Description of the engines:
Engine:
Lycoming O-360-A1AD, rated at 180 hp
TBO 2000 hr or 12 years recommended
approx. 1130 SMOH compl. in 09/1996
Leak Test: 78/74/72/70 of 80 psi
Propeller:
Hartzell HC-C2YK-1BF/F7666A-2, 2-blade constant speed
TBO 2000 hr or 6 years recommended
approx. 260 SPOH compl. in 02/2016
Avionics:
Audio/Marker : Garmin GMA 340
COM/NAV: Garmin GNC 255A
GPS: Garmin aera 760
Transponder: Trig TT31 Mode S
ELT: Kannad 406 AF-Compact
Equipment:
Wheel fairings
FLARM
204 litres usable fuel
Digital logs
Exterior:
White and red with a dark blue fuselage stripe and red-and-white striped tail.
Interior:
Cognac-brown seats with red inserts, beige-brown side panels and red carpet.
Status of the inspection:'
Annual: August 2027
Maintenance: The latest annual / 100-hour inspection was released on 13 August 2026 at 2,304:32 total flight hours. The ARC is valid until 13 August 2027. The AD status report is dated 14 August 2026.
All four existing cylinders were repaired in May 2025, including new exhaust valve guides, exhaust valves and piston rings. The transponder and ELT were tested on 13 August 2026; the ELT battery is valid until August 2031.
Other comments:
History
Manufactured in 1979 as serial number 15, this Socata TB10 Tobago was previously registered as F-ODKD. Its German Certificate of Airworthiness was issued on 19 May 1980. The current Certificate of Registration is dated 17 June 2022.
Logbooks and maintenance records have been digitised and are available for review.
Damage History
1991: Propeller and governor overhauled following ground contact.
1996: Right wing repaired and reinstalled. The cause and extent of the repair have not been established.
Separate skin deformation at the left wing-to-fuselage junction, described in the 2025 maintenance report as known since 1996 and acceptable to SOCATA. The original manufacturer statement is not available.
Aircraft Subject to Prior Sale or Removal from Market without Notice. Specification Subject to Verification by Purchaser.
