1966 Cessna 337B
Multi Engine Piston
Aircraft Details
Seller reportedDescription
Selling a Skymaster with several mods. Great Performer. Fresh Annual just completed 2310TT Front Engine 205 SBOH 730SMOH Rear Engine 103.5 SMOH Hangared in Southern KY NO TRADES
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 |
|---|---|---|---|---|---|---|
|
Calvin Wiley
trade-a-plane.com
|
$129,500
|
Summer shade, KY | Jun 02, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna 337B
This 1966 Cessna 337B (N5478S) is a 6-seat multi engine piston with 2,310 hours on the airframe. There are currently 3 337B aircraft listed for sale with asking prices ranging from $95,000 to $129,500. This aircraft is priced above the market average at $129,500.
The 337B cruises at 170 kts (315 km/h) with a range of 900 nm (1,667 km) — ideal for short hops and local flights.
Operating costs: Fuel burn is 18 GPH (68 L/h), which at current Jet-A prices (~$5.50/gal) means approximately $99/hr in fuel alone. Total variable cost including maintenance reserves is approximately $260/hr. Annual fixed costs (hangar, insurance, crew, annual inspection) average $25,000. With 2,310 hours on the airframe, this aircraft has exceeded TBO (1,500 hrs) — verify engine status and overhaul reserve.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 2 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 337B — Model Specs
Model specificationStandard specs for this model. Actual aircraft may differ.
Estimated Cost of Ownership
AeroGurus estimateCESSNA 337B
AeroGurus estimates based on industry averages for the CESSNA 337B. Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.
Ownership & Registration
FAA registration data pending for N5478S.
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 N5478S against the NTSB accident database.
Airworthiness Directives — Cessna 337B
ADs are mandatory safety instructions issued by the FAA. 2 recent ADs found for this aircraft type.
Cessna Aircraft Company (Cessna) Models 337, 337A (USAF 02B), 337B, 337C, 337D, 337E, T337E, 337F, T337F, 337G, T337G, M337B, F 337E, FT337E, F 337F, FT337F, F 337G, and FT337GP Airplanes
View full AD →Cessna Aircraft Company (Cessna) Models 336, 337, 337A (USAF 02B), 337B, M337B (USAF 02A), T337B, 337C, T337C, 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G, 337H, P337H, T337H, T337H-SP, F337E, FT337E, F337F, FT337F, F337G, FT337GP, F337H, and FT337HP Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna 337B
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
(CAN) ON INSP OF WING AD 78-09-05 WAS ACCOMPLISHED AND THE LT WING FWD SPAR AFT WEB WAS FOUND CRACKED.
WHILE INVESTIGATING A HYD FLUID LEAK IN THE NOSE WHEEL WELL, LOCATED CRACK IN THE RETRACT CYLINDER HEAD BETWEEN THE ATTACH BOLT/BUSHING BOSS AND THE BARREL THREADS, IN THE UPPER RADIUS. THERE WERE NO TOOL MARKS TO CREATE A STRESS RISER, AND NO HARD ...
RELEVENT INDICATION (CRACKED). (K)
ENGINE RUNNING ROUGH. COLD COMPRESSION CHECK SHOWED -0- COMPRESSION ON NR 6 CYLINDER. AIR LEAKING PAST EXHAUST VALVE. DISASSEMBLY REVEALED EXHAUST VALVE STUCK IN OPEN POSITION. EVIDENCE OF PISTON STICKING EXHAUST VALVE. THIS IS THE SECOND OCCURA...
ENGINE RUNNING ROUGH. PERFORMED COLD COMPRESSION CHECK. COMPRESSION WAS ZERO. AIR LOOKING PAST EXHAUST VALVE. REMOVED ROCKER ARM COVER, NOTED EXHAUST VALVE STICKING IN OPEN POSITION. REMOVED CYLINDER. PISTON HAD STRUCK EXHAUST VALVE. REPLACED ...
AFTER LANDING FROM A ROUTINE COMPANY FLIGHT, THE MAINTENANCE ENGINEER NOTED MORE THAN NORMAL OIL ON THE LT REAR COWLING. UPON FURTHER INVESTIGATION, A 3 INCH CRACK WAS DETECTED ON THE CRANKCASE HALF STARTING FROM THE ENGINE DRIVEN FUEL PUMP BOSS TO ...
(AUS) LH TRAILING EDGE FLAP CONTROL CABLE CONTAINED BROKEN STRANDS IN AREA APPROXIMATELY 25.4MM (1IN) FROM SWAGE AT BELLCRANK END.
(AUS) RT INBOARD FLAP CABLE CONTAINED BROKEN STRANDS LOCATED IN AREA APPROXIMATELY 25.4MM TO 38.1MM (1IN TO 1.5IN) FROM THE INBOARD BELLCRANK TURNBUCKLE.
WITH A HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT, THE NONE DRIVEN FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH THE MIXTURE LEVER IN IDLE CUT OFF, THE FUEL FLOW IS THE SAME AS IN FULL RICH. 3 TO 4MM/0.012 TO 0.016IN/ AWAY FR...
HIGHWING TANK CONNECTED TO THE FUEL PUMP INLET PORT. THE NONE DRIVE FUEL PUMP LEAKS REGARDLESS THE MIXTURE LEVER POSITION. WITH MIXTURE LEVER IN IDLE CUTOFF, FUEL FLOW IS SAME AS IN FULL RICH. 3 TO 4 MM/0.012IN TO 0.016IN AWAY FROM THE IDLE CUT OF...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.
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