1970 Mooney M20F
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
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Description
Maintenance Condition: Annual Due: January 2027 Useful Load: 988 Lbs.
Airframe: 65 Gallons Modern Spinner with AD free Hartzell Scimitar Two Blade NAV Light Detectors Ram Air Induction Brackett AIr Filter Electric Flaps Electric Gear Overhead Lighting Full Length Rudder One Piece Windshield Same Fuselage Length as a 201 Rosen Vizors Innertia Reel front Shoulder Harnesses Throttle Quadrant Indiviual Reclining Rear seats Rear Seat Vents
Interior: Blue and Gray Vinyl and Fabric Seats with Matching Side Panels and Carpet. Overall Rated 8 Out of 10
Exterior: Overall White with Custom Retro Scheme with Metallic Blue Major Accent and Black Pinstripe. Overall Rated 9 Out of 10
History: Well maintained M20F. Same airframe as Mooney 201, same Fuel Capacity as Mooney 201. Airframe and interior in great condition, Clean paint. Mooney amazing performance of 1000 mile range at 8.4 gallons per hour and 150mph. Mooney safety with a full chromoly cage and one piece carry-through wing spar.
Interior
Blue and Gray Vinyl and Fabric Seats with Matching Side Panels and Carpet. Overall Rated 8 Out of 10
Exterior
Overall White with Custom Retro Scheme with Metallic Blue Major Accent and Black Pinstripe. Overall Rated 9 Out of 10
Inspection
Annual Due: January 2027 Useful Load: 988 Lbs.
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Listing Source
aso.com
|
$95,000
|
CA | Mar 14, 2026 | 1 days | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Mooney M20F
This 1970 Mooney M20F is a 4-seat single engine piston with 4,340 hours on the airframe. There are currently 26 M20F aircraft listed for sale with asking prices ranging from $29,000 to $157,500. This aircraft is priced below the market average at $95,000.
Operating costs: Fuel burn is 10 GPH (38 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $55/hr in fuel alone. Total variable cost including maintenance reserves is approximately $140/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $18,000. With 4,340 hours on the airframe, this aircraft has exceeded TBO (2,000 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 3 airworthiness directives applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Mooney M20F — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateMOONEY M20F
AeroGurus estimates based on industry averages for the MOONEY M20F. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
Registration number not available.
Location & Ownership
Title Status
No FAA title records
Available for US-registered aircraft only
Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.
Safety Record
NTSB database checked for this aircraft.
Airworthiness Directives — Mooney M20F
ADs are mandatory safety instructions issued by the FAA. 3 recent ADs found for this aircraft type.
Mooney Aircraft Corporation Models M20B, M20C, M20D, M20E, M20F, M20G, and M20J Airplanes
View full AD →Mooney Aircraft Corporation Models M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, and M20R Airplanes
View full AD →Mooney Aircraft Corporation Models M20F, M20J, and M20L Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Mooney M20F
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
DURING ENGINE OVERHAUL AND ANNUAL INSPECTION, THE R/H LOWER ENGINE MOUNT WAS FOUND CRACKED. THIS WAS HIDDEN UNTIL THE ENGINE MOUNT WAS REMOVED. RECOMMEND THAT MECHANICS VISUALLY INSPECT THE LOWER ENGINE MOUNT AREA WHERE IT AFFIXES TO THE FIREWAL, WIT...
NOSE/FRONT LANDING GEAR SHEARED AFTER ENCOUNTERING 2-DEGREE DRAINAGE INDENTURE/DIP WHEN TAXING FROM PARKING. EXAMINATION OF NOSE GEAR ASSEMBLY REVEALED THAT FRONT GEAR FORK/GEAR LEG OF THE NOSE GEAR ASSEMBLY (PN: 54004-505) AT WELDING POINT, JUST AB...
#1 FUEL INJECTION LINE CAME APART AT SOLDER JOINT BY INJECTOR B-NUT. CYLINDER SHUT DOWN IN FLIGHT AND CAUSED A FUEL LEAK. AIRCRAFT MADE EMERGENCY LANDING AT MILITARY INSTALLATION. PART IS 1029.9 HOURS SINCE NEW FROM FACTORY. REPETITIVE INSPECTION U...
LUG SUPPORT CRACKED AT LANDING GEAR ACTUATOR AFT ATTACH TO FUSELAGE ALLOWING FORE AND AFT MOVEMENT OF ACTUATOR. LUG MOUNTING HOLES ELONGATED IN BRACKET ASSEMBLY.
EXCESSIVE CORROSION FOUND IN THE MLG SPINDLE, UPPER TORQUE TUBE. CORROSION WAS HIDDEN BY PAINT AND DIRT. PAINT WAS REMOVED FROM THE GEAR SPINDLES IN PREPARATION FOR REPAIR AND REPAINT. IT WAS ONLY THEN THE DAMAGE WAS LOCATED. TWO OTHER SERVICEABLE SP...
DURING LANDING FLARE, PILOT'S CONTROL YOKE SEPARATED FROM THE CONTROL SHAFT. INSPECTION REVEALED THE SHAFT HAD SHEARED OFF AT THE HOLES FOR THE TAPER PIN HOLDING THE YOKE TO THE SHAFT. CONDITION IS THE SUBJECT OF AD 77-17-04. AIRCRAFT WAS IN COMPL...
DURING CRUISE FLIGHT, THE MIXTURE CONTROL ROD END SEPARATED FROM THE PRESSURE CARBURETOR CONTROL ARM, WHICH RESULTED IN POWER LOSS.
DURING TAXI NLG TRUSS SEPARATED FROM ACFT. DISCOVERED DURING RECORDS INSPECTION, IN 1999 THE TRUSS WAS R & R WITH A TRUSS WITH STOPS INSTALLED. THE ENTRY READS, REPLACED TRUSS WITH PN L540041-501. THE TAG READS REPLACED BENT TUBES, ADD STOPS, HEAT...
WHILE TAXING FOR T/O, THE NLG COLLAPSED, FOLLOWED BY BOTH MAIN GEARS. INSPECTION REVEALED THE LANDING GEAR RETRACTION LEVER ASSEMBLY SEPARATED AT THE WELD. THE WELD SHOWED SIGNS OF AN OLDER CRACK BEING PRESENT AT WELD, PRIOR TO COMPLETE FAILURE.
REPLACED SPINNER AND ADAPTER PLATE WITH PN 103585F2 WHEN PROPELLER HAD 29.96 TSMOH AND SINCE NEW THAT WAS INSTALLED IAW THE MM. DURING A RECENT ANNUAL INSPECTION, REMOVED THE SPINNER FOR INSPECTION AND LUBRICATION OF THE PROPELLER. FOUND CRACK EMAN...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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