AIRFRAME

Airframe total time: 9816:20 hrs

ENGINES

Engines: 
LH: Textron-Lycoming IO-360-C1E6, sn L-1118-51A
TT: 10186, TSOH: 1025:48 overhauled by Mattituck in September 1998, 
RH: Textron-Lycoming LIO-360-C1E6, sn L-444-67A 
TT: 7693:38, TSOH: 1556:32 overhauled by Mattituck in July 1996
TBO: 2000 hrs / 12 Years (Calendar overhaul not mandatory in Switzerland for private operation. 
Also read new EASA Notice of Proposed Amendment (NPA) No 2011-15 for future "Non-binding guidance on TBO limits")
2 Bladed Hartzell Propellers: 
LH: CH -C2YK-2CGUF, sn AU13103B
TT: 5672, Time Since Overhaul: 79:25 hrs
Overhauled with New improved hubs in July. 2007. 
RH: HC-C2YK-CLGUF. sn AU13099B
TT: 6583:19, Time Since Overhaul: 79:25
Overhauled with New improved hubs in July. 2007. 
TBO: 2000 hrs / 6 Years. 
(Calendar overhaul not mandatory in Switzerland for private operation. 
Also read new EASA Notice of Proposed Amendment (NPA) No 2011-15 for future "Non-binding guidance on TBO limits")

IFR,
KMA20 Audio/MB,
2 x KX125 COM 760 Ch, FM Immune,
KN72 NAV,
KN75 ILS,
KCS55 HSI,
KR85 ADF with RMI,
KN62A DME,
Narco ELT10,
Garmin 330 Mode "S" XPDR,
ACK A30 Encoder,
Autocontr III Autopilot 3 ax coupled to HSI and VOR,
Intercom. Garmin GPS 155 TSO , approved for VFR/IFR enroute, B-RNAV, terminal and instrument approach (GPS, VOR, VOR-DME, NDB, NDB-DME) operation. Within the US National Airwspace System in accordance with AC 20-138 and such countries where GPS enroute, terminal and non-precision approaches are authorized by the appropriate airworthiness authority.
WX900 Strmscope,
Copilot instruments Airspeed, Attitude Indicator, Altimeter, VOR/GS, DG
Certified VFR Day/Night, IFR Category 1, B-RNAV (RNP 5)

Blue vinyle 9/10,
Gray fabric seats 9/10,
Pilot and Copilot Adjustable seats,
Blue carpet 9/10

Light gray with marroon stripes 7/10

Lightweight Surface Pneumatic De-icing system and propeller electrothermal de-icing system, 
Windshield hot plate, 
Pitot and stall warning heat system protected by landing gear switch
Propellers with dampers
Electric pitch trim installation, 
Logo light, 
Additional FOCA Approved 98 USG fuel tank for ferry flights. Increased MTOW approved for 4560 Lbs
Remaining Useful Load with full tanks and ferry tank: 453.45 Lbs

In good conditions. 
Landing accident with one main gear collapse and wing spar repair in performed in 1991 at TT: 6557 
Missing logs from 1972 to 1981, Prior to Swiss registration.
Replaced fuel tank vent line hoses 12/07
Next annual inspection due 12/08
EASA Certificate of Airworthiness
EASA Noise Certificate 74.8 dB(A)
Maximum Take Off Weight: 1905 kg - 4199.00 lbs
Empty Weight: 2960.55
Useful Load: 1235.45 Lbs
Fuel Capacity: 93 USG
WILL TRADE FOR ULM (Ultralight) Aircraft
Will sell with fresh 100 hrs annual inspection that will include:
fresh ARC
updated approved maintenance program
new battery
compliance with repetitive AD's
new nose baggage door lock
altimeters and pitot static test
avionics ramp test
magnetic compass swing
new ELT battery
nose gear trunnion 1000 hrs inspection
wing spar check
7 years inspection
magnetos 500 hrs inspection
new engine driven fuel pumps
one new electric fuel booster pump
many additional new items replaced