“Christavia Mk4 is in very good condition, this aircraft has the O 360 A1A model of which was one of.
Item specifics
| Used |
| “Christavia Mk4 is in very good condition, this aircraft has the O-360 A1A model of which was one of the better engines Lycoming made. The engine logs are complete from 1970, engine was factory new at that time. The engine oil pressure is 80 psi and engine runs great, fires right up, excellent compressions. TTSN 2,089 TSOH 164. Useful load is 820 lbs., empty weight 1,430 lbs. Climb rate, over 1,000 feet per minute average load. Stalls at about 36 mph under 30 degrees of flap, very docile forward stall, cruise prop, cruises at 118 mph at 2,200 rpm, 138 mph at 2,550 rpm. Vne is 140 mph. The magnetos are due for rebuild in about 50 hours or so (approaching 500 hours). More avionics than the average aircraft! Not IFR certified, but could qualify with some changes and certification. Wing spars are made of wood. Selling because I have two aircraft and only need one, the other has more hp. and faster, but more expensive...” |
| Make: | CHRISTAVIA MK4 | Model Year: | 2009 |
| TTAF 162.4 Lycoming O-360 A1A (180 hp.) TTSN 2089 TSOH 164 - All cylinder compressions in the 70"s Sensenich 76EM8S-5-0 TTSN 1722.3 TS re-pitched 150.1 Very nice panel, docked Garmin 295 32 gal wing tanks total with aux. 12 gallon under rear bench seat. Adjustable main seats, deer skin covered rear bench seat. All passenger 4 pt. restraints. Early C-182 main landing gear with 8.50-6"s. Scott tail-wheel. Aero flash nav. lights/wingtip strobes. Aircraft is being flown regularly. Consider trade for motorhome of equal $ EQUIPMENT LIST: Standard 3 1/8” aeronautical gauges; heading, attitude, turn, airspeed, vertical airspeed, tachometer, altimeter (Falcon), and horizon indicator. Other gauges; oil pressure and temp, voltage and amperes, fuel (dual), OAT, CHT, EGT. Nav/Comm – Terra TXN-920/Indicator Comm – Icom ICA-200 Transponder – King KT-76A Intercom - PS Engineering PM501 Fast Stack – Approach Pro G Antennas – Internal - Advanced Aircraft ELT - ACK Technologies - E-01 EGT – Westburg Mfg. CHT – Westburg Mfg. Tachometer – Mitchell Aircraft Products Encoder – ACK Technologies-Model A30-4 PTT, both sticks. Fuel selector, L, R or both. Garmin 296, with docking station. Hour meter. Suction, 1” Wheels, axles and disc brakes, Matco Mfg. Toe brakes, pilot only. Parking brake, cylinder lock lever. Hinged windows, left and right. Flap activation lever, overhead, Johnson bar. Oil filter adapter, CL1000 Lycoming spin-on, STC SE01930NY. Alternator, Plane Power 65 amp. Starter, Sky Tech 122-12HT. Oil cooler, Positech P20003C. Battery, 12 volt Odyssey PC680. Magnetos, Bendix S-20 Series. Carburetor, Marvell Shebler MA-4-5. Induction air filter – Brackett. Complete engine and airframe logs, partial prop log. Have all equipment manuals. Last “condition report” done in December 2014. The "Annual" and/or "Condition inspection" is due in December. This aircraft is not certified at this time for IFR. There are some other minor instrumentation requirements. These include a slip/skid indicator (which it has), a clock that can accurately measure seconds (does not have, easily acquired), and IFR-certified navigation equipment suitable for the type of flight intended DME, VOR, (some of which it has). Note: If GPS is used, it must be installed in the aircraft and the databases have to be current (does not have, the Garmin 295 does not qualify). Other requirements include a mode C transponder (which it has), a gyroscopic heading indicator (which it has), navigation lights (which it has), pitot tube heat (does NOT have), sufficient fuel capacity (which it has). FAR 91.411 mandates a pitot-static system inspection every two years. According to the FAR"s, it meets the requirements for IFR flight as long as the componentry pass their required tests for the plane to be IFR-legal, it must ensure the instrumentation is accurate enough for IFR use. |