1950 Cessna 170A
Single Engine Piston
Aircraft Details
Seller reportedDescription
1950 C-170A, TTAF: 3,454.2, SM0H: 635.7 C-145-2. Annual, October 2025. Garmin portable GPS 660, GTR-225 com, 2 place intercom, GTX-335 ADS-B transponder. USB ports. Two ptt switches. Hooker harness seatbelts. New headliner, new seat rails installed last annual. Compressions: 1-76, 2-79, 3-78, 4-79, 5-79, 6-78.
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 |
|---|---|---|---|---|---|---|
|
Chris Sheriff
trade-a-plane.com
|
$106,900
|
Dubuque, IA | May 19, 2026 | — | Active |
Estimate Monthly Payment
Cessna 170A loan calculator
AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 170A
This 1950 Cessna 170A (N9969A) is a 4-seat single engine piston with 3,454 hours on the airframe. This aircraft is listed at the market average at $106,900.
The 170A cruises at 105 kts (194 km/h) with a range of 500 nm (926 km) — ideal for short hops and local flights.
Operating costs: Fuel burn is 9 GPH (34 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $50/hr in fuel alone. Total variable cost including maintenance reserves is approximately $130/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $18,000. With 3,454 hours on the airframe, this aircraft has exceeded TBO (2,000 hrs) — verify engine status and overhaul reserve.
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
Cessna 170A — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 170
AeroGurus estimates based on industry averages for the CESSNA 170. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N9969A.
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 N9969A against the NTSB accident database.
Service Difficulty Reports — Cessna 170A
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
CABLE BROKE AFT OF REAR PULLEY AND BULKHEAD. NO INSPECTION HOLES IN THIS AREA. (K)
NOSE LANDING GEAR LEG BROKEN AT FORWARD WELD ON SHOCK ABSORBER ATTACHMENT BRACKET. EXISTING INTERNAL CRACK. PROBABLE CAUSE, BAD WELD. (K)
LT MAIN GEAR WHEEL AXLE BROKE BETWEEN GEAR LEG AND WHEEL RACE. (GL11200505686) (K)
(CAN) UPON INSPECTION SEVERE CORROSION IN HUB CAVITY AND IN MOUNTING BORE. DIMENSIONS AT MINIMUM BEFORE REWORK. PROPELLER IS UNSERVICEABLE.
(CAN) LT UPPER ENGINE MOUNT BRACKET AFT OF FIREWALL EXTREME CORROSION (HALF OF BRACKET MISSING) VERY DIFFICULT TO SEE DUE TO INSULATION COVERING ON FIREWALL.
AIRCRAFT SUFFERED A LOSS OF OIL PRESSURE. TEARDOWN OF THE ENGINE REVEALED THE HYDRAULIC LIFTER BODY ON THE NR 5 CYLINDER HAD BROKEN.
RUDDER PEDALS WERE REMOVED TO FACILITATE OTHER MAINTENANCE. UPON REMOVAL, FOUND PEDAL ATTACH HOLES SEVERELY ELONGATED. TO REPAIR, A .125 INCH DOUBLER OF 6061-T6 WAS USED ON EACH SIDE OF THE PEDAL AS THE PEDAL PIN WAS JUST LONG ENOUGH TO ACCOMODATE ...
DURING ANNUAL INSPECTION FOUND HEAVY RUST ON ENDS OF BATTERY PACK WHERE TERMINALS AND CONNECTING BUSS BARS ARE SOLDERED. CORROSION WAS NOT VISIBLE UNTIL PACK WAS DISASSEMBLED (RENDERING IT NOT USABLE) BECAUSE CARDBOARD WAS GLUED OVER ENDS THEN WHOLE...
TAIL WHEEL SEPARATED FROM AIRCRAFT. INVESTIGATION FOUND ASSY HAD SEPARATED DUE TO BROKEN BOLT. BOLT HAD BEEN DYE CHECKED AT LAST ANNUAL DUE TO REPORT OF ANOTHER AIRCRAFT WITH BROKEN BOLT. THE BOLT CRACK DID NOT SHOW UP ON A DYE CHECK. SUBMITTER R...
ONE-PIECE VENTURI INSTALLED TO COMPLY WITH AD 93-18-03. AFTER INSTALLATION, AIRCRAFT WOULD NOT RUN SMOOTHLY, FUEL CONSUMPTION INCREASED ABOUT ONE AND ONE-HALF GALLONS PER HOUR. SUBMITTER STATED THAT THE AD SHOULD HAVE BEEN A MANDITORY INSPECTION AT...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
Similar Aircraft for Sale
