1974 Cessna T207
Single Engine Piston
Aircraft Details
Seller reportedDescription
ENGINE: TSO 957.3 ON CONDITION DUE 27/04/2024 CALENDER PROPELLER: TSO 309.4HRS ON CONDITION DUE 14/01/2021 CALENDER
Engine
ENGINE: TSO 957.3 ON CONDITION DUE 27/04/2024 CALENDER
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 |
|---|---|---|---|---|---|---|
|
Amber Aero Engineering
controller.com
|
Contact for price
|
Tooradin, Victoria, Australia | Mar 25, 2026 | — | Active | |
|
Amber Aero Engineering
controlleremea.co.uk
|
Contact for Price *
Contact for Price
|
Tooradin, Victoria, Australia | Apr 04, 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 Cessna T207
This 1974 Cessna T207 (VH-PYG) is a 7-seat single engine piston with 8,518 hours on the airframe. There are currently 6 T207 aircraft listed for sale with asking prices ranging from $249,000 to $359,000.
The T207 cruises at 150 kts (278 km/h) with a range of 650 nm (1,204 km) — ideal for short hops and local flights.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 4 airworthiness directives applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Cessna T207 — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Ownership & Registration
FAA registry covers US-registered aircraft (N-numbers).
This aircraft (VH-PYG) 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 safety data coming soon.
We'll check VH-PYG against the NTSB accident database.
Airworthiness Directives — Cessna T207
ADs are mandatory safety instructions issued by the FAA. 4 recent ADs found for this aircraft type.
Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes
View full AD →Cessna Aircraft Company P206, TP206, TU206, U206, 207, T207, 210, P210, and T210 Series Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna T207
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
AIRCRAFT TAXIING THROUGH SHELTAIR RAMP AT KPMP PARKING RAMP AND THE PROPELLER CAME INTO CONTACT WITH A STACK OF 3 TO 4 RUBBER CONSTRUCTION CONES, WITCH RESULTED IN TWO OF THE THREE BLADES OF THIS PROPELLER TO BREAK FREE OF THE RETAINING RING CLIPS T...
SMOKE IN CABIN FROM ELECTRICAL SWITCH PANEL. CHAFED WIRE FOUND IN LEFT HAND WING LEADING EDGE NEAR RIB/SKIN JUNCTION. REPLACED WIRE, SWITCH AND CIRCUIT BREAKER. HOURS ON SWITCH UNKNOWN, WAS INSTALLED FEB. 10, 2013.
THE PILOTS REPORTED THAT HE SET TAKEOFF POWER, ENGINE PARAMETERS READ NORMAL AND UPON REACHING 40 KNOTS HE SAW A ROLL BACK. HE EXECUTED AN ABORTED TAKEOFF AND HEARD SOME ENGINE SPUTTERING FOLLOWED BY THE ENGING SHUTTING OFF. MAINTENANCE FOUND NO AB...
REMOVED ALL HYDRAULIC LIFTERS TO INSPECT FOR SPALLING, DISCOVERED BADLY SPALLED EXHAUST LIFTER ON CYLINDER #4. INSPECTED CAM IN ACCORDANCE WITH CONTINENTAL SERVICE DIRECTIVE SID05-1B, INSTALLED NEW LIFTER AND WILL INSPECT CAM AGAIN IN 100 HOURS. IT...
LEFT BRAKE FAILED, IT HAD WORKED FINE DURING RUN-UP. PILOT TOOK OFF AND THEN FOUND IT INOPERATIVE ON LANDING. LANDING WAS UNEVENTFUL.
THE ACFT WAS WRITTEN UP & INVESTIGATED MULTIPLE TIMES DUE TO FUEL SMELL IN THE CABIN. AFTER SEVERAL ATTEMPTS TO FIX THE PROBLEM, PROCESS OF ELIMINATION LED TO THE RT WING TANK LEAKING. BECAUSE THE ACFT HAD A FIBERGLASS TANK INSTALLED, THE WING & BU...
DUE TO LEAKAGE OF THE RT WING TANK, THE LT WING WAS REMOVED TO ACCESS & INSPECT IT'S FIBERGLASS TANK. ON TANK REMOVAL, IT WAS FOUND TO HAVE ONE LOCATION OF APPARENT CRACKING & LEAKAGE. DUE TO THE DIFFICULTIES INVOLVED IN ACCESSING THESE TANKS FOR I...
DURING A PREFLIGHT RUN UP, THE GOVERNOR WOULD NOT CYCLE THE PROPELLER EVEN WHEN LT IN THE LOW RPM POSITION FOR 10+ SECONDS. THE PROPELLER GOVERNOR WAS REPLACED WITH SERVICEABLE & OPERATIONS WERE NORMAL. THE GOVERNOR ONLY HAD 29.5 HOURS SINCE OVERHA...
DURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 2 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT.
DURING 100 HR INSPECTION BORESCOPED ENG & FOUND NR 3 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS TOWARDS EXHAUST VLV SEAT.
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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