Normal Check List P2006T

TECNAM P-2006T · Checklist

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Overview

This document is a normal checklist for the Tecnam P-2006T aircraft, detailing the procedures for pre-flight inspections, engine starting, taxiing, and takeoff preparations. It includes specific checks for both external and cockpit components to ensure safety and operational readiness.

Perform thorough external walkaround checks before flight.
Ensure all doors are closed and locked.
Check fuel quantity and quality before starting engines.
Verify engine parameters during startup.
Conduct pre-taxi and pre-takeoff checks for safety.
Monitor engine oil temperature and pressure during operations.
Ensure avionics are off during engine start to prevent damage.
Check that all safety belts are fastened before taxiing.

Document

Source

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

View original at skyservices-flightacademy.com

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Document details

Type: Checklist
Year: 2020
File size: 416 KB
Publisher: skyservices-flightacademy.com
Language: en

About this document

What is the Normal Check List P2006T?

The Normal Check List P2006T is a checklist for the TECNAM P-2006T, dated 2020.

Where does the Normal Check List P2006T come from?

This copy of the Normal Check List P2006T was originally published by skyservices-flightacademy.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Normal Check List P2006T published?

The Normal Check List P2006T — the TECNAM P-2006T checklist on file — is dated 2020.

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

External Walkaround

Inspect the aircraft's exterior, including doors, landing gear, propellers, engine nacelles, fuel tanks, and wings for integrity and proper function.

Cockpit Inspection

Check that the parking brake is engaged, weight and balance are within limits, and all necessary equipment is on board.

Engine Starting

Follow specific procedures for starting both the right and left engines, including checks for oil pressure and RPM.

Before Taxiing

Ensure engines are warmed up, and all necessary lights and instruments are operational before taxiing.

Taxiing

Monitor fuel selectors, pressure, and perform checks on flight and engine instruments during taxi.

Before Takeoff

Engage the parking brake, check fuel selectors, engine parameters, and perform propeller governor checks.

Safety notes

Ensure area around engine propeller disc is clear before starting.
Avionics switches must be off during engine starting to prevent damage.
Do not cause prop speed drop below 1150 RPM in any case.
Check for water and sediment in fuel before flight.
Verify that all inspection doors are closed before flight.
Check emergency landing gear extension system pressure.

Full document text

NORMAL CHECK LIST P2006T NORMAL CHECK LIST P2006T Edizione3 Rev 0 del 01 Aprile 2020 1 EXTERNAL WALKAROUND 1 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 turnOFF 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. 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 tie-down device if employed. 18 Stabilator 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 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 other defects and should rotate freely. Check fixing and lack of play between blades and hub. 28 Right engine nacelle Apply as reported forstation 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 as reported for Station 2 31 Wheel chock Remove if employed 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 (cuts, bruises, cracks and excessive wear), slippage markers integrity, gear structure and retraction mechanism, shock absorber and gear doors attachments. Check no sign of hydraulic fluid leakage. 36 Radome

Show full text

Check for integrity; 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 EXTERNAL WALKAROUND COMPLETED COCKPIT INSPECTION 1 PARKING BRAKE CHECK ENGAGED 2 AFM CHECK ON BOARD 3 WEIGHT AND BALANCE CHECK WITHIN LIMITS 4 FLIGHT CONTROLS REMOVE SEAT BELT USED AS LOCK 5 SEAT ADJUST AS REQUIRED 6 SEAT BELT FASTENED 7 PASSENGER BRIEFING COMPLETED 8 DOORS CLOSED AND LOCKED 9 LANDING GEAR CONTROL KNOB CHECK DOWN 10 BREAKERS ALL IN 11 MASTER SWITCH ON 12 FUEL QUANTITY CHECK 13 RH FUEL SELECTOR RIGHT 14 LH FUEL SELECTOR LEFT 15 RH ELECTRICAL FUEL PUMP ON CHECK FUEL PRESSURE GAUGE CORRECT OPERATION & ADVISORY LIGHT ON 16 RH ELECTRICAL FUEL PUMP OFF CHECK PRESSURE DECREASED AT ZERO 17 LH ELECTRICAL FUEL PUMP ON CHECK FUEL PRESSURE GAUGE CORRECT OPERATION & ADVISORY LIGHT ON 18 LH ELECTRICAL FUEL PUMP OFF CHECK PRESSURE DECREASED AT ZERO 19 ANNUNCIATOR PANEL TEST 20 LANDING GEAR LIGHTS TEST 21 ELT CHECK SET TO ARM 22 FIRE DETECTOR TEST 23 ELECTRICAL PITCH TRIM SELECTOR TEST 24 ENGINE LEVERS FRICTION ADJUST IF REQUIRED 25 FLIGHT CONTROLS CHECK FREE 26 ALTERNATE STATIC PORT CHECK CLOSED 27 CABIN HEAT CLOSED 28 FLAPS OPERATE CONTROL TO FULL POSITION, VERIFYING EXTENSION. THEN RETRACT FLAPS 29 PITCH & RUDDER TRIM CONTROL SET TO NEUTRAL POSITION. 30 BATTERY VOLTMETER CHECK 12 TO 14 VOLT COCKPIT INSPECTION CHECK LIST COMPLETED NORMAL CHECK LIST P2006T NORMAL CHECK LIST P2006T Edizione3 Rev 0 del 01 Aprile 2020 2 ENGINE STARTING CAUTION AVIONICS SWITCHES MUST BE SET OFF DURING ENGINE STARTING TO PREVENT AVIONIC EQUIPMENT DAMAGE 1 START CLEARANCE Obtain if needed 2 CHRONOMETER START RH ENGINE STARTING 4 RH THROTTLE LEVER IDLE 5 RH CARBURETOR HEAT OFF 6 RH PROPELLER LEVER FULL FORWARD 7 RH CHOKE ON if required Cold engine. Throttles fully closed, chokes fully opened. Soon after starting advance the throttle to ~800 RPM and slowly close the choke. Keep engine at ~900 RPM for warm up period. Hot engine. Park the aircraft with the nose pointing into wind in order to aid cooling. Keep chokes closed and slowly open the throttles one inch while cranking. “Flooded Engine” (after engine start failure). Keep chokes closed, open throttle fully and start the engine, then quickly reduce throttles to idle. 8 RH ELECTRICAL FUEL PUMP ON CHECK ADVISORY LIGHT ON & POSITIVE FUEL PRESS BUILD UP 9 STROBES ON 10 RH ENGINE PROPELLER ZONE CHECK free 11 RH IGNITIONS SWITCHES BOTH ON WARNING ENSURE THAT AREA AROUND ENGINE PROPELLER DISC IS CLEAR FROM PEOPLE AND OBSTACLES. CALL OUT FOR PROPELLER FREE. 12 RH START PUSHBUTTON PUSH 13 RH ENGINE OIL GAUGE CHECK INCREASING WITHIN 10 SEC. (MAX 7 BAR IN COLD OPERATION) 14 RH PROPELLER RPM 1200 RPM 15 RH CHOKE OFF 16 RH FIELD ON 17 RH AVIONICS ON 18 RH CROSS BUS ON 19 RH AMMETER CHECK AMPS POSITIVE 20 RH VOLTMETER CHECK 12 TO 14 VOLT 21 RH ELECTRICAL FUEL PUMP OFF LH ENGINE STARTING 1 LH THROTTLE LEVER IDLE 2 LH CARBURETOR HEAT OFF 3 LH PROPELLER LEVER FULL FORWARD 4 LH CHOKE ON IF REQUIRED 5 LH ELECTRICAL FUEL PUMP ON CHECK ADVISORY LIGHT ON & POSITIVE FUEL PRESS BUILD UP 6 LH ENGINE PROPELLER ZONE CHECK FREE 7 LH IGNITIONS SWITCHES BOTH ON WARNING ENSURE THAT THE AREA AROUND ENGINE PROPELLER DISC IS CLEAR FROM PEOPLE AND OBSTACLES. CALL OUT FOR PROPELLER FREE. 8 LH START PUSHBUTTON PUSH 9 LH ENGINE OIL GAUGE CHECK INCREASING WITHIN 10 SEC. (MAX 7 BAR IN COLD OPERATION) 10 LH PROPELLER RPM 1200 RPM 11 LH CHOKE OFF 12 LH FIELD ON 13 LH AVIONICS ON 14 LH CROSS BUS ON 15 LH AMMETER CHECK AMPS POSITIVE 16 LH VOLTMETER CHECK 12 TO 14 VOLT 17 LH ELECTRICAL FUEL PUMP OFF ENGINE STARTING CHECK LIST COMPLETED BEFORE TAXING 1 Let engines warm up to a minimum oil temperature of 50°C at 1200 RPM 2 NAV, TAXI LIGHT ON 3 AUDIO PANEL ON 4 COM /NAV ON 5 TRANSPONDER STANDBY 6 PASSENGERS AND CREWS SEAT BELTS Fastened 7 PASSENGERS AND CREWS HEADPHONES Set as required BEFORE TAXIING CHECK LIST COMPLETED TAXIING 1 LH/RH FUEL SELECTOR AS REQUIRED 2 LH AND RH FUEL PRESSURE MONITOR 3 PARKING BRAKE RELEASE 4 FLIGHT INSTRUMENTS CHECK 5 ENGINE INSTRUMENTS CHECK 6 ALTIMETERS SET & CHECK MAX DIFF. 150 FT 7 BRAKES TEST TAXIING CHECK LIST COMPLETED BEFORE TAKE OFF 1 PARKING BRAKE ENGAGED 2 RH FUEL SELECTOR RIGHT 3 LH FUEL SELECTOR LEFT 4 LH & RH FUEL PRESSURE CHECK 5 LH & RH ENGINE PARAMETERS CHECKS Oil temperature: 50-110 ° CHT: 50° -135° Oil pressure: 2-5 bar (above 1400 RPM) 0.8 bar (below 1400 RPM) Fuel pressure: 2.2 – 5.8 psi (0.15 - 0.40 bar) 6 LH & RH GENERATOR LIGHTS CHECK BOTH OFF 7 LH & RH PROPELLER LEVER FULL FORWARD 8 LH & RH THROTTLE LEVER 1650 RPM 9 RH THROTTLE LEVER Set L / R / BOTH (RPM drop with single ignition circuit selected must not exceed 130 prop’s RPM; maximum RPM difference by use of either circuits LEFT or RIGHT cannot exceed 50 RPM) 10 RH PROPELLER GOVERNOR CHECK . A. Retard the prop lever until 1200 RPM. B. Move propeller lever back to full forward position C. Repeat A) and B) 3 times D. Verify that the governor closely and firmly controls the RPM E. Verify that 1650 prop rpm are restored with prop lever in full forward position NOTE Do not cause prop speed drop below 1150 RPM in any case 11 RH CARBURETTOR HEAT ON, verify propeller RPM decreasing about 100 RPM 12 RH CARBURETTOR HEAT OFF 13 RH ENGINE INSTRUMENTS GREEN ARCS 14 LH IGNITIONS SWITCHES Set L / R / BOTH (RPM drop with single ignition circuit selected must not exceed 130 prop’s RPM; maximum RPM difference by use of either circuits LEFT or RIGHT cannot overcome 50 RPM) 15 LH PROPELLER LEVER GOVERNOR CHECK . A. Retard the prop lever until 1200 RPM. B. Move propeller lever back to full forward position C. Repeat A) and B) 3 times D. Verify that the governor closely and firmly controls the RPM E. Verify that 1650 prop rpm are restored with prop lever in full forward position NOTE Do not cause prop speed drop below 1150 RPM in any case 16 LH CARBURETTOR HEAT ON, verify propeller RPM decreasing about 100 RPM 17 LH CARBURETTOR HEAT OFF 18 LH ENGINE INSTRUMENTS GREEN ARCS 19 LH & RH FUEL Q.TY INDICATOR CHECK consistent with fuel plan 20 FLAPS T/O OR AS REQUIRED (See section 5 T/O performances) 21 PITCH TRIM & RUDDER TRIM SET TO NEUTRAL POSITION 22 FLIGHT CONTROLS CHECK FREE 23 SEAT BELTS & DOORS CHECK FASTEN/CLOSED/LOCKED BEFORE TAKE OFF CHECK LIST COMPLETED LINE UP 1 PARKING BRAKE RELEASE CHECK FULL IN 2 ANNUNCIATOR PANEL CAUTIONS & WARNINGS OFF 3 RH FUEL SELECTOR RIGHT 4 LH FUEL SELECTOR LEFT 5 PITOT HEAT AS REQUIRED 6 TRANSPONDER SET ALT 7 COMPASS / HEADING INDICATOR ALIGN/CROSSCHECK LINE UP CHECK LIST COMPLETED NORMAL CHECK LIST P2006T NORMAL CHECK LIST P2006T Edizione3 Rev 0 del 01 Aprile 2020 3 TAKEOFF AND CLIMB 1 LANDING LIGHT ON 2 LH AND RH ELECTRICAL FUEL PUMP BOTH ON 3 CARBURETTORS HEAT CHECK OFF 4 LH AND RH PROPELLER LEVER FULL FORWARD 5 LH AND RH THROTTLE LEVER FULL POWER 6 ENGINES INSTRUMENTS PARAMETERS WITHIN GREEN ARCS 7 ROTATION SPEED Vr = 65 KIAS 8 APPLY BRAKES TO STOP WHEEL SPINNING APPLY 9 LANDING GEAR CONTROL KNOB UP CHECK GREEN LIGHTS AND TRANS LIGHT OFF WITHIN 20 SEC 10 LANDING AND TAXI LIGHTS OFF ABOVE 10000 FT 11 LH & RH PROPELLER LEVER AT SAFE ALTITUDE MAX CONT POWER CAUTION Limit max TO power to 5 minutes. Reduce MAP before retracting Prop to 2250 RPM or below 12 LH AND RH ELECTRICAL FUEL PUMP BOTH OFF TAKEOFF AND CLIMB CHECK LIST COMPLETED CRUISE 1 PROPELLER SET to 1900- 2250 RPM CAUTION Throttles MAP decrease should be made before propeller Speed reduction below 2200 RPM, as, contrariwise, Propeller Lever increase RPM should be set before engine Throttle Levers are advanced. 2 ENGINE INSTRUMENTS OIL TEMPERATURE: 90° 110 ° C. CHT: 90° 110 °C OIL PRESSURE: 2 - 5 BAR. FUEL PRESSURE: 2.2 – 5.8 PSI 3 CARBURATOR HEATING AS REQUIRED WARNING DESELECT AND DO NOT USE AUTO PILOT IF POSSIBLE ICING CONDITION AREA IS INADVERTENTLY ENTERED. 4 FUEL BALANCE AND CROSSFEED CHECK AS NECESSARY CRUISE CHECK LIST COMPLETED DESCENT & APROACH 1 PROPELLERS MAX CONT - 2250 RPM NOTE In order to control engine cooling and life, it is preferable to descend with power above idle and RPM lower than full continuous 2 CARBURETTORS HEAT AS REQUIRED 3 ALTIMETER SETTING QNH SET/CROSSCHECK 4 REAR PASSENGER SEATS SET FULL AFT POSITION DESCENT & APPROACH CHECK LIST COMPLETED BEFORE LANDING 1 REAR PASSENGERS SEATS FULL AFT/LOWER POSITION 2 LH & RH ELECTRICAL FUEL PUMP BOTH ON 3 ON DOWNWIND LEG VFE=122KIAS FLAPS T/O 4 SPEED BELOW VLO/VLE 93 KIAS LANDING GEAR CONTROL KNOB-DOWN CHECK GREEN LIGHTS ON 5 CARBURETTORS HEAT CHECK OFF 6 LH & RH PROPELLER LEVER FULL FORWARD 7 ON FINAL LEG: SPEED BELOW 93 KIAS FLAPS FULL 8 FINAL APPROACH SPEED VAPP=71KIAS 9 LANDING & TAXI LIGHT ON 10 TOUCHDOWN SPEED 65 KIAS BEFORE LANDING CHECK LIST COMPLETED BALKED LANDING/MISSED APPROACH 1 LH AND RH PROPELLER LEVER FULL FORWARD 2 LH AND RH THROTTLE LEVER FULL POWER CAUTION Propeller Lever increase to max RPM should be attained before engine Throttle Levers are advanced to max take off power. Limit max take off power to 5 minutes. 3 FLAPS T/O 4 SPEED KEEP OVER 62 KIAS, CLIMB TO VY OR VX AS APPLICABLE 6 LANDING GEAR UP AT POSITIVE CLIMB 7 FLAPS UP BALKED LANDING/MISSED APPROACH CHECK LIST COMPLETED AFTER LANDING 1 LH & RH ELECTRIC FUEL PUMP OFF 2 FLAPS RETRACT 3 PITOT HEAT OFF 4 LANDING LIGHT OFF 5 TRANSPONDER STBY AFTER LANDING CHECK LIST COMPLETED PARKING/SHUT DOWN 1 PARKING BRAKE SET 2 TAXI LIGHT OFF 3 ENGINES 1 MIN AT IDLE POWER 4 FLAPS CHECK UP 5 TRIMS CHECK NEUTRALS NOTE Ensure the engine is at its lowest possible idle speed before selecting ignitions OFF 6 IGNITIONS TURN OFF ONE AT TIME 7 LH & RH AVIONIC BUS OFF 8 LH & RH CROSS BUS OFF 9 LH/RH FIELD OFF 10 ALL EXSTERNAL LIGHT SWITCHES OFF 11 DOORS SAFETY LOCKS OFF 12 MASTER SWITCH OFF 13 EMG BATT / EMG COCKPIT LIGHT / EMG ADI SWITCHES CHECK OFF PARKING/SHUT DOWN CHECK LIST COMPLETED WARNING BEFORE DISEMBARKATION VERIFY PROPELLERS ARE FULLY STOPPED CAUTION Instruct passengers to fully open pax door (against nacelle stop) and depart alongside aircraft fuselage, avoiding contact with hot / oily parts such as engine exhaust pipes, drainage tubes and wheel brakes, or sharp wing control surfaces edges. CAUTION Crew should avoid propeller disc area crossing while proceeding alongside a fully opened pilot’s door (up to 110°). POST FLIGHT 1 PROTECTIVE COVER FOR PITOT TUBES, STALL WARNING AND STATIC PORT PLUGS INSTALL 2 LOCK ONE CONTROL WHEEL WITH SAFETY BELT. 3 WHEEL CHOCKS PLACE UNDER MLG 4 AILERON LOCK PLACE AND TIGHTEN 5 PILOT AND PASSENGERS DOORS. CLOSE AND LATCH 6 TLB FILL POST FLIGHT CHECK LIST COMPLETED GROUND TOWING, PARKING AND MOORING CAUTION When the a/c is moved on the ground, the Master Switch must be turned ON until the a/c is parked WHEEL CHOCKS PLACE UNDER MLG AILERON LOCK PLACE AND TIGHTEN PILOT AND PASSENGERS DOORS. CLOSE AND LATCH TLB FILL POST FLIGHT CHECK LIST COMPLETED The aircraft is certified in normal category in accordance with EASA CS-23. Non aerobatic operations include: Any manoeuvre pertaining to “normal” flight Stalls (except whip stalls) Lazy eights Chandelles Turns in which the angle of bank is not more than 60° This Check List is compliant to Section 4 – Normal Procedure of the Aircraft Flight Manual Doc. No. 2006/044 4th Edition – Rev. 14 issued by Costruzioni Aeronautiche TECNAM srl - Via Maiorise CAPUA (CE) – Italy on the 03 March 2020. AIRCRAFT MODEL: P2006T EASA TYPE CERTIFICATE NO:A .185(DATED 2009,JUN 5TH) Sky Services Flight Academy NORMAL CHECK LIST P2006T NORMAL CHECK LIST P2006T Edizione3 Rev 0 del 01 Aprile 2020 4 Intentionally Left Blank Intentionally Left Blank

All TECNAM P-2006T checklist