SP-CAD - 2009 ZLIN Z242L
Aircraft Summary
General
Year
2009
Manufacturer
ZLIN
Model
Z242L
Condition
Used
Registration #
SP-CAD
FlightRules
VFR
Description
Aircraft Purchased from Manufacturer. Approved for aerobatic maneuvers: stall, spin, loop, Immelman turn, half roll and dive out, stalled turn, slow roll, snap roll, whip stall, inverted flight, inverted turn, inverted loop from normal flight, inverted loop from inverted flight, inverted spin.
Load factor limits: +6 / -3,5 G.
Airframe
Total Time
110.0
Airframe Notes
Airframe 110hrs TTSN (TBO 3500h)
Always hangared
Adjustable rudder pedals
Banner/glider towing equipment
* EU VAT Paid
Engine
Engine Time
110
Engine Time Since
SNEW
Engine Notes
Lycoming AEIO-360-A1B6 with fuel injection
Rotating as viewed from the rear - CW
110hrs TTSN (TBO 1400h/12 years)
Props
Prop Notes
MTV-9-B-C/C188-18a with Woodward D-210 982 governor
Three blade, hydromatic, constant speed
110hrs TTSN (TBO 2400h/6 years)
Avionics
Avionics/Radios
- Garmin GMA 340 audio panel
- Garmin GNS 430 COM/NAV/GPS transceiver + Garmin GI 106A VLOC/GPS indicator
- Garmin GTX 328 Mode S transponder
- ELT Artex ME406 frequency 406 MHz
- airspeed indicator x2
- altimeter x2
- vertical speed indicator x2
- accelerometer
Additional Equipment
Additional Equipment
Equipped with SK-94 rescue parachute x2
Interior
Number of Seats
2
Inspection Status
Inspection Status
Airworthiness Review Certificate valid till 28.05.2014
Annual inspection valid till 28.03.2014
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