1999 Socata TBM 700
Single Engine Turboprop
Aircraft Details
Seller reportedAvionics & Equipment
Honeywell EFIS 40 EADI & EHSI Garmin GNS530W #1 GPS/Nav/Comm WAAS Upgraded Garmin GNS530 #2 GPS/Nav/Comm BF Goodrich Skywatch TAS KFC 325 Three Axis Honeywell Digital Autopilot & Yaw Damper Autopilot Altitude Pre-Select Garmin GDL69 XM Satellite Weather Garmin MX20 MFD KT71 Mode-C #1 Transponder KT71 Mode-C #2 Transponder KN63 DME KR87 ADF RDR 2000 Radar WX 1000 Stormscope PMA 8000 PS Engineering Audio Select Panel Standby Vacuum Artificial Horizon KRA405 Radar Altimeter Artex ELT 1000
Description
jetAVIVA is pleased to present this Socata TBM700B, serial number 149. This TBM is equipped with updated Garmin avionics and features a six-place leather appointed interior in very good condition. Contact us for more information on this highly capable TBM700B.
Engine
Pratt & Whitney PT6A-64 TBO: 3,500 hours 3,250 Hours Since New
Propeller
Hartzell HC-E4N-3 4-Blade 450 Hours Since Overhaul
Interior
Six (6) Passenger Light Beige Leather High gloss woodwork throughout Executive writing table Six-place intercom system
Exterior
Metallic Forest Green and Autumn Brown Striping Factory Original
Modifications / STCs
• Electrically Powered Freon Air Conditioning System Socata Service Center Maintained
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 |
|---|---|---|---|---|---|---|
|
jetAVIVA
jetaviva.com
|
Contact for Price
|
PA | Apr 03, 2026 | — | 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 1999 Socata TBM 700 (N800GS) is a 6-seat single engine turboprop with 3,250 hours on the airframe. There are currently 26 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.
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.
Ownership & Registration
FAA registration data pending for N800GS.
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 N800GS against the NTSB accident 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.
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