2006 Socata TBM 700
Single Engine Turboprop
Aircraft Details
Seller reportedAvionics & Equipment
Description
TBM-700C2 Best-in-Class, Ready to Fly Anywhere Meticulously maintained by the Daher CAO facility in Tarbes (Official Daher Service Centre) and kept in a private hangar from day one, this TBM-700C2 represents one of the finest examples on the market today. Highlights at a Glance New Luxury Interior excellent quality leather, elegant upholstery, refreshed trim, immaculate cabin Exterior recently polished Factory Avionics Upgrade (Daher, Tarbes) Garmin GTN 750xi and GTN 650xi + FlightStream 510 (Wi-Fi/iPad connectivity) LPV capable Bendix/King RDR-2000 weather radar digitally integrated with vertical profile in GTN 750xi Wx500 stormscope digitally integrated in GTN 750xi Radar altimeter and Integrated Terrain System (TAWS) GTX-345R and GTX-330D transponders with diversity and WAAS ADS-B In/Out A-20 box upgrade with modern aural alerts (gear, oxygen, stall, etc.) Digital intercom integrated in GTN 750xi with Bluetooth and music 120V cabin outlet Performance Safety Latest C2 Upgrade Package MTOW increased to 3,354 kg / 7,394 lb STOL capability for short and grass runways RVSM approved for efficient high-altitude cruise Bleed-air air conditioning certified FIKI (Flight Into Known Icing) Cockpit oxygen masks upgrade (MC-10) Recent Overhauls Propeller fresh overhaul, only 60h Main generator fresh overhaul, only 60h B+ annual inspection completed March 2026 at Daher Tarbes Records History All SBs ADs complied with Clean damage history. Single hail event while parked (RHS elevator) fully repaired by Daher Tarbes, documented Pre-purchase inspection welcomed at any official Daher Service Centre Logistics Worldwide ferry, delivery transition training available Sold from an EU company no VAT applicable for EU-to-EU company transactions Specs Total Time: 3,287 hours Engine Time: 3,280 hours Airplane time state: Total Time: 3,287 hours Engine Time: 3,280 hours
Engine
1 Engine, Turboprops
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 |
|---|---|---|---|---|---|---|
|
Marcos Jodar
planecheck.com
|
$1,235,000
|
Spain | May 03, 2026 | — | Active | |
|
Factory Avionics Upgrade
globalplanesearch.com
|
$1,235,000
|
MD | Apr 04, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Socata TBM 700
This 2006 Socata TBM 700 (F-HAMJ) is a single engine turboprop with 3,287 hours on the airframe. There are currently 29 TBM 700 aircraft listed for sale with asking prices ranging from $999,900 to $1,750,000. This aircraft is priced below the market average at $1,235,000.
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
Ownership & Registration
FAA registry covers US-registered aircraft (N-numbers).
This aircraft (F-HAMJ) is registered outside the US.
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 F-HAMJ.
Note: NTSB covers US-registered aircraft (N-numbers). This aircraft is registered in a non-US country (F-HAMJ). Safety records from the national aviation authority may not be included in our database.
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.