2003 Socata TBM 700
Single Engine Turboprop
Aircraft Details
Seller reportedAvionics & Equipment
IFRDual Garmin G600 TXi Flight Deck with Dual GTN 750 XI PFD and MFD: Pilot and Co-Pilot Garmin G600 TXi Displays Comms: Dual Garmin GTN 750 XI Navs: Dual Garmin GTN 750 XI Autopilot: Garmin G600 Autopilot DME Honeywell KN-63 GPS: Dual Garmin GTN 750XI Radar: Garmin GWX 75 Transponder: Garmin GTX-345R w/ADS-B In and Out Transponder 2: Garmin GTX-330R w/ ADS-B Out Standby Instrument: Garmin GI-275 Weather and Music: Garmin GDL69 XM Remote Access and Automatic Database Updates: Garmin GDL 60 Engine Instruments: Garmin GEA-71B for displaying on GDU 1060’s
Description
Garmin G600 TXi Displays for Pilot and Co-Pilot • Dual GTN 750 XI • Garmin Engine Instruments • Garmin G600 Autopilot VIRTUAL TOUR (
Engine
2,135 Hours Total Time
Interior
Executive six seat interior, tan leather seating with tan sidewalls, high-gloss wood trim with retractable working table, baggage compartment with straps and net.
Exterior
White top, blue bottom with gold, black and red accent striping.
Modifications / STCs
• Dual Garmin G600 TXi/GTN 750 XI
• Synthetic Vision
• Garmin Smart Glide
• Pulse Anti-Collision Lights
• Battery Maintainer/Minder
• Voice Alerter
• Microkit Solutions Landing Height System
• LED Exterior Lights
• RVSM
• USB Plugins
• Rosen Visors
• Chartview
• (3) Cabinet Sets Available
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Steve Davis
avbuyer.com
|
Make offer
|
IL | Mar 16, 2026 | 124 days | Active |
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Socata TBM 700 loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Socata TBM 700
This 2003 Socata TBM 700 (N220MA) is a 6-seat single engine turboprop with 2,135 hours on the airframe. There are currently 27 TBM 700 aircraft listed for sale with asking prices ranging from $999,900 to $1,750,000.
The TBM 700 cruises at 300 kts (556 km/h) with a range of 1,350 nm (2,500 km) — suitable for regional and medium-distance travel. Service ceiling of 31,000 ft allows operation above most weather.
Operating costs: Fuel burn is 50 GPH (189 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $275/hr in fuel alone.
NTSB records show 0 incidents for this airframe — a clean safety record. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Socata TBM 700 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateSOCATA TBM 700
AeroGurus estimates based on industry averages for the SOCATA TBM 700. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N220MA.
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 N220MA.
Service Difficulty Reports — Socata TBM
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
STARTER/GEN FAILURE IN FLIGHT FORCING PILOT TO DECLARE EMERGENCY LANDING. UPON INSPECTION, STARTER BEARING FOUND THROUGHOUT STARTER HOUSING, ALONG WITH STATOR WINDINGS AND OTHER FOD MATERIAL. SPLINED SHAFT WAS ALSO SHEARED.
ELEVATOR LEADING EDGE DELAMINATION
LANDING GEAR PUMP FAILURE. GEAR WOULD NOT GO DOWN. USED EMERGENCY HAND PUMP TO EXTEND THE GEAR.
THE RUDDER TRIM TAB IS OPERATED BY AN ELECTRIC ACTUATOR AND CONNECTED BY A LOWER AND AN UPPER RUDDER TRIM TAB CONTROL ROD. AFTER RUDDER REMOVAL FOR ROUTINE INSPECTION, THE UPPER RUDDER TRIM CONTROL ROD DETACHED FROM THE ACTUATOR WHILE THE BEARING WAS...
ROLL PIN THAT HOLDS PINION GEAR ON SERVO DRIVESHAFT WORKED ITS WAY OUT SO THAT THE GEAR SLIPPED ON THE SHAFT AND THE SERVO WAS MECHANICALLY DISCONNECTED FROM THE FLIGHT CONTROLS. THE SYSTEM DID NOT PROVIDE ANY WARNING OF THIS FAILURE. IT IS ALSO LI...
PILOT DIVERTED TO PMP DUE TO LOST POWER FROM MAIN GENERATOR.
THE PILOT CHANGED SWITCH POSITION FROM AUTO TO MAX DIFF AND EXPERIENCED LOSS OF BLEED AIR. PILOT WAS ALERTED BY A BLEED OFF MESSAGE, CABIN PRESSURE BEGAN TO DECREASE. INITIATED A DESCENT, RESET BLEED, STABILIZED PRESSURIZATION AND MADE UNEVENTFUL LAN...
DURING ANNUAL INSPECTION, A TEST OF THE PASSENGER OXYGEN MASK DROP IS REQUIRED. PASSENGER MASK DEPLOYED @10,500 FT INSTEAD OF THE 12,500 REQUIREMENT. REMOVED AND REPLACED ALTMETRIC VALVE WITH OVERHAULED UNIT.
DURING ANNUAL INSPECTION, A FUNCTIONAL CHECK OF THE OXYGEN MASKS WAS PERFORMED. THE OXYGEN MASKS DROPPED AT 105000 FT INSTEAD OF 125. ALTIMETRIC VALVE REPLACED
ENGINE SLOW TO START, HANGING AT 33 PERCENT 50+ SECONDS TO START. CHANGED ACFT BATTERY SAME RESULTS. CALIBRATED FCU STARTS AT 38 SECONDS.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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