all inspection doors are closed.
Check safety belts and baggage positioning.
Follow specific procedures for engine start.

Document

Source

Originally published by adriana-aviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at adriana-aviation.com

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Document details

Type: Checklist
Year: 2022
File size: 1.3 MB
Publisher: adriana-aviation.com
Language: en

About this document

What is the TECNAM P2006T CHECK LIST?

The TECNAM P2006T CHECK LIST is a checklist for the TECNAM P-2006T, dated 2022.

Where does the TECNAM P2006T CHECK LIST come from?

This copy of the TECNAM P2006T CHECK LIST was originally published by adriana-aviation.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the TECNAM P2006T CHECK LIST published?

The TECNAM P2006T CHECK LIST — the TECNAM P-2006T checklist on file — is dated 2022.

Documentation completeness

2/7

Most owners only have the POH. Here's the essential set for the TECNAM P-2006T.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More TECNAM P-2006Tmanuals & documents

In this document

Pre-Flight Check

A complete aircraft check including external and cockpit inspections, focusing on various components such as doors, landing gear, and engines.

Post-Flight Checks

Similar to pre-flight checks, ensuring the aircraft remains in good condition after landing.

Before Engine Starting

Checklist items to complete before starting the engine, including engaging the parking brake and checking flight controls.

Engine Start Procedure

Step-by-step instructions for starting the left and right engines, including checks for oil pressure and RPM.

Visual Inspections

Detailed visual inspection requirements for various aircraft parts, including wings, landing gear, and propellers.

Fluid Checks

Instructions for checking and replenishing oil and coolant levels, as well as inspecting for leaks.

Safety notes

Ensure all inspection doors are closed before flight.
Check for hydraulic fluid leakage in landing gear.
Verify coolant levels before the first flight of the day.
Drain gascolator for water and sediment before flight.
Check for obstructions in air intake filters.
Use protective caps on Pitot tubes when not in use.

Full document text

Tecnam P2006 01 08 2022 rev 1 1 TECNAM P2006T CHECK LIST 01 08 2022 rev1 Tecnam P2006 01 08 2022 rev 1 2 PRE-FLIGHT CHECK – AIRCRAFT WALK-AROUND Before each flight, it is necessary to carry out a complete aircraft check comprising an external inspection followed by a cockpit inspection as below detailed. Technical log book Training of record keeping in the technical logbook 1 Pilot door and cabin Check door for integrity. Turn ON the Master Switch and check Stall Warning switch for operation and condition; check lighting of landing/Taxi/Nav/Strobe lights, then turn OFF the Master Switch. 2 Left main landing gear Check fuselage skin status, tire status (cuts, bruises, cracks and excessive wear), slippage markers integrity, gear structure and shock absorber, hoses, gear door attachments and gear micro-switches. There should be no sign of hydraulic fluid leakage. 3 Wheel chock Remove if employed 4 Propeller and spinner The propeller blades and spinner should be free of cracks, nicks, dents and other defects and should rotate freely. Check fixing and lack of play between blades and hub. 5 Left engine nacelle Perform following inspections: a) Check the surface conditions. b) Nacelle inlets and exhausts openings must be free of obstructions. If inlet and outlet plugs are installed, they should be removed. c) Check radiators. There should be no indication of leakage of fluid and they have to be free of obstructions. d) Only before the first flight of a day: (1) Verify coolant level in the expansion tank, replenish as required up to top (level must be at least 2/3 of the expansion tank). (2) Verify coolant level in the overflow bottle through the slot under the nacelle: level must be between min. and max. mark. Replenish if required removing the upper cowling; after that, install upper cowling checking for interferences with radiators (3) Turn the propeller by hand to and fro, feeling the free rotation of 15°or 30° before the crankshaft starts to rotate. If the propeller can be turned between the dogs with practically no friction at all further investigation is necessary. Turn propeller by hand in direction of engine rotation several times and observe engine for odd noises or excessive resistance and normal compression. Tecnam P2006 01 08 2022 rev 1 3 e) Check oil level and replenish as required. Prior to oil check, switch off both ignitions circuits and turn the propeller by hand in direction of engine rotation several times to pump oil from the engine into the oil tank, or let the engine idle for 1 minute. This process is finished when air is returning back to the oil tank and can be noticed by a murmur from the open oil tank. Prior to long flights oil should be added so that the oil level reaches the “max” mark. f) Drain off Gascolator for water and sediment (drain until no water comes off). Then make sure drain valve is closed. g) Check drainage hoses clamps h) Verify all parts are fixed or locked. i) Verify all inspection doors are closed. 6 Air induction system Check engine air inlet for integrity and correct fixing. The air intake filter must be free of obstructions. 7 Left fuel tank Check that the refuelling port cap is properly secured, then perform the fuel tank sump drainage operating the related valve which, after operation, must be checked closed. Fuel must checked for water and sediment. Verify the tank vent outlet is clear. 8 Landing and taxi lights Visual inspection 9 Left wing leading edge Visual inspection. Check cabin ventilation inlet and carburettor heating inlet for condition and free of obstruction. Check stall strip 10 Left wing top and bottom panels Visual inspection 11 Left winglet, nav and strobe lights, static discharge wick Check for integrity and fixing 12 Left aileron and balance mass Visual inspection, remove tie-down devices and control locks if employed. 13 Left Flap and hinges Visual inspection 14 Left static port Remove protective cap – Visual inspection 15 Antennas Check for integrity 16 Gear pump, external power and battery compartment Check emergency landing gear extension system pressure (low pressure limit: 20 bar), external power and battery compartments closure. 17 Horizontal and vertical empennage and tabs. Static discharge wicks. Check the actuating mechanism of control surfaces and the connection with related tabs. Check wicks for integrity. Remove tiedown device if employed. 18 Stabiliser leading edge Check for integrity 19 Fuselage top and bottom skin Visual inspection 20 Right static port Remove protective cap – Visual inspection 21 Right Flap and hinges Visual inspection 22 Right aileron and balance weight Visual inspection, remove tie-down devices and control locks if employed. 23 Right winglet, nav and strobe lights, static discharge wick Check for integrity and fixing and lighting 24 Right wing top and bottom panels Visual inspection 25 Right wing leading edge Visual inspection. Check cabin ventilation inlet and carburettor heating inlet for condition and free of obstruction. Check stall strip. 26 Right fuel tank Tecnam P2006 01 08 2022 rev 1 4 Check that the refuelling port cap is properly secured, then perform the fuel tank sump drainage operating the related valve which, after operation, must be checked closed. Fuel must checked for water and sediment. Verify the tank vent outlet is clear. 27 Propeller and spinner: The propeller blades and spinner should be free of cracks, nicks, dents and otherdefects and should rotate freely. Check fixing and lack of play between blades and hub. 28 Right engine nacelle Apply check procedure reported in the walk-around station 5 and 6 29 Passenger door and cabin Check door for integrity. Check safety belts for integrity and baggage for correct positioning and fastening. Check ditching emergency exit safety lock. Check passengers ventilation ports for proper setting. 30 Right main landing gear Apply check procedure reported in the walk-around Station 2 31 Wheel chock Remove if employed

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32 Bottom fuselage antennas Check for integrity 33 Right cabin ram-air inlet Visual inspection 34 Right Pitot tube Remove protective cap and check for any obstruction 35 Nose landing gear Check tire status (cuts, bruises, cracks and excessive wear),slippage markers integrity, gear structure and retraction mechanism, shock absorber and gear doors attachments. There should be no sign of hydraulic fluid leakage. 36 Radome Check for integrity 37 Radome access door Visual inspection 38 Left Pitot tube Remove protective cap and check for any obstruction 39 Left cabin ram-air inlet Visual inspection POSTFLIGHT CHECKS Pilot door and cabin Check door for integrity. 1 Left main landing gear Check fuselage skin status, tire status (cuts, bruises, cracks and excessive wear), slippage markers integrity, gear structure and shock absorber, hoses, gear door attachments and gear micro-switches. There should be no sign of hydraulic fluid leakage. 2 Wheel chocks Use if needed 3 Aileron lock The propeller blades and spinner should be free of cracks, nicks, dents and other defects and should rotate freely. Check fixing and lack of play between blades and hub. 4 Left engine nacelle Perform following inspections: a) Check the surface conditions. b) Nacelle inlets and exhausts openings must be free of obstructions. If inlet and outlet plugs are installed, they should be removed. c) Check radiators. There should be no indication of leakage of fluid and they have to be free of obstructions. g) Check drainage hoses clamps h) Verify all parts are fixed or locked. i) Verify all inspection doors are closed. 5 Air induction system Check engine air inlet for integrity and correct fixing. The air intake filter must be free of obstructions. 6 Landing and taxi lights Visual inspection. Tecnam P2006 01 08 2022 rev 1 5 7 Left wing leading edge Visual inspection. Check cabin ventilation inlet and carburettor heating inlet for condition and free of obstruction. Check stall strip. 8 Left wing top and bottom panels Visual inspection 9 Left winglet, nav and strobe lights, static discharge wick Check for integrity and fixing 10 Left aileron and balance mass Visual inspection, remove tie-down devices and control locks if employed. 11 Left Flap and hinges Visual inspection 12 Left static portVisual inspectionand use protective cap 13 Antennas Check for integrity 14 Gear pump, external power and battery compartment Check emergency landing gear extension system pressure (low pressure limit: 20 bar), external power and battery compartments closure. 15 Horizontal and vertical empennage and tabs. Static discharge wicks. Check the actuating mechanism of control surfaces and the connection with related tabs. Check wicks for integrity. Remove tiedown device if employed. 16 Stabilator leading Edge Check for integrity 17 Fuselage top and bottom skin Visual inspection 18 Right static port Visual inspection and use protective cap 19 Right Flap and hinges Visual inspection 21 Right aileron and balance weight Visual inspection, remove tie-down devices and control locks if employed 22 Right winglet, nav and Strobe lights, static discharge wick Check for integrity and fixing and lighting 23 Right wing top and bottom panels Visual inspection 24 Right wing leading Edge Visual inspection. Check cabin ventilation inlet and carburettor heating inlet for condition and free of obstruction. Check stall strip. 25 Propeller and spinner The propeller blades and spinner should be free of cracks, nicks, dents and other defects and should rotate freely. Check fixing and lack of play between blades and hub. 26 Right engine nacelle Apply check procedure reported in the walkaround station 5 and 6 27 Passenger door and cabin Check door for integrity. Check safety belts for integrity and baggage for correct positioning and fastening. Check ditching emergency exit safety lock. Check passengers ventilation ports for proper setting. 28 Right main landing gear Apply check procedure reported in the walkaround 29 Wheel chock Use if needed 30 Bottom fuselage antennas Check for integrity 31 Right cabin ram-air inlet Visual inspection 32 Right Pitot tube Check for any obstructionand use protective cap 33 Nose landing gear Check tire status (cuts, bruises, cracks and excessive wear), slippage markers integrity, gear structure and retraction mechanism, shock absorber and gear doors attachments. There should be no sign of hydraulic fluid leakage 34 Radome Check for integrity 35 Radome access door Visual inspection 36 Left Pitot tube Check for any obstruction and use protective cap 37 Left cabin ram-air inlet Visual inspection Tecnam P2006 01 08 2022 rev 1 6 BEFORE ENGINE STARTING PREFLIGHT CHECK COMPLETE PARKING BRAKE ENGAGE FLIGHT CONTROLS CHECK DOORS CLOSED SEAT & SEATBELTS ADJUST THROTTLE FRICTION SET LANDING GEAR DOWN MASTER ON NAV LIGHT ON FUEL QUANTITY CHECK ON CONTROLLED AIRFIELD: AUDIO PANEL, HORIZ, PFD BREAKERS IN WX INFO/ ATIS OBTAIN FLIGHT CLEARANCE OBTAIN START UP CLEARANCE OBTAIN AUDIO PANEL,HORIZ, PFD BREAKERS OUT FLAPS UP FUEL SELECTORS CHECK L-L/R-R FILD LH, RH OFF AVIONICS LH, RH OFF CROSS BUS LH, RH OFF THROTTLE LH, RH IDLE CARB. HEAT LH, RH OFF PROP. LEVERS LH, RH FORWARD CHOKE LH, RH DOWN (COLD) Tecnam P2006 01 08 2022 rev 1 7 ENGINE START START RELAY BREAKER IN (LEFT) FUEL PUMP ON, ~ 4 PSI (LEFT) PROPELLER AREA CLEAR (LEFT) ENGINE IGNITION BOTH ON (LEFT) ENGINE START (LEFT) OIL PRESSURE CHECK during 10 sec. (LEFT) RPM 1000 - 1200 (LEFT) CHOKE UP RPM adjust (LEFT) FIELD ON (LEFT) AVIONICS ON (LEFT) CROSS BUS ON (LEFT) AMPS, VOLTS Select, Press & CHECK (LEFT) FUEL PUMP OFF Repeat all (LEFT) items of engine start Procedure for (RIGHT) engine ALTERNATE HORIZON PULL TO CAGE AND HOLD ALL BREAKERS IN CHECK HEADSET ON AUTOPILOT MASTER ON & CHECK ALERTS WARNING ON PFD ANNUNCIATOR PNL CHECK FIRE DETECTOR PUSH CHECK ACOUSTIC + PFD MSQ AUDIO, COM, NAV, ALT SET BEFORE TAXI XPDR CODE GND SET AHRS PFD & MFD (NO CROSSES) CHECK FUEL SELECTORS CROSSFEED L-R, R-L FUEL PRESSURE LH, RH MONITOR OIL TEMPERATURE LH, RH MINIMUM YELLOW Tecnam P2006 01 08 2022 rev 1 8 TAXI TAXI CLEARANCE OBTAIN OFF BLOCK TIME NOTE TAXI LIGHT ON BRAKES OFF, TEST FLIGHT INSTRUMENTS CHECK RUN UP PARKING BRAKE SET TAXI LIGHT OFF ENGINE INSTRUMENTS CHECK RPM LH, RH 1650 ENGINE IGNITIONS LH, RH DROPS NOT MORE THAN 130 RPM, DIFFERENCE UP TO 50 RPM LEFT PROPELLER FEATHERING CHECK (3X) DROPS 200 RPM RIGHT PROPELLER FEATHERING CHECK (3X) DROPS 200 RPM BOTH CARBURATOR HEATS ON DROPS 50 RPM THROTTLE LH, RH IDLE BOTH CARBURATOR HEATS OFF CHECK RPM INCREASE RPM LH, RH 1000 - 1200 Tecnam P2006 01 08 2022 rev 1 9 BEFORE TAKE OFF (Clearance, WX) LEFT FUEL SELECTOR LEFT TANK RIGHT FUEL SELECTOR RIGHT TANK FUEL PRESSURE LH, RH MONITOR FUEL QUANTITY CHECK BOTH ALTIMETERS SET & COMPARE FLAPS T/0 PITH, RUDDER TRIMS SET NEUTRAL TAKE OFF BRIEFING PERFORM* ALL FREQUENCIES COMM, NAV & ALT SEL CHECK & SET COMPASS & HDG BUG SET & COMPARE MFD OBS OR FLIGHT PLAN SET LINE UP (Departure/ line up Clearance) STROBES ON PARKING BREAK RELEASE RUNWAY, APP SECTOR FREE ALL EXTERNAL LIGHTS ON FUEL PUMPS ON TRANSPONDER ALT PITOT HEAT AS REQUIRED ALERTS, WARNINGS NONE Tecnam P2006 01 08 2022 rev 1 10 TAKE OFF ALL LEVERS FORWARD ENGINE INSTRUMENTS GREEN ROTATE MIN 64 KIAS POSITIVE CLIMB GEAR UP BRAKES APLLY CLIMB (SPEED 80-85 KIAS) ABOVE 200 FEET AGL/ SAFE ALTITUDE FLAPS UP MANIFOULD PRESSURE 25 INCHES RPM BORDER/ 2250 LANDING LIGHTS OFF FUEL PUMPS OFF *ALTIMETERS SETTING (IF HIGHER THEN TRANS ALT) STD CRUISE MANIFOULD PRESSURE 21 INCHES RPM 2100 ENGINES PARAMETERS CHECK TRIMES ADJUST CARB HEAT AS REQUIRED FUEL BALLANCE AND CROSS CHECK DESCEND MANIFOULD PRESSURE AS REQUIRED RPM AS REQUIRED AIRSPEED BELOW VNO CARB. HEAT AS REQUIRED ALTIMETER SETTING QNH Tecnam P2006 01 08 2022 rev 1 11 APPROACH (APP Clearance RECEIVED) APPROACH BRIEFING COMPLETED LANDING LIGHTS ON FUEL PUMPS ON BEFORE LANDING SPEED < 93 KIAS LANDING GEAR DOWN FUEL PUMPS ON LANDING LIGHTS ON CARB. HEAT ON / AS REQUIRED 3 GREEN CONFIRMED FINAL CHECK CLOSED LOOP LANDING GEAR DOWN 3 GREEN PROPELLER FULL FORWARD/ MOVE CARB. HEAT ON / AS REQUIRED FLAPS TAKE OFF/ FULL LANDING LIGHTS ON FUEL PUMPS/ PFD ON GO AROUND PROPELLER LEVER FORWARD THROTTLE LEVEL FORWARD FLAPS TAKE OFF POSITIVE CLIMB SPEED OVER 62 KIAS GAIN TO Vx OR Vy GEAR UP FLAPS UP (STEP BY STEP) Tecnam P2006 01 08 2022 rev 1 12 AFTER LANDING FLAPS UP FUEL PUMPS OFF PITOT HEAT OFF AFTER VACATING STROBES OFF LANDING LIGHTS *DURING DAY OFF TAXI LIGHT ON TRANSPONDER GND SHUTDOWN PARKING BRAKE SET TAXI LIGHT OFF AUTOPILOT MASTER OFF LH, RH AVIONICS OFF LH, RH FIELDS OFF LH, RH CROSS BUS OFF LH, RH IGNITION OFF NAV. LIGHTS OFF ON BLOCK TIME NOT MASTER SWITCH OFF START RELAY BREAKER OUT AUDIO PANEL, HORIZON, PFD, BREAKERS OUT POST-FLIGHT CHECK COMPLETE Tecnam P2006 01 08 2022 rev 1 13 ENGINE SECURE /stopped engine/ Throttle Lever IDLE Propeller Lever FEATHER Desired Engine Ignition OFF Fuel Selector OFF Electrical Fuel Pump OFF Desired Field OFF Operative Engine RPM ADJUST ENGINE START IN AIR Throttle Lever IDLE Carburetor Heat ON (if required) Propeller Lever FORWARD Choke OFF Throttles and RMP ADJUST Eng. Ignition Switches BOTH ON Fuel Selector ON Desired Field OFF Pitot Heat OFF Stand By Instruments CHECK Desired Cross Buss OFF LH,RH Avionics BOTH OFF Fuel Pump ON (4 psi) Start Button PUSH > 5 sec Fuel Pump OFF Desired Cross Buss ON Desired Field ON LH,RH Avionics BOTH ON If Volt Buss High, counter field RESET COM Frequency CHECK CHT Temperature MONITOR TRAINING ENGINE FAIL TRAINING Propeller Lever FORWARD Throttle Lever FORWARD Landing gear UP Flaps Up Identify >> >> Verify Tecnam P2006 01 08 2022 rev 1 14

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