C-GMKZ - 1979 MOONEY M20K 231
Aircraft Summary
General
Year
1979
Manufacturer
MOONEY
Model
M20K 231
Serial Number
25-0280
Registration #
C-GMKZ
Condition
Used
FlightRules
IFR
Description
**1979 Mooney M20K 231 – C-GMKZ**
A well-equipped 1979 Mooney M20K 231 offering the speed, efficiency, and high-altitude capability that has made the turbocharged Mooney a popular choice for serious cross-country flying.
Powered by the turbocharged, fuel-injected Continental TSIO-360 six-cylinder engine, C-GMKZ has approximately **1,186 hours SMOH** and only **65 hours since top overhaul**. The aircraft is equipped with a two-blade heated constant-speed propeller, built-in oxygen system, electric retractable landing gear, and 72 gallons of usable fuel.
The M20K 231 combines excellent cruise performance with Mooney’s famously efficient airframe. Its laminar-flow wing and direct torque-tube flight controls provide responsive handling while allowing owners to cover considerable distances without the fuel consumption associated with larger high-performance singles.
C-GMKZ is also well equipped for IFR and cross-country operations. The panel features a **Garmin GNS 430W WAAS GPS/Nav/Com**, Garmin SL30, GTX 330ES Mode S transponder with ADS-B Out, Century 41 autopilot, and an Edo-Aire Mitchell primary HSI. A Garmin GPSMAP 696 coupled with the 430W provides additional navigation capability, complemented by Garmin GXM40 XM Weather.
Additional equipment includes a PMA8000B audio panel, King DME and ADF, ACK 406 MHz ELT, and an EI UBG-16 engine analyzer.
The windscreen has also been upgraded with thicker replacement glass.
For a pilot looking for an efficient step-up aircraft with turbocharged performance, retractable gear, onboard oxygen, capable IFR avionics, and excellent cross-country capability, **C-GMKZ represents a compelling Mooney 231 opportunity.**
**Highlights:**
- Continental TSIO-360 turbocharged, fuel-injected engine
- 1,186 hours SMOH
- Only 65 hours since top overhaul
- Two-blade heated constant-speed propeller
- Built-in oxygen system
- Electric retractable landing gear
- 72 gallons usable fuel
- Garmin GNS 430W WAAS
- Garmin SL30 Nav/Com
- Garmin GTX 330ES Mode S / ADS-B Out
- Century 41 Autopilot
- Garmin GPSMAP 696
- Garmin GXM40 XM Weather
- PMA8000B Audio Panel
- Primary HSI
- King DME and ADF
- EI UBG-16 Engine Analyzer
- ACK 406 MHz ELT
- Upgraded thicker windscreen
Airframe
Total Time
3818
Max Takeoff Weight
2,899.08 lb
Complete Logs
Yes
Engine
Engine Manufacturer
CONTINENTAL
Engine Model
TSIO360A
Engine Horsepower
210 HP
Engine Time
1186
Engine Time Since
SMOH
Engine TBO
1800
Turbocharged
Yes
Engine Notes
65 Hours since Top Overhaul
Props
Number of Blades
2
Avionics
ADS-B Equipped
Yes
WAAS
Yes
Avionics/Radios
Garmin GNS 430W
Garmin GTX 330 ES Mode S Transponder
ADS-B Out
Garmin SL 30
Century 41 Autopilot
Garmin GPS 696, coupled to 430W
Garmin GXM40 XM Weather
PMA8000B Audio Control
Edo-Aire Mitchell primary HSI
King ADF
King DME
ACK 406 ELT
EI UBG-16 Engine Analyzer
Additional Equipment
Oxygen System
Yes
Inspection Status
Airworthy
Yes
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