8720 - 2009 TECNAM P2006T
Aircraft Summary
General
Year
2009
Manufacturer
TECNAM
Model
P2006T
Serial Number
011
Registration #
8720
Condition
Used
FlightRules
IFR
Description
Newly Certified, burning only 9-10 gallons per hour, the Tecnam P2006T is the perfect twin for flight schools and cross country travelers. It is a twin that makes sense! Place Your Deposit Today!
This is a general listing for the new Tecnam P2006T twin engine aircraft.
Quoted price includes ALL standard configuration equipment. Available in Analogue or Glass Cockpit (Garmin G950) Configuration for additional cost.
ABOUT THE AIRPLANE:
Dimension:
Wing...37.4 ft
Cabin width...49.2 inches
Length, overall...28.5 feet
Height, overall...9.3 feet
Engines...Rotax 912S3, 4 cylinders, 98 HP per side...92 continuous.
Tanks...2 tanks x 25.6 US gallons
Propellers...MT propeller, constant speed, full-feathering...2 blades
Design and weight loading
Standard equipped weight....1723 ilbs.
MTOW...2599 ilbs.
Useful load....880 ilbs.
Performance....
Max Speed sea level...148 knots
Cruise speed (75% 7000 feet) 140 knots
Cruise speed (65% 9000 feet) 135 knots
Rate of climb...1,140 ft/min
Rate of climb...single engine is 230 ft/min
Stalling speed...with flaps is 49 knots
Service ceiling...15,000 feet
Service ceiling...single engine 7,500 feet
Max. range at 65% power, 30 min reserve is 620 nm.
Take off distance...1213 feet
Take off run....898 feet
Landing distance....1279 feet
Landing run...656 feet
VLO....91 knots
VA...116 knots
VNE 168 knots
Fuel burn is 4.5 gallons on each side...
Airframe
Total Time
1113.0
Engine 1
Engine 1 Time Since
SNEW
Engine 1 Notes
- Manufacturer Bombardier-Rotax GmbH Model 912 S3
- Certification basis FAR 33 - Amendment 15
- Type Certificate EASA TCDS no. E.121 dated 1 April 2008
- Engine type 4 cylinders horizontally opposed with 1352 c.c. of overall displacement, liquid cooled cylinder heads, ram-air cooled cylinders, two carburetors, integrated reduction gear box with torsional shock absorber and overload clutch.
- Maximum power (at declared rpm) 73.5 kW (98.6hp) @ 5800 rpm –5 minutes maximum. 69.0 kW (92.5hp) @ 5500 rpm (continuous)
Props
Prop Notes
PROPELLERS:
MANUFACTURER MT PROPELLER
TYPE CONSTANT SPEED, FULL FEATHERING
NUMBER OF BLADES 2
MODEL MTV-21-A-C-F/CF178-05
Avionics
Avionics/Radios
IFR Equipped:
Garmin GNS 530 GPS/WAAS COM/NAV
Garmin GNS 430 GPS/WAAS COM/NAV
Two Garmin GI106A VOR-Glide Slope Indicators
Garmin GTX 328 Mode "S" Transponder
King KN 63 DME
S-Tec 55X Autopilot with electric pitch trim (NO Altitude Hold Function)
Artex ME 406 ELT with panel mounted remote switch
Pilot and copilot push to talk switch
Digital Clock
Full Co-Pilot instrument panel with folliwing instruments:
Attitude Indicator
Airspeed Indicator
Altimeter
Additional Equipment
Additional Equipment
TANKS:
FUEL TANKS STANDARD (USABLE) 2 x 25.6 US GAL
Exterior
Year Painted
2009
Exterior Notes
Like new
White with white stripes
Interior
Year Interior
2009
Number of Seats
4
Interior Notes
Like new
Light beige leather
Inspection Status
Inspection Status
- (ATA 05) Inspection A+B+C+D Performed
- (ATA 05) MLG dampers replaced pn 26-8-1110-000
- (ATA 05) Rudder Trim Actuator pn-7T replaced
- (ATA 05) Flush hydraulic fluid replaced
- (ATA 05) Weight fire extinguisher performed
- LG up down switch replaced. Pn MS24660-23D
- Fuel assy televel (aforador) RH pn 26-1-5100-000 replaced
- Hot air in cabin cable assy pn 29-9-0015-00 replaced
- Replaced LH and RH Orings brake caliper MS 28775-224
- Replaced LH and RH linings brake pn 066-11200 and rivets RA 105-00200
- Replaced Taxi Landing GE 4509 and Lamp assy A555A-V-14V
- Spark plugs LH and RH replaced pn DCPR8E
- Oil filter LH and RH replaced pn 825706
- Sb080-CS performed
- AD 2012-0043 performed iaw SB080CS
- Sb102-CS performed
- AD 2012-0146 performed iaw SB102CS
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