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Mooney M20K 252 ’87

Published by runwayalliance on July 2, 2019July 2, 2019

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by Dave Mathiesen
$114,900
Category
Sold
Location
Trenton Robbinsville (N87)
General Info
Make: Mooney Registration Number: N32DG
Model: M20K (252) Serial Number: 25-1128
Model Year: 1987 Engine: TSI0-360-MB1 (210 HP) 
Location: Robbinsville, NJ  (N87) Gear: Retractable (electric)
  Prop: Constant Speed
Summary Info
Well-equipped 252 with Garmin GNS 480, KAP 150 autopilot, altitude pre-select, roll steering, GTX 33 transponder, 2-blade heated prop, radar altimeter, JPI 700,  Hoskins fuel flow, and much more!
Logbook Time
Total Time: (Hours since New)      3028 Log books Complete:
    Yes
Engine: (Hrs SFRM)
     1420 Prop:  (Since Overhaul )     1420
Maintenance Info
Annual Due: (Date) July 2019
IFR Certification Due: Now
AD’s complete:
Yes
Other: Mooney Service Center maintained
Features
2-blade Hot-Prop Speed brakes
Factory Oxygen Stand-by vacuum system
Avionics
Make / Model
Nav/Com/GPS 1: Garmin GNS 480W
Nav/Com 2: King KX 165 with Glide Slope
GPS 2: Garmin 496 (panel mount)
HSI: King KCS-55A
Autopilot: King KAP 150
Altitude Pre-select King KAS 297B
GPSS Roll Steering: Icarus SAM (steering assist module)
Radar Altimeter: King KRA 10
Transponder: Garmin GTX 33 (remote)
Audio Panel: Garmin GMA 340
Weather: 3M WX-11 Stormscope
Engine Monitor: JPI EDM 700
Fuel Flow: Hoskins FT-101
Exterior
Color(s): White w/ Silver & Black trim
Paint Condition:
(1 to 10, 10 being the highest)
8
Interior
Color(s): Light Gray
Fabric: Leather
Condition:
(1 to 10, 10 being the highest)
7
Glass: Good
Performance
Cruise Speed: (at 75% power) 190 kts *
Useful Load: (remaining after full fuel) 450 lbs *
Fuel Capacity: 75 gal
Fuel burn: (average) 13 GPH *
Range: 900 nm *
Specific Range: ((Efficiency = Cruise Speed ÷ Lbs per hour of fuel burn) (The higher the number, the better the efficiency)) 2.37
*Note: Performance figures are estimates based on best available information (from POH, Vref, etc.) and may not be exact for this particular aircraft.
Comments
Mooney drivers share a unique and deeply seated characteristic – they like to go fast!  Mooneys are among the most efficient and structurally sound airplanes manufactured.  The low profile cross-section and laminar flow wings reduce drag to enable the fast air speeds typically unachievable in other manufacturers’ airplanes with similar horsepower.  The tubular steel frame, acting as a cockpit roll cage, along with the wingtip-to-wingtip wing spar make the Mooney airframe the strongest and safest among GA airplanes.

The M20K 231 was the first non-pressurized Turbo Mooney.  Introduced in 1979, the 231 (numbered for it’s top speed) was hailed as the fastest single-engine production aircraft in the world.  It was an instant success and even outsold the ever so popular Mooney 201 during the first two years of production.

For the 231, the Mooney engineers capitalized on the aerodynamic airframe improvements already added to the Mooney 201 by installing an engine with a high horsepower to weight ratio – the Teledyne Continental TSIO 360 GB. This combination of engine and airframe gave Mooney drivers the optimum blend of high altitude flying coupled with incredible speed and performance synonymous with Mooney Aircraft.  The 231 included other improvements such as the NASA air scoop placed in the dorsal for improved cabin ventilation, new wing tips for better slow-speed control and enclosed navigation and strobe lights. 

In 1984, Mooney upgraded the GB  engine with the TSIO 360 LB1B which included a redesigned fuel distribution system plus nitrited cylinders, steel belted pistons, and a new rod design that resulted in more efficient power and extended service life.

In 1985, Mooney’s engineers were tasked with making as many improvements as possible to the 231 and bringing to the market a vastly improved airplane in 1986 – the M-20K 252TSE.  Among the improvements were improved engine cooling and a redesigned primary air induction system.  Just as monumental, TCM listened to customers and made big improvements to the LB engine that resulted in the MB1 version. The changes were many.  Most important were a tuned induction system for more even induction airflow to the cylinders, a larger Garret turbocharger, a manifold pressure controlling system allowing full throttle operations for takeoff, and the incorporation of an intercooler that cooled induction air temperatures by as much as 100 degrees F.  The improvements resulted in the 252 that ran cooler than the 231, required only 36 inches of manifold pressure versus 40 with the 231, and flew 10 kts faster than the 231.

This 252 includes a very well-appointed panel with a KAP 150 autopilot, altitude pre-select, and roll steering that reduces pilot workload during cross-country flights.  The heated prop, factory oxygen, and radar altimeter further improves safety.  You really need to see and fly this airplane!

Contact Us About This Aircraft
Please call Dave Mathiesen at 609-259-2400
Show Contact Information

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