P2012 Traveller
TECNAM P2012 TRAVELLER · Checklist
Overview
The document is a checklist for the Tecnam P2012 Traveller aircraft, detailing its specifications, performance, and operational guidelines. It includes historical context about Tecnam as a manufacturer and outlines the aircraft's design features and testing requirements.
- Tecnam was founded in 1948 in Capua, Italy.
- The P2012 Traveller can accommodate one or two pilots and up to nine passengers.
- The aircraft features a high wing configuration for improved passenger access and rough field operations.
- The baggage compartment has a volume of 88.3 ft³.
- The engine is a Lycoming TEO-540-C1A, a turbocharged, air-cooled engine.
- TECNAM produces over 200 aircraft annually.
- The P2012 Traveller is designed for reliability, efficiency, and passenger comfort.
- The aircraft is capable of using both Mogas and Avgas.
Document
Source
Originally published by aeropolis.it. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- File size ·
- 5.2 MB
- Publisher ·
- aeropolis.it
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Baggage capacity ft3 ·
- 88.3
What is the P2012 Traveller?
The P2012 Traveller is a checklist for the TECNAM P2012 TRAVELLER.
Where does the P2012 Traveller come from?
This copy of the P2012 Traveller was originally published by aeropolis.it 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 P2012 TRAVELLER.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
In this document
History
Tecnam was established in 1948 and has become a leading producer in General Aviation, known for its innovative aircraft designs.
What We Do Today
TECNAM is recognized as a major player in General Aviation, delivering over 200 aircraft per year and offering a wide range of models.
P2012 Traveller Program
The P2012 Traveller is designed to meet the demands for a next-generation aircraft that emphasizes reliability and passenger comfort.
Engine Specifications
The P2012 Traveller is equipped with a Lycoming TEO-540-C1A engine, featuring advanced electronic control systems for improved performance.
Flight Test Requirements
The document outlines various flight test requirements, including climb performance, stability, and equipment functionality.
Performance Metrics
The aircraft's performance metrics include specifications for climb rates, landing distances, and stability assessments.
Full document text
Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… P2012 Traveller Seminari interdisciplinari di cultura aeronautica – IV Ciclo Le Attività di progettazione ed esecuzione delle prove in volo dei velivoli Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… History Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… P48B Astore P52-Tigrotto P55-Tornado P57 Fachiro 1959 1964 P64 Oscar P59 Jolly 1968 1968 P68 R P68 Victor AP68 TP Viator 1966 P66 Oscar 100/150 1966 P66 Charlie 1970 Giovanni and Luigi Pascale Brothers and Founders History ➢ Founded in 1948 in the South of Italy – Capua, Naples by Pascale Brothers. ➢ Became a leading producer of General Aviation at this time as Partenavia. ➢ Producer of parts for other important Manufacturers: • Alenia (Horizontal tail for the ATR aircraft family) • Aer Macchi (Vertical tail of M346 Military Trainer) • Boeing (Fuselage panel for B717 Commercial Aircraft) • Augusta (Fuselage Structural Parts) Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… What We Do Today ➢ One of the most innovative company in General Aviation in the last decade; ➢ In the last years TECNAM have delivered more than 200 aircraft per year, becoming one of the most important GA’s OEM according to GAMA; ➢ TECNAM have 250 employees and our production capability is to produce 1 ½ single engine two seater aircraft per day, 1 twin engine per week and 1 single engine four seater every two weeks. ➢ More than 33’s models along AUL – LSA – CS/VLA – CS/23//FAR23’s categories. Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… TECNAM is spread all over the world: TECNAM Headquarters in Capua- Italy Casoria Facility in Naples - Italy Sebring Facility in Florida - US Shenyang Facility in China by LUSY MORE THAN 65 DEALERS MORE THAN 125 SERVICE CENTER WORLDWIDE Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… TECNAM Research & Development NASA has selected the Tecnam P2006T twin as the airframe on which it will evaluate the potential of LEAPtech (Leading Edge Asynchronous Technology), with the aim of developing safer, more energy efficient, lower operating cost and greener general aviation aircraft. CIRA has selected the Tecnam P92 to be developed as an UNMANNED aircraft. TECNAM is the only company who has a complete aircraft certified by EASA with hand controls in order to allow disable pilots to get their license in GA. This certification was supported by a recognized entity from UK called Aerobility. Tecnam is actively evaluating the potential of developing and producing a two-seater, single turbofan engine powered aircraft TECNAM PJET Concept. Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Today TECNAM is the World Leader in Light and General Aviation Aircraft Manufacturing: Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… • More than 33 models along AUL – LSA – CS/VLA – CS/23//FAR23’s categories; TECNAM Airplanes: • All family of aircraft have the widest range of choice for any Flight School, Private Owner, Surveillance and Regional Airlines. • All our fleet is capable of using Mogas (Automobile Fuel) and Avgas. • TECNAM is the only company offering the most affordable fleet in terms of acquisition price and operational cost in the sector. Market Share • Recognized as the First Choice for many Flight Training Organizations (FTO); Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… ➢ Operators have been demanding a next generation aircraft that can deliver not only profits but reliability, efficiency and of course, passenger comfort. ➢ One of the first new FAR23/CS23 aircraft to address this marketplace in more than many years. ➢ The P2012 Traveller builds on Tecnam’s commitment to continue to develop outstanding, stylish, innovative and affordable aircraft. Tecnam P2012 Traveller Program Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Benefits of high wing configuration - comparison Passenger Friendly Ease of Cabin and Cargo Access Rough Field Operations (Propeller and engine air intakes clearance from debris) Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… One or two pilots – 9 passengers Pitch between seats 32.00” Baggage compartment volume 88.3 ft3 Seating Arrangement standard configuration Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Seating Arrangement - 402C comparison P2012 402C Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… P2012 402C Seating Arrangement - 402C comparison Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Passenger and Cargo Doors Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Cabin section Comparison Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Baggage Compartment Comparison Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Baggage Loading Comparison Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Weights Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Performances Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Engine Lycoming TEO-540-C1A Lycoming TEO-540-C1A Engine is a direct-drive six-cylinder, horizontally opposed, turbocharged, air-cooled engine. It has electronic fuel injection, electronic ignition, down exhaust, and induction air coolers. As equipment, this engine has an automotive type starter, one 28V alternator (130A) and a propeller governor. The EECS (Electronic Engine Control) is an electronic, microprocessor controlled system that continuously monitors and adjusts ignition timing, fuel
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injection timing, and fuel mixture based on operating conditions. The EECS eliminates the need for magnetos and manual fuel/air mixture. The EECS connects engine hardware with electronic controls to replace mechanical control systems and enables single lever engine control. data Engine EECS Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… TIO-540 vs. TEO-540 Fuel Consumption vs. Power Power Setting Power TEO-540 -C1A TIO-540 –J2B Delta 60% 210HP@2200rpm 14.5 14.6 -0.1 gph (0.7%) 75% 263HP@2400rpm 18.1 20.7 -2.6 gph (-12.6%) 100% 350HP@2575rpm 32.6 40.2 -7.6 gph (-18.9%) Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Cockpit layout Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Aerodynamic Analysis Computational fluid dynamics analysis to confirm preliminary studies Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Aerodynamic Analysis Wind Tunnel testing confirm espected data Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Flight Test ➢ Manage aircraft configuration(s) ➢ Define applicable requirements and test pass/fail criteria ➢ Development Tests ➢ Define test procedure and loading conditions ➢ Define Flight Test Points (FTP) and Flight Test Order (FTO) ➢ Risk Assessment and Risk Management ➢ Data Reduction and/or Pilot Statements Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Aircraft Configuration ➢ Aircraft Weighing ➢ Pilot, Crew, Ballast, Fuel, etc. ➢ List of experimental change installed ➢ Configuration notes ➢ Flight Test Instrumentation (FTI) Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Applicable Requirements (EASA CS-23) Subpart Requirements Flight 23.45, 23.49, 23.51, 23.53, 23.63, 23. 65, 23.66, 23. 67, 23.69, 23.73, 23.75, 23.77, 23.141, 23. 143, 23.145, 23.147, 23.149, 23.153, 23.155, 23.157, 23.161, 23.171, 23.173, 23.175, 23.177, 23.181, 23.201, 23.203, 23.207, 23.231, 23.233, 23.235, 23.251 Design and Construction 23.629, 23.671, 23.677, 23.697, 23.701, 23.735, 23.745, 23.773, 23.831 Powerplant 23.901, 23.903, 23.905, 23.909, 23.939, 23.943, 23.951, 23.959, 23.961, 23.975, 23.1011, 23.1017, 23.1023, 23.1041, 23.1043, 23.1047, 23.1091, 23.1093, 23.1141, 23.1143 Equipment 23.1301, 23.1311, 23.1321, 23.1322, 23.1323, 23.1325, 23.1327, 23.1331, 23.1337, 23.1351, 23.1381, 23.1383, 23.1401, 23.1431, 23.1431 Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Test Pass/Fail Criteria(s) Req. Title Test Pass/Fail Criteria(s) MoC 23.65 Climbs: all engine operating The steady gradient of climb at sea level must be at least 4.0% Data Reduction 23.75 Landing Distance No excessive vertical acceleration No tendency to bounce No tendency to nose-over No tendency to ground loop No porpoise Data Reduction Pilot Statement 23.629 Flutter The A/C is free from flutter The A/C is free from control reversal The A/C is free from divergence Data Reduction 23.1301 Function and Installation Each item of installed equipment must function properly Pilot Statement Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Development Flight Test - Aerodynamic Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Development Flight Test - Ice Protection Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… SoC Flight Tests ➢ Flight Performance (Stalling Speed, Take-Off, Landing, Rate of Climb, etc.) ➢ Stability (Static Longitudinal Stability, Static Directional and Lateral Stability, Dynamic Stability) ➢ Flutter ➢ Powerplant (Controls, Cooling, Fuel System, Oil System, etc.) ➢ Equipment ➢ Human Factor Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Flight Performance – Rate of Climb Title All Engine Operating En-route Climb Procedure A series of climbs, known as sawtooth climbs, will be conducted at several constant indicated airspeed and several altitude using a constant power setting and a prescribed configuration. Requirements 23.45, 23.63, 23.69, 23.141, 23.161, 23.1301 Flight Test Points # W C.G. Flap Pwr Alt. 1 MTOW FWD UP MCP LOW 2 MTOW FWD UP MCP MID 3 MTOW FWD UP MCP HIGH Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Flight Performance – Rate of Climb Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Stability– Static Longitudinal Stability Title Static Longitudinal Stability - Cruise Procedure Trim the airplane in the prescribed configuration and for the condition required by the regulation. Apply a pull force and stabilize at a lower speed. Continue this process in appropriate steps (5 to 10kts) and record displacements and effort at each step. At prescribed stabilized point the pull force should be very gradually relaxed to allow the airplane to slowly return toward trim speed and zero stick force. Set again at the initial trim speed and apply a push force and stabilize at a higher speed. Continue this process in appropriate increments (5 to 10kts) and record displacements and effort at each increment. Relax stick in the same manner as previously described. Requirements 23.141, 23.171, 23.175 Flight Test Points # W C.G. Flap Pwr Alt. 1 LIGHT AFT UP PLF LOW 2 LIGHT AFT UP PLF HIGH Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Stability – Static Longitudinal Stability Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Flutter – Flutter Test Title Flutter Procedure At several trim speed points (up to VD), each axis must be pulsed, with bands off controls, prior to the next impulse or speed point, in order to verify the A/C is free from flutter, control reversal, and divergence. Requirements 23.629 Flight Test Points # W C.G. Flap Pwr Alt. 1 LIGHT FWD UP A.R. LOW 2 LIGHT FWD UP A.R. HIGH Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Flutter – Flutter Test Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Equipment – Air Data System Title Air Data System Procedure Check for proper functioning of all related equipment. The compliance with this requirement will be shown with a pilot judgement during the flight test campaign. Requirements 23.1301 Flight Test Points # W C.G. Flap Pwr Alt. 0 ALL ALL ALL ALL ALL Copyright © Tecnam. All rights reserved. MORE THAN 65 YEARS SHARING OUR PASSION… Human Factor – Human Factor for IFR Title Human Factor for IFR Procedure Simulate IFR legs, VOR and RNAV RNP, and NON PRECISION (VOR) and ILS approaches. Requirements CRI B-52 Flight Test Points # W C.G. Flap Pwr Alt. 1 ANY ANY TO A.R. A.E. 2 ANY ANY UP MTOP ANY 3 ANY ANY UP MCP ANY 4 ANY ANY UP PLF ANY 5 ANY ANY UP DESCENT ANY 6 ANY ANY LN APP ANY 7 ANY ANY LN A.R. A.E. 8 ANY ANY ANY A.R. A.E.