Tecnam p2006 t systems
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This is a Multi Engine training presentation describing the various systems of the Tecnam P2006T. The Systems include the Controllable Pitch Propeller, Landing Gear, Powerplant, Cooling/Lubrication, Electrical and Fuel System
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Tecnam p2006 t systems
- 1. Tecnam P2006T Systems Brian Yanowski, CFI, CFII, MEI
- 2. OBJECTIVE: • Understand the various systems of the Tecnam P2006T IAW the respective ACS. • References: AFH, POH, Coast Tecnam Supplement
- 3. Agenda • General Construction • Primary/Secondary controls • Constant Speed Prop • Powerplant/Engine • Coolant System (Liquid Cooled) • Oil system • Electrical System • Fuel • Brakes • Landing Gear
- 4. General Construction The fuselage is constructed by a light –alloy semi monocoque structure wrapped around by stressed skin panels Radome, Tail cone and winglets are of composite material Wingspan 37.4 feet; length 28.5 feet
- 5. Primary Controls • Ailerons w/ balance mass (differential up 20; down 17 degrees) • Stabilator • Vertical stabilizer/ Rudder
- 6. Secondary Controls • Electric Flaps (3 position Flaps- 0, Takeoff, Full) • Antiservo Tab • Electric Rudder Trim
- 10. Powerplant
- 12. Coolant System
- 13. Coolant System Components Cooler (radiator) Water Pump Expansion Tank Overflow Tank
- 14. Coolant System cont’d Cooler (radiator) Larger of the 2 filters
- 15. Oil System (Dry Sump) Overview
- 16. Oil System (Dry Sump)
- 17. Oil System Oil Cooler Oil Filter
- 18. Oil System Oil Cooler Smaller of the 2 filters
- 19. Electrical System (2) 12 Volt batteries, 14 VDC system, 40 amp Alt ** One Alternator can supply the entire load of the AC Refer to load shedding in POH
- 21. Fuel System 100 liters total capacity each tank, 97 useable. 52.8 Gallons Total Capacity; 51.3 Useable. Designed to be used with Unleaded Gasoline & 100LL.
- 22. Hydraulic/ Brake System ** Brakes are operated in Series!
- 23. Landing Gear
- 24. Landing Gear Hydro/electric Landing Gear Gear handle activates pump (electrically) Pump; gear pump hydraulically extends/retracts Gear. Pump is fully reversable, and is also the reservoir, Located in the empennage Up/Down Microswitches turn pump off/ on. Down switches illuminate green gear lights
- 25. Landing Gear Safety Mechanisms: • Squat Switch- prevents inadvertent gear retraction on ground if gear handle is moved to up position • Gear switch Detent- pull out and up/down • Gear warning horn- sounds if one of the 2 throttle levers are pulled to idle with gear raised; will also sound if flaps are set to full (land) with gear raised
- 26. Landing Gear (Emergency) Emergency gear retraction is controlled by accessing 2 T handles located on the floor of the left pilot station. Right T handle neutralizes pressure; Left Handle activates Nitrogen charge forcing the into the down and locked position