1980 Socata TB10 Tobago
Single Engine Piston
Equipment & Features
- Seats
- 4
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Andrew Freeman
avpay.aero
|
$121,866
$121,511
|
— | Apr 05, 2026 | — | Active | |
|
Europlane Sales
planecheck.com
|
$109,950 *
€ 109,950
|
United Kingdom | May 03, 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 Socata TB10 Tobago
This 1980 Socata TB10 Tobago (G-IGGL) is a single engine piston with 4,200 hours on the airframe. There are currently 2 TB10 Tobago aircraft listed for sale with asking prices ranging from $60,904 to $121,866. This aircraft is priced above the market average at $121,866.
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 (G-IGGL) is registered outside the US.
Location & Ownership
Aircraft Location
Location not available
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 G-IGGL against the NTSB accident database.
Service Difficulty Reports — Socata TB10
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
(AUS) ENGINE CYLINDERS (4OFF) HAD TOP PISTON RINGS DELAMINATING. PLASMA FACE SECTION COMING AWAY FROM BASE MATERIAL. ALL 4 CYLINDERS ALSO HAD EXCESSIVELY WORN EXHAUST VALVE GUIDES AND 2 EXHAUST VALVES REQUIRED REPLACEMENT. (CASA NR 510001642)
FOUND TOP RUDDER HINGE CORRODED.
ENGINE MOUNT CRACKED. FOUND DURING INSPECTION IAW AD/TB10/8 AND TBSB NO 16/1.
RT STABILATOR HINGE CORRODED, AD/SB DESC: CASA SCHEDULE 5.
TOP COMPRESSION RINGS ON ALL PISTONS DELAMINATING.
NR 2 CYLINDER PISTON TOP COMPRESSION RING PLASMA COATING DELAMINATING. TOP RINGS ON ALL OTHER PISTONS SHOWING SIGNS OF DELAMINATION BEGINNING TO OCCUR.
(AUS) MAGNETO DRIVE SHAFT OUTER BEARING COMPLETELY DESTROYED. BEARING HAD BEEN RUNNING DRY FOR SOME TIME. SUSPECT MAGNETO ASSEMBLED WITHOUT GREASE IN THE BEARING. PERSONNEL/MAINTENANCE ERROR.
(AUS) LT UPPER AFT REAR SPAR WEB CONTAINED LIGHT EXFOLIATION CORROSIONIN AREA ADJACENT TO MAIN LANDING GEAR. FOUND DURING INVESTIGATION FOLLOWING CORROSION IN RT WING SPAR. SEE MDR 03/0900.
(AUS) RT WING MAIN SPAR AFT LOWER WEB CONTAINED EXFOLIATION CORROSION. CORROSION WAS MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR LEG.
(AUS) LT AND RT WING MAIN SPAR AFT LOWER WEBS CONTAINED EXFOLIATION CORROSION. CORROSION MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
Price History
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