2007 Mooney M20M
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
IFRDescription
It would take just short of a novel to explain the whole story on this aircraft. We will try here, but give me a call if you want to go over any questions. A one-off Bravo unlike any other in existence. If you know Mooneys well, you will know that Mooney didn’t make a Bravo in 2007. While technically correct, this plane was actually certified airworthy and delivered in by Mooney in 2007. But that is just trivia. Here is what you really need to know about the plane. This plane was provided by Mooney to the guys at Garmin as an experimental aircraft in ‘03 in order to certify the G-1000 for the Mooneys. You may know, that the G-1000 was not available until 2005 models. Then, the aircraft went back to Garmin and they certified the GFC-700 Autopilot in the aircraft. You may also know that the GFC-700 was not available in a Mooney until the 2007 Models. As far was we know, it is the only Bravo in existence with the GFC-700 autopilot (unless someone paid the $75,000 price tag to upgrade from their STEC-55X). After Garmin finished, plane then went back to Mooney where it was serviced, brought up to new standards, and was production certified airworthy for the first time at 299 hours in 2007. Then it flew off to Firewall Forward in Colorado for engine work (Crakshaft AD plus a ton of other work including the STC for the Centrilube Camshaft!). Then back to Mooney for a redo of the interior prior to delivery to the first owner. The end result of all this; a one-off Bravo unlike any other in existence.
Engine
1825 Hours Total Time Since New! (Lycoming TIO-540-AF1B). 1525 Hours Since Firewall Forward Teardown to Replace Crankshaft. FFW Centrilub Camshaft installed while Crank was replaced. Compressions at September 2025 Annual Inspection: 74 / 77 / 75 / 74 / 76 / 77 Compressions at July 2024 Top Gun Aviation Annual Inspection: 79 / 76 / 76 / 77 / 76 / 77.
Propeller
1225 Hours Total Time Since New (3-Blade). Changed by Mooney under warranty
Interior
Grey Leather Seats with Grey Carpets. Seat Cushions and Leather Replaced in 2007 prior to delivery to the first owner.
Exterior
White over Black with Maroon and Silver Trim. Beautiful.
Inspection
Next Annual Due October 2026. Very Good Maintenance History. May 2007 Replacement of Crankshaft due to AD by Firewall Forward. STC for Centrilube Camshaft installed at the replacement.
Modifications / STCs
• TKS Known Ice Weeping Wing System, Monroy Long Range Fuel Tanks (118 Gallons Usuable), Charts and Safe Taxi, European Ready (with Mode S, DME and ADF), LED Landing and Taxi Lights (one each in both wings), LED Strobes), GamiJectors Fuel Injectors, Backup Alternator, 115 cf Factory Oxygen, Speed Brakes, Wing Sight-Fuel Guages, Dual Batteries, Dual Brakes.
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 |
|---|---|---|---|---|---|---|
|
GMax American Aircraft
controller.com
|
$299,000
|
Spring Branch, TX | Mar 25, 2026 | — | Active | |
|
GMax American Aircraft
controlleremea.co.uk
|
$304,264 *
GBP £225,971
|
Spring Branch, TX | Apr 08, 2026 | — | Active | |
|
GMax American Aircraft
aviationtrader.com.au
|
$308,219
|
Spring Branch, Texas, Australia | Apr 06, 2026 | — | Active |
* Converted to USD at daily European Central Bank (ECB) exchange rates
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Mooney M20M
This 2007 Mooney M20M (N18GX) is a 4-seat single engine piston with 1,825 hours on the airframe. There are currently 25 M20M aircraft listed for sale with asking prices ranging from $105,000 to $349,900. This aircraft is priced above the market average at $299,000.
Operating costs: Fuel burn is 16 GPH (61 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $88/hr in fuel alone. Total variable cost including maintenance reserves is approximately $180/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $22,000. With 1,825 hours on the airframe, this aircraft has 175 hours remaining to engine TBO .
NTSB records show 0 incidents for this airframe — a clean safety record. There are 4 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 M20M — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateMOONEY M20M
AeroGurus estimates based on industry averages for the MOONEY M20M. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N18GX.
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 safety data coming soon.
We'll check N18GX against the NTSB accident database.
Airworthiness Directives — Mooney M20M
ADs are mandatory safety instructions issued by the FAA. 4 recent ADs found for this aircraft type.
Mooney Airplane Company, Inc., (Mooney) Models M20M and M20R 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 M20J, M20K, M20M, and M20R Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Mooney M20M
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
AIRCRAFT CAME IN FOR ANNUAL INSPECTION WITH PILOT-REPORTED DISCREPANCY OF AVIONICS FAN CIRCUIT BREAKER INTERMITTENT TRIPPING AND #2 ALTERNATOR INTERMITTENT FAULT LIGHT. DURING PRELIMINARY SYSTEMS CHECK IT WAS DISCOVERED THAT THE AVIONICS FAN CIRCUIT ...
DURING INSPECTION, SEVERE INTERGRANULAR CORROSION HAS BEEN FOUND IN TWO PLACES ON THE UPPER MAIN SPAR CAP.
LOWER ENGINE MOUNT TUBE BETWEEN THE LOWER AFT MOUNTS WAS CHAFED APPROX HALFWAY THROUGH. INSPECTION REVEALED THAT AN OIL LINE ON THE BOTTOM REAR ENGINE THAT WAS ROUTED BETWEEN THE MOUNT AND THE FUEL CONTROL UNIT WAS THE CAUSE OF THE CHAFING. THERE IS...
DURING ANNUAL INSP THE ACFT WAS JACKED AND LANDING GEAR TESTED. EMERGENCY ESTENSION SYS TESTED. FOUND LOOSE NUT. FINGER TIGHT ONLY AT PULLEY WITHIN BELLY AREA FOR EMERGENCY EXTENSION SYSTEM PULL CABLE. ANA-7A BOLT, AN960-10L WASHER AND AN363-428 ...
TURBOCHARGER V BAND CLAMP PN NH1009399-10/40D23255-340M FOUND CRACKED .7500 THRU OUTER STRAP. AD2004-23-17, EFF. DATE 12/1/2004 CALLS FOR REPLACEMENT OF THIS CLAMP. THIS IS THE NEW STYLE CLAMP THAT WAS FOUND CRACKED. CLAMP OUTER STRAP CRACK IS WIT...
CUSTOMER SENT IN THE EXHAUST SYSTEM BECAUSE OF CRACKS FOUND IN THE WELDS OF THE RISER LEGS TO THE STACK TUBES OF THE NR 1 AND NR 2 SECTIONS. ADVISED CUSTOMER TO REPLACE COMPONENTS. CUSTOMER BOUGHT NEW PARTS AND BROUGHT THEM IN TO HAVE ATTACHING PIEC...
DURING PROP REMOVAL FOR A GROUND STRIKE, FOUND CRANKSHAFT WELSH PLUG LOGGED IN THE PROP HOUSING, RESTRICTING OIL FLOW TO PROP. ENGINE HAD BEEN INSTALLED 30 DAYS EARLIER, 4 HOURS SINCE INSTALL. (K)
COMBINATION VOLTAGE AND OVERVOLTAGE REGULATOR FAILED. THIS FAILURE CAUSED A VOLTAGE SPIKE IN THE ELECTRICAL SYSTEM WHICH IN TURN DAMAGED ALL OF THE COM AND NAV RADIOS, THE ANNUNCIATOR PANEL, AND NUMEROUS COMPUTER RELATED AVIONICS ITEMS. MULTIPLE LI...
AVIONICS BLOWER AND COWL FLAP BREAKER POPPED IN FLIGHT, UNABLE TO RESET. LANDING AND TAXI CIRCUITS DRAW 18 AMPS EACH AND WERE ROUTED THROUGH CIRCUIT BREAKER DISCONNECT WITH CONTACT RATING OF 13 AMPS EACH. THE OVERHEATED CONNECTION MELTED INSULATION O...
PILOT SEAT HEIGHT ADJUST BELL CRANK CRACKED AND SPLIT OPEN ON RT SIDE. THIS CAUSED SEAT TO LEAN DOWN TO THE RT. CRACK APPEARS TO START AT A WELD ON THE END OF THE TUBE. CRACK CONTINUED IN SPIRAL TOWARD ACTUATOR ATTACH POINT. OPPOSITE END OF TUBE ...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
Price History
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