2004 Socata TBM 700
Single Engine Turboprop
Aircraft Details
Seller reportedAvionics & Equipment
Garmin G600 Glass Panel with Synthetic Vision Dual Garmin GNS-530W NAV/COM/GPS WAAS Upgraded King KR87 ADF King KN63 DME Bendix King KRA-405 Radar Altimeter Garmin GTX-330 Transponder with ADS-B Out Garmin GTX-327 Transponder King KFC-325 Autopilot / Flight Director Honeywell KMD-850 MFD Honeywell KMH-880 IHAS
EGPWS and TAS Shading ETM-700 Engine Trend Monitor Garmin GDL-69A XM Satellite Receiver Bendix King RDR-2000 Weather Radar L3 WX-500 Stormscope Garmin GMA-340 Intercom Dual AM250 Altimeters
Description
jetAVIVA is excited to bring to market this gorgeous TBM 700C2. It features Garmin avionics upgrades, full engine enrollment on ESP gold, a well-appointed platinum edition leather interior refurbished in 2013, and a January 2018 A+ Annual inspection completed by Muncie Aviation, an Authorized Socata Service Center.
Engine
Pratt & Whitney PT6A-64 3,100 TT SNEW Fully enrolled on ESP Gold - $171/hr
Interior
All new leather, carpet and refinished sidewalls May 2013 Platinum edition, high comfort Tan leather seats, leather side panels, Blond wood overhead panel and executive table. Dual cabinets, including one cooler drawer
Exterior
Original Overall White with Kelly Green lower fuselage and Gold flying accents stripes
Inspection
January 2018 A+ Inspection by Muncie Aviation On Socata New Maintenance Program with extended 200-hour intervals
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
|
Pontiac, MI | 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 2004 Socata TBM 700 (N48UM) is a 6-seat single engine turboprop with 3,100 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 N48UM.
Location & Ownership
Aircraft Location
Pontiac, MI
MI
Seller reportedTitle 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 N48UM 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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