THE INNOVATIVE FOUR-SEAT SINGLE
TECNAM P2010 MKII · Checklist
Overview
The Tecnams P2010 MKII checklist provides essential information about this innovative four-seat single-engine aircraft designed for flight training. It covers specifications, performance metrics, and features that enhance training efficiency and safety.
- Available with two Lycoming engine options: 180 hp and 215 hp.
- Max cruise speed of 145 knots (269 km/h).
- Max range of 720 nautical miles (1,333 km).
- Spacious cabin with four seats and three passenger doors.
- Equipped with Garmin G1000 NXi avionics suite.
- Designed for VFR and IFR training operations.
- Direct operating costs range from €145.31 to €164 per hour.
- Carbon fiber fuselage enhances strength and efficiency.
Document
Source
Originally published by aerotec.lat. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- File size ·
- 61 MB
- Publisher ·
- aerotec.lat
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Useful load (lb) ·
- 970
- Baggage allowance (lb) ·
- 88
- Max take off weight (lb) ·
- 2690
- Empty weight standard (lb) ·
- 1720
- Fuel tank capacity us (gal) ·
- 63
Performance
- Max range (nm) ·
- 720
- Landing run (ft) ·
- 860
- Stall speed (kt) ·
- 53
- Take off run (ft) ·
- 1192
- Service ceiling (ft) ·
- 14000
- Max cruise speed (kt) ·
- 145
V-speeds
- VS_KIAS ·
- 53
Weight & balance
- Useful load (lb) ·
- 970
- Empty weight (lb) ·
- 1720
- Max take off weight (lb) ·
- 2690
What is the THE INNOVATIVE FOUR-SEAT SINGLE?
The THE INNOVATIVE FOUR-SEAT SINGLE is a checklist for the TECNAM P2010 MKII.
Where does the THE INNOVATIVE FOUR-SEAT SINGLE come from?
This copy of the THE INNOVATIVE FOUR-SEAT SINGLE was originally published by aerotec.lat and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the TECNAM P2010 MKII.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P2010 MKIImanuals & documents
In this document
Engine Options
The P2010 offers two Lycoming engine options: IO-360M1A (180 hp) for fuel flexibility and lower costs, and IO-390-C3B6 (215 hp) for enhanced performance.
Cabin Design
The cabin features four seats, three passenger doors, and ergonomic seating for comfort, with a dedicated external baggage door.
Performance
The aircraft boasts a max cruise speed of 145 knots, a max range of 720 nautical miles, and a service ceiling of up to 14,000 feet.
Avionics
Equipped with a dual-screen Garmin G1000 NXi IFR suite and GFC700 autopilot, enhancing training with modern navigation capabilities.
Safety Features
The aircraft includes advanced safety features such as a carbon fiber fuselage and a reliable engine for reduced maintenance and downtime.
Specifications
The P2010 MKII has a maximum takeoff weight of 2,690 lb and a useful load of 970 lb, with a baggage allowance of 88 lb.
Safety notes
- Always consult specific aircraft weight and balance parameters for flight planning.
- Actual useful load may vary depending on options installed.
- Refer to Lycoming Service Instruction No. 1070 for fuel type details.
Full document text
THE INNOVATIVE FOUR-SEAT SINGLE THE INNOVATIVE FOUR-SEAT SINGLE Fuel AvGas or 100 LL (ASTM D910) Approval CS-23 | FAR23 Flight rules VFR-VFR/N-IFR-PBN Tailored for PPL+HB+VFR/N+IR+PBN+VP Direct operating costs € 145,31/h - 164/h ($149,45 - 168,7) incl. TBO reserve TRUSTED BY FLIGHT SCHOOLS WORLDWIDE AND MANY OTHERS CHOOSE YOUR POWERPLANT The P2010 offers two Lycoming engine options, allowing flight schools totailor their fleet to their training needs: • Lycoming IO-360M1A (180 hp) – Supports MoGas and AvGas, offering fuel flexibility and lower operating costs. • Lycoming IO-390-C3B6 (215 hp) – Runs on AvGas, providing enhanced performance for more demanding training operations. This versatile powerplant selection ensures optimal efficiency, cost management, and adaptability, making the PTwentyTen a forwardthinking investment for flight training programs. MAX CRUISE 145 kts - 269 km/h HORSEPOWER 180-215 hp MAX RANGE 720 NM - 1.333 km USEFUL LOAD 970 lb - 440 kg The TECNAM PTwentyTen MkII is the most advanced high-wing, modern single-engine aircraft for flight training, offering exceptional performance, stability, and safety. With balanced controls and the cutting-edge Garmin G1000 NXi avionics suite, it ensures a smooth transition from basic to advanced training. The GFCN00 autopilot delivers precision and reliability, reducing workload while enhancing safety and efficienc. Perfect for mastering IFR operations and advanced flight training. Its carbon fiber fuselage, metal wing, and stabilator enhance strength and efficiency, while the spacious cabinprovides ergonomic seating and superior legroom. A third entry door allows easy rear-seat access, making it ideal for instructors and students alike. DESIGNED TO OFFER THE BEST TRAINING TO THE PILOTS OF THE FUTURE CABIN Four seats, three passenger doors, and a dedicated external baggage door, the PTwentyTen offers a spacious and well-designed cabin, built for bothcomfort and functionality. The third entry door provides easy access forstudents, instructors, and passengers, enhancing convenience during training and everyday operations. Ergonomic front and rear seats ensure exceptional legroom and comfort. For added refinement, the electrically adjustable front seats enhance comfort while meeting the highest industry standards for safety and durability. PERFORMANCE BASED NAVIGATION The spacious composite cabin accommodates a large instrument panel, optimized for flight training operations. Equipped with a twinscreen Garmin G1000 NXi IFR suite and an integrated GFC700 autopilot, it provides students with real-world experience using advanced avionics. Performance-Based Navigation (PBN) enhances training by shifting from traditional sensor-based navigation to a modern performance-driven approach, preparing pilots for today’s airspace requirements. Cutting edge platform with a trusted powerplant - The PTwentyTen MkII is the obvious choice for those who want a modern aircraft in line with the latest safety amendments with a reliable engine. Its composite fuselage, metal wings, and stabilator maximize efficiency and durability, while advanced avionics ensure a smooth transition to modern flight decks. Powered by popular Lycoming engines, it guarantees easy maintenance, minimal downtime, and nationwide availability of spare parts. Maximized efficiency - PTwentyTen is designed to reduce operating costs for flight schools. The IO-360M1A engine supports MoGas, offering a more affordable fuel option. Combined with low maintenance requirements and efficient performance, the P TwentyTen helps flight schools maximize training hours while minimizing expenses. MAKE YOUR CHOICE SPECS DESIGN WEIGHT AND LOADING Maximum Take Off Weight 2.557 lb - 1.160 kg 2.690 lb - 1.220 kg Empty Weight, Standard 1.687 lb - 765 kg 1.720 lb - 780 kg Useful Load 870 lb - 395 kg 970 lb - 440 kg Baggage Allowance 88lb - 40 kg 88lb - 40 kg PERFORMANCE Max Cruise Speed TAS 140 kts - 259 km/h 145 kts - 269 km/h Stall Speed (Flaps Down Power Off ) CAS 52 kts - 96 km/h 53 kts - 98 km/h Service Ceiling 12.000 ft - 3.658 m 14.000 ft - 4.267 m Take Off Run 1.102 ft - 336 m 1.192 ft - 363 m Take Off Distance 1.952 ft - 595 m 1.612 ft - 491 m Rate of Climb 841 ft/min - 4,27 m/sec 1.009 ft/min - 5,1 m/sec Landing Run 778 ft - 237 m 860 ft - 262 m Landing Distance 1.709 ft - 521 m 1.887 ft - 575 m Max Range 720 NM - 1.333 km 720 NM - 1.333 km POWER PLANT P2010 180 HP P2010 215 HP Engine Manufacturer Lycoming IO-360 Lycoming IO-390-C3B6 Engine Power 180 HP 215 HP Propeller 2/3 Bladed Fixed/Variable Pitch Propeller 3 Bladed Variable Pitch Propeller Fuel Consumption 11,9 USG/h (45 lt/h) 12 USG/h (46 lt/h) Fuel Type AvGas grade 91/96 or MoGas 100 LL (ASTM D910)* AvGas Fuel Tank Capacity 63 US Gal (240 lt) 63 US Gal (240 lt) * For additional information, refer to Lycoming Service Instruction No. 1070, latest issue. Garmin G1000 Nxi includes: • GDU 1050 10-inches PFD • GDU 1054 10-inches MFD • Dual GEA 71B Engine & Airframe unit • Dual GIA 64WAAS Com/nav/GPS/GS/Loc • GMA1360 Digital audio system • GMU44B Magnetometer • GDC72 Air data computer • GRS79 AHRS • GTP59 OAT • GTX345R Mode S Transponder (ADS-B In and OUT) • GFC 700 Autopilot Including Electronic Stability & Protection (ESP) Flight instruments and indicators • Magnetic Compass • GI275/MD302 Standby Attitude Module • Pitot System Heated • Static System • Alternate Static Source • Stall Warning Audible • Stabilator Trim Position Indicator • Rudder Trim Position Indicator Flight controls • Hydraulic Toe Brakes • Parking Brake • Electrical Flaps • Dual Flight Controls • Castering Nose Wheel • Aileron Lock and Elevator Lock • Flight Trim Controls – Rudder with Indicator – Stabilator with Indicator • Engine Controls: – Throttle – Mixture – Alternate Air – Fuel Control Selector with LH/RH/OFF Electrical system • Alternator, 28 Volt, 60 Amp • Battery, 24 Volt 19 AH • Rocker Switches:
Show full textShow less
– Master Switch – Fuel Pump – Landing Light – Taxi Light – Navigation Lights – Strobe Light • External Power Supply Receptacle • Circuit Breaker Panel • Static Discharge Wicks • Landing/Taxi Light LED Fuel system • Two Integral Fuel Tanks With 240 Litres (64 UsGal) Total Capacity • Engine Driven Fuel Pump • Auxiliary Fuel Pump, Electric • Fuel Tank Quick Drain • Fuel Selector Valve, Left/Right/Off Exteriors lights • Nav. Lights LED with Strobe Aveo Full LED TSO • Landing/Taxi Light LED Interiors • Pilot and Co-Pilot Seats Leather: – Adjustable Fore and Aft – Electric Vertical Adjustment • Two Rear Passenger Seats Leather • Seat Belts & Shoulder Harness, All Seats • Wall To Wall Carpeting • Hand Held Fire Extinguisher • Map & Storage Pockets • USB socket Type C • Radio Call Plate • Tow Bar • Soundproofing • Luggage Compartment • Overhead Cockpit Speaker • Four Position Intercom System • First Aid Kit • Powerplan Exterior • Epoxy Corrosion Proofing, All Structure • LH/RH Front Door Pilot/Co-Pilot, Lock and Key • Rh Rear Door Passenger • Rh Baggage Door With Lock • Rear Window • All Lateral Windows Tinted • Fixed Landing Gear • White Polyurethane Exterior Paint • Tie Down Rings • Main Wheels, 6.00 X 6 • Nose Wheel, 5.00 X 5 Cabin comfort system • Windshield Defroster • Ventilator adjustable, 4 Place • Heating System • Soundproofing • Cabin Monoxide Detection System Powerplant and Propeller • Lycoming IO-360-M1A Engine 180 HP @ 2700 RPM • Fuel Injection System • Tubular Steel Engine Mount • Dynafocal Rear Mount • Engine Driven Vacuum Pump • Alternate Engine Air • Oil Cooler • Shock Mounted Cowling • Throttle Control • Mixture Control • Dual Ignition System, Shielded Magneto Engine Exhaust Muffer • Fixed Pitch 2 Blade MT Propeller • Propeller Spinner • Electric Starter Product Support/Documents • Manufacturer’s Full Two Year Limited Warranty • Pilot’s Operation Handbook • Maintenance Manual • Parts Catalog • Aircraft Log Book • Engine Log Book Standard Avionics Package also includes: • Altitude Encoder • Avionics Master Switch • Mic & Phone Jacks / Lemo Plug Pilot/ Copilot/Passengers • Hand Held Microphone • Avionics Circuit Breaker Panel • Pilot And Co-Pilot PTT • ELT 406 Antennas • Marker Beacon Antenna • Transponder Antenna • VHF Antenna • NAV Antenna • Emergency Locator Transmitter Antenna Specifications,weights,representations,colors,listofequipment,useofmaterialsandmodelreferenceslistedhereinarenotwarrantedorguaranteedtobetrueoraccurate.Actualusefulloadwillvary dependingonoptionsinstalledontheaircraft.Alwaysconsultspecificaircraftweightandbalanceparametersanddataforflightplanning.Thepicturescontainedinthisbrochureofspecificmodelsorother productsmaycontainoptionalequipmentornonstandardfeatures,whichevenifavailablemaybeatanadditionalcost.Someoptionalequipmentmayrequireseparatepaidsubscriptionsfromthird-party providers.YoumayrelyonlyuponstatementsandrepresentationscontainedinactualcontractsthatyouenterintowithTECNAM.ReferencedTECNAMtrademarksareownedbyCostruzioniAeronautiche TECNAMSpAoritssubsidiaries.Allotherbrands,productnames,companynames,trademarksandservicemarksarethepropertiesoftheirrespectiveowners.Allrightsreserved.©2024,Costruzioni Aeronautiche TECNAM SpA. 250709-20 CGS www.aerotec.lat WWW.TECNAM.COM info@aerotec.lat