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Aircraft Summary
GEM Engine Monitor, Built in O2, 2 Axis Auto Pilot, IFR Certified, GNS 430


    Airframe: 1991 Socata TB-20 Trinidad
  • 2286 TT

  • Engine:
  • 1388 SMOH - March 2005 by Air West Aircraft
  • 250 HP Lycoming IO-540-C4D5D
  • s/n L-24366-48A
  • New engine mounts March 2005
  • Compressions
  • 10/22/08 - 78, 72, 42, 74, 76, 72 -- Replaced #3 cylinder exhaust valve, seat, and riser.
  • 4/20/09 - 71, 70, 74, 72, 73, 75
  • 8/14/09 - 76, 74, 76, 76, 76, 76
  • 6/2/10 - 76, 76, 76, 74, 74, 76
  • 10/5/10 - 75, 73, 72, 73, 68, 72
  • 10/6/11 - 78, 74, 65, 74, 74, 74

  • Prop:
  • SMOH: 1388 - March 2005 overhauled by United Propeller Technologies
  • 3-blade McCauley
Avionics
  • Audio Panel - King KMA-24
  • Com/Nav/GPS 1 - Garmin GNS 430 (coupled)
  • Com/Nav 2 - King KX 165
  • Autopilot/Flight Director - KFC 150 2-axis
  • Transponder - King KT76A
  • 3M WX-8 Stormscope (INOP)
  • Intercom - Symphony 4 place with Audio input
  • ARGUS 5000
  • Garmin GNS 430 coupled to ARGUS and Autopilot.
  • Insight GEM Engine Monitor
  • Fuel Flow Monitor
  • Built in Ox bottle with 4 canulas.
Additional Equipment
  • - AM/FM/CD radio,
  • - built in Oxygen bottle,
  • - Landing gear Power pack converted to American.
  • - Belly panel screws converted to English (vs. metric).
  • - High Intensity Landing and Taxi Lights “Boom Beam” from LoPresti
  • - Gami Injectors
  • -Aftermarket pilot side vent window
  • -All logs and additional pictures available upon request
Interior
  • Grey Leather front seats replaced 2010
Exterior
  • Good condition
  • Blue with White Base
  • Red striping
Remarks
  • Current owners purchased in 2007.
  • Overall Dimensions:
  • Maximum Span - 32.05 ft.
  • Total Length - 25.29 ft
  • Total Height - 9.35
  • Internal Cabin Dimensions:
  • Length - 8.3 ft
  • Maximum Width - 4.2 ft
  • Maximum Height 3.67 ft
  • Door - 2
  • Luggage Compartment Door - 2.1 x.1.44 ft
  • Airspeed Limitations
  • VNe - 189
  • VNo - 151
  • VLe - 140
  • VLo - 130
  • Va - 127
  • VFe - 100
  • Yellow Arc - 151-189
  • Green Arc - 64-151
  • White arc - 53-100
  • Maximum Take-off and Landing Weight - 2943lbs
  • Maximum Baggage Weight - 143lbs
  • Useful Load 1333 lbs
  • Total Fuel Capacity 88.8 Gallons
  • Usable Fuel 86.2 Gallons
  • DAMAGE HISTORY:
  • June 17, 1992 - TACH 83.3
  • Damage was sustained to the left wing from a runway light and propeller from the ground as the aircraft rolled out on landing. Factory new left wing was installed and the engine sent back to Lycoming for tear down inspection. All documented and signed off in the log books.
  • Inspection Status:
  • Annual completed 10/2011. Will provide fresh annual and IFR certification upon purchase.
  • Fuel Flow
  • MAX POWER
  • 75% - 15.9 (4h52m)
  • 65% - 14 (5h32m)
  • 55% - 12.3 (6h18m)
  • MINIMUM CONSUMPTION
  • 75% - 13.7 (5h39m)
  • 65% - 12.1 (6h24m)
  • 55% - 10.6 (7h19m)
 
 
 
 
 
 

 
Lone Mountain Aircraft
Henderson, NV 
Phone: (937)689-6586
Fax: (815)425-8991

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