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Cessna · 1961–1985

Cessna 185 Skywagon

BackcountryBush PlaneTaildraggerShort FieldLoad HaulerCross Country

Specifications

Cruise

145KTAS

Range

720nm

Seats

6

Useful Load

1550lbs

Full-fuel payload

1,046lbs

Fuel Burn

14.5gph

Fuel Cap.

84gal

MPG

11.5mpg

Stall (Vs0)

51KIAS

T/O roll

825ft

Ldg roll

610ft

Power

300hp

Engine

piston single

Gear

Fixed

IFR

Yes

Category

certified

Pricing

Typical

$250k

Range

$150k – $465k

Annual all-in

~$22k/yr

All-in estimate at ~100 flying hours a year — fuel, annual inspection, engine reserve, insurance, and hangar. It scales with your actual hours, and insurance and hangar vary most by region and pilot.

Cost to own — estimate

Set your yearly hours and local fuel price. Fixed costs (insurance, hangar, annual inspection) don't change with hours; fuel and the engine reserve do.

100
20300
$6.50
$3$10
Fuel (14.5 gph)
$9,425
Engine reserve (toward overhaul)
$2,471
Fixed (insurance, hangar, annual, subscriptions)
$10,104
Total per year
$22,000
Per flight hour
$220
Miles flown / year (at cruise)
16,686 mi
Cost per mile
$1.32/mi

Estimate, not a quote — insurance and hangar (the fixed bucket) vary most by region and pilot. Anchored to our model figure at 100 hrs and $6.50/gal.

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Strengths

  • Exceptional useful load (~1,500 lbs) for single-engine tailwheel
  • Proven Alaska bush capability on wheels, floats, or tundra tires
  • Strong parts and mechanic support across Cessna/Continental ecosystem
  • Legitimate 145 KTAS cross-country performer with 720+ NM range

Weaknesses

  • Tailwheel ground handling requires skilled pilots; not for novices
  • IO-520-D overhaul at TBO is expensive ($38,000–$58,000)
  • Age-related airframe corrosion (belly skins, float fittings) on used examples
  • Exhaust system cracking is recurring maintenance headache ($4,000–$6,000 per replacement)

Overview

The Cessna 185 Skywagon is, simply put, THE Alaska bush plane. Produced from 1961 to 1985 with over 4,400 built, the 185 is a 300-horsepower brute that can haul more than its own empty weight, operate from unimproved strips and water, and do it all with the reliability of a Cessna airframe backed by one of the most common engine families in general aviation. If the cessna-180-skywagon is the nimble mountain goat, the 185 is the pack mule that carries everything and everyone.

The 185 is essentially a strengthened Cessna 180 with a larger vertical fin and a fuel-injected Continental IO-520-D putting out 300 HP at takeoff (285 HP continuous). That extra 70 horsepower over the 180 translates directly into hauling capability -- approximately 1,500 pounds of useful load in a single-engine piston aircraft is remarkable, and it is one of the highest useful-load-to-empty-weight ratios in general aviation.

In Alaska, the 185 is ubiquitous. On floats, tundra tires, wheel-skis, or straight wheels, it serves as air taxi, freight hauler, hunting/fishing transport, and lifeline to remote communities. The aircraft's reputation for ruggedness and load-carrying ability has kept prices strong and rising for decades, even as the fleet ages. Well-equipped late-model A185Fs routinely sell for $300,000-$465,000, and demand consistently outstrips supply.

The 185 also saw military service as the U-17A/B with the US Army and was widely exported. Cessna produced the AgCarryall variant (1972 onward) with a chemical spray system for agricultural use, though most surviving AgCarryalls have been converted back to standard configuration.

Variants & History

VariantYearsEngineHPGross Weight (lbs)Key Changes
1851961Continental IO-470-F2603,200Initial production; IO-470 engine, 6 seats
185A1962Continental IO-470-F2603,200Minor refinements
185B1963Continental IO-470-F2603,200Minor refinements
185C1964Continental IO-470-F2603,200Minor refinements
185D1965Continental IO-470-F2603,200Minor refinements
185E1966 (early)Continental IO-470-F2603,200Last of IO-470 production
A185E1966-1967Continental IO-520-D3003,350IO-520-D introduced mid-1966; became standard 1967. Gross weight increase to 3,350 lbs. The defining upgrade.
A185F1973-1985Continental IO-520-D3003,350Camber-lift flaps, improved systems. The definitive production model and the most desirable variant.
AgCarryall (A185F)1972-1985Continental IO-520-D3003,350151-gal chemical tank, 30-nozzle spray booms, wire cutters, cable deflector. Agricultural variant.

The critical dividing line is the 1966 switch from the 260 HP IO-470-F to the 300 HP IO-520-D. Pre-IO-520 aircraft (185 through early 185E) are worth significantly less and perform notably worse, particularly on floats and at high density altitudes. The A185F (1973-1985) is the most sought-after variant, combining the 300 HP engine with the most refined airframe.

Performance

The 185's 300 HP Continental IO-520-D gives it authority that the 230 HP cessna-180-skywagon simply cannot match, particularly in demanding conditions. At high density altitudes and on floats, that extra 70 horsepower is the difference between a comfortable margin and a white-knuckle departure.

Book cruise is 145 KTAS at 75% power, burning approximately 14.5 GPH. At economy settings (57% power at 15,000 feet), fuel burn drops to 10.8 GPH with a TAS around 130 knots. The 84-gallon fuel capacity provides 720 NM range at 75% power and over 800 NM at economy cruise.

Takeoff ground roll of 825 feet at max gross (3,350 lbs) is respectable but notably longer than the lighter 180. With STOL modifications and operating below max gross, 400-600 foot departures are achievable. On floats, expect approximately 1,200-1,500 feet of water run depending on conditions.

Rate of climb at 1,075 FPM (sea level, max gross) is adequate but not spectacular given the weight. Lightly loaded, the 185 climbs substantially better. The IO-520-D maintains power better at altitude than the normally-aspirated O-470 in the 180, giving the 185 an advantage at mountain strip elevations.

The aircraft's spring steel gear is designed for abuse. The larger vertical fin (compared to the 180) provides improved directional stability, particularly on floats where the additional side area of the float installation demands more rudder authority.

Payload & Range

The Cessna 185's payload-range capability is one of its defining strengths and the primary reason for its dominance as a bush utility aircraft.

Full Fuel (84 gal / 504 lbs) + 2 Passengers:

  • Payload for pax + baggage: 1,046 lbs (two 200-lb passengers + 646 lbs cargo/baggage)
  • Range: ~720 NM at 75% power, ~850+ NM at economy cruise
  • This is an extraordinary combination -- two people, full fuel, and over 600 lbs of cargo. This is why the 185 is the Alaska workhorse.

4 Passengers + Reduced Fuel:

  • 4 x 200-lb passengers = 800 lbs
  • Remaining for fuel + baggage: 750 lbs
  • Max fuel: 84 gal (504 lbs) + 246 lbs baggage -- range ~720 NM
  • Practical: 65 gal fuel (390 lbs) + 360 lbs baggage -- range ~530 NM
  • The 185 handles 4 adults plus meaningful baggage with full or near-full fuel. Few single-engine aircraft can match this.

6 Passengers (all seats occupied):

  • 6 x 170-lb occupants = 1,020 lbs
  • Remaining for fuel: 530 lbs (~88 gal -- exceeds tank capacity of 84 gal)
  • Full fuel (504 lbs) + 26 lbs baggage: range ~720 NM
  • Remarkably, the 185 can carry 6 adults and full fuel and still be under gross weight. This is nearly unique among single-engine piston aircraft.

Bush Freight (pilot + max cargo):

  • Pilot (200 lbs) + 50 gal fuel (300 lbs) = 500 lbs
  • Remaining for cargo: 1,050 lbs
  • Range: ~330 NM
  • With cargo pod: add 150-250 lbs external capacity
  • This freight capacity is why Part 135 operators in Alaska built their businesses around the 185.

Float Operations (A185F on Wipaire 3000):

  • Float weight penalty: approximately 350-400 lbs (amphibious) or 200-250 lbs (straight)
  • Useful load on amphibious floats: ~1,150-1,200 lbs
  • Useful load on straight floats: ~1,300-1,350 lbs
  • Even on floats, the 185 carries more useful load than most landplane singles. This is the fundamental reason it dominates Alaskan float operations.

Comparison with cessna-206: The cessna-206 offers a wider cabin, larger cargo doors (the 206's double cargo doors are a major advantage), and comparable useful load. However, the 206 is a nosewheel aircraft and is noticeably slower on floats when loaded. The 185's tailwheel configuration gives it better rough-field capability, and its lighter empty weight translates to better float performance. For pure cargo access and loading ease, the 206 wins. For all-around bush utility including unimproved strips and float work, the 185 remains the benchmark.

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Mission Suitability

MissionScoreRationale
flight-training2Not a trainer. 300 HP tailwheel aircraft is too much for primary training. Advanced tailwheel transition only, and even then the 180 is more commonly used for training.
backcountry-bush10The gold standard for backcountry/bush operations. Highest useful load in the single-engine tailwheel class, proven float/ski capability, legendary ruggedness. This is the aircraft that built the Alaska bush flying tradition.
business-travel4Can cruise at 145 KTAS with IFR capability, but the tailwheel configuration, noise, and conventional-gear ground handling make it a poor business machine.
aerobatics2Utility category allows limited maneuvers. Not an aerobatic aircraft.
cross-country7Strong cruise speed (145 KTAS), excellent range (720 NM), IFR capable, and 84-gallon tanks make it a legitimate cross-country machine. The tailwheel ground handling and noise levels keep it from top scores.
cargo-hauling8One of the best single-engine cargo haulers ever built. 1,550 lbs useful load is extraordinary. The relatively small cargo door (18x20 inches) is the main limitation -- the cessna-206 wins on cargo access. Cargo pod STCs help.
Local Fun8300 HP taildragger flying is an experience. Responsive, powerful, and deeply satisfying for skilled tailwheel pilots.
surveying6High wing for ground visibility, stable platform. No dedicated survey features but perfectly adequate.

Avionics Ecosystem

The avionics picture on 185s mirrors the cessna-180-skywagon but with a bias toward more working-airplane configurations:

Working Bush Plane ($150K-$225K): Minimal IFR panel. Single nav/com (Garmin GNC 255 or older King KX-155), basic GPS (Garmin GPS 175 or aera 660 portable), ADS-B compliant transponder (GTX 345 or uAvionix skyBeacon). Many Alaskan operators strip panels to the bare minimum for weight savings and simplicity.

Mid-Range ($225K-$350K): Garmin GTN 650Xi or GNS 430W, GTX 345 transponder, GI 275 as primary flight display, basic autopilot. Capable of light IFR but primarily a VFR bush machine with weather capability.

Premium ($350K+): Full Garmin GTN 750Xi/650Xi stack, G500 TXi or dual GI 275s, GFC 500 autopilot, GMA 345 audio panel. These are typically late-model A185Fs with comprehensive restorations. They command top dollar from buyers who want the ultimate bush airplane with modern capability.

STCs & Modifications

The 185 modification ecosystem is even more extensive than the 180's, driven by the aircraft's professional utility role:

STOL Kits:

  • Sportsman STOL Kit (~$3,500-$5,500 installed): Leading edge cuff and gap seals. Significantly lowers stall speed and improves low-speed handling. The community favorite for 185s as well as 180s.
  • Horton STOL Kit (~$2,500-$4,000 installed): More modest cuff. Less aggressive than Sportsman but still beneficial.
  • Vortex Generators (~$1,500-$2,500 installed): Often combined with STOL kits. Improve slow-flight characteristics and reduce stall speed.

Tundra Tires:

  • Alaskan Bushwheel (29" to 35"): Standard equipment on serious bush 185s. The 185's stronger gear handles larger tires better than the 180.
  • Airframes Alaska complete landing gear kits: Extended gear legs, heavy-duty springs, and large tire packages purpose-built for the 185.

Engine Modifications:

  • Continental IO-550 STC (300 HP, modern variant): Drop-in replacement for the IO-520-D with improved reliability and parts availability. Some versions produce 310 HP.
  • Turbo normalizer STC: Maintains sea-level power to altitude. Significant performance improvement for mountain operations, though adds complexity and maintenance cost.

Float Installations:

  • Wipaire 3000 amphibious floats: The premier amphibious installation for the 185. Approximately $80,000-$120,000 installed. Gross weight on floats: 3,350 lbs (landplane) or higher with STC.
  • Edo 3430 straight floats: Classic straight float installation. Less expensive than amphibious but limited to water operations.
  • Aerocet floats: Composite construction, lighter than traditional aluminum floats. Growing in popularity.
  • The 185 on floats is the definitive Alaskan float plane. Its 300 HP ensures adequate performance even when loaded to gross on hot days.

Cargo Door STCs:

  • Several STCs exist to enlarge or add cargo doors, addressing the 185's main utility limitation. These range from enlarged baggage door openings to full cargo door conversions.
  • Cost: $5,000-$15,000 depending on the modification scope.

Cargo Pods:

  • Belly-mounted cargo pods add 150-300 lbs of external cargo capacity. Speed penalty of 5-10 knots.

Speed Modifications:

  • Various fairing kits (wheel pants, gear leg fairings, gap seals) can add 5-10 knots of cruise speed.
  • The "speed mod" packages with comprehensive fairings are popular on cross-country-oriented 185s.

Tail Modifications:

  • Scott 3200 heavy-duty tailwheel: Improved steering and durability for bush operations.
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Maintenance & Support

Parts Availability: Excellent. The Cessna 185 shares substantial parts commonality with the 180, 182, and 206 families. Airframe parts are widely available from Air Power Inc., Wag-Aero, Univair, and Cessna/Textron. Continental IO-520 engine parts are stocked by Continental Aerospace Technologies, Air Power Inc., and Superior Air Parts (PMA alternatives). Float-specific parts (Wipaire, Edo, Aerocet) are available from the respective manufacturers. See maintenance-ecosystem.

Mechanic Familiarity: Common. The 185 airframe is well-known to any Cessna A&P. The IO-520 engine is one of the most common high-performance Continental engines and is well-understood. Float rigging and inspection require some specialization but float-experienced mechanics are readily available in Alaska, the Pacific Northwest, Minnesota, and other float-flying regions.

Annual Inspection Cost: $3,000-$6,000 depending on shop, region, and squawks. Float-equipped aircraft inspections run higher due to additional float-specific inspections.

Expensive Maintenance Items:

  • Continental IO-520-D overhaul: $38,000-$45,000 (field overhaul) to $48,000-$58,000 (factory reman)
  • Propeller overhaul (constant-speed, 3-blade if equipped): $3,000-$5,000
  • Exhaust system replacement: $4,000-$6,000
  • IO-520 fuel injection servo overhaul: $2,000-$3,500
  • Float annual inspection and maintenance: $3,000-$7,000 (amphibious floats more expensive)
  • Crankcase replacement (if cracked): $8,000-$12,000 plus labor
  • Landing gear leg replacement: $2,000-$3,500 per side
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Valuation Factors

Year/Condition Tiers:

EraTypical Price RangeNotes
1961-1965 (IO-470, 260 HP)$150,000-$200,000Significantly less desirable. Lower power, lower gross weight.
1966-1972 (A185E, IO-520-D)$185,000-$280,000The 300 HP upgrade makes these viable bush planes. Good value.
1973-1985 (A185F)$250,000-$465,000The definitive variant. Last-of-production models (1983-1985) command highest premiums.

Key Value Drivers:

  • Engine time: Fresh IO-520-D overhaul adds $35,000-$42,000 vs run-out. Factory reman commands $45,000-$55,000 premium.
  • Float rigging: Wipaire 3000 amphibious float installation adds $60,000-$100,000 to aircraft value. Straight floats add $25,000-$40,000.
  • STOL modifications: Sportsman kit + tundra tires + gear upgrades add $8,000-$15,000 collectively.
  • Avionics: Full Garmin panel adds $25,000-$45,000 vs basic steam gauges.
  • Cargo door STC: Adds $5,000-$10,000 for utility-oriented buyers.
  • Paint and interior: Clean cosmetics add $8,000-$20,000 vs rough.
  • Logbooks: Complete logs from new are critical. The 185's professional-use heritage means many aircraft have changed hands frequently -- gaps in logs are common and reduce value 15-25%.
  • Alaska provenance: Alaskan 185s with documented professional use and good maintenance records can command premiums, as can aircraft with desirable N-numbers.
  • AgCarryall conversion: Former AgCarryalls converted to standard configuration sell at a slight discount unless the conversion is well-documented and the airframe shows no chemical damage.
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ADs & Common Problems

Active/Recurring ADs:

  • Seat Rail AD (AD 2011-10-09): Same as the cessna-180-skywagon -- repetitive inspections of seat rails, pins, rollers, and springs. Critical safety AD that applies across Cessna single-engine fleet.
  • Tailcone/Horizontal Stabilizer AD: Inspection for cracks and corrosion in tailcone and horizontal stabilizer attachment structure.
  • IO-520 Crankcase AD: Inspections for crankcase through-bolt torque and case cracking. The IO-520 is generally reliable but age-related case cracking is a known issue.
  • Fuel System ADs: Various ADs related to fuel selector valve and fuel system components.
  • Alternate Static Air Source Valve AD: Placard obstruction inspection.

Pre-Buy Red Flags:

  • Corrosion in lower fuselage belly skins -- especially on floatplane aircraft exposed to saltwater or lake water
  • Gear attach point fatigue -- the 185's higher gross weight puts more stress on gear fittings than the 180
  • IO-520 crankcase cracks -- inspect carefully with dye penetrant. Cases are expensive ($8,000-$12,000) and availability can be tight
  • Prop strike history -- check for any unlogged prop strikes. Engine teardown is required after a prop strike
  • Float fitting corrosion and wear on aircraft with float history
  • Exhaust system condition -- Continental exhaust systems crack and are expensive ($4,000-$6,000 for a complete system)
  • Firewall condition -- hard landing damage accumulates on working bush planes

Known Maintenance Items:

  • IO-520 fuel injection system requires careful maintenance and tuning
  • Magneto overhaul/replacement at TBO (~500-hour intervals for inspection)
  • Tailwheel shimmy damper wear
  • Exhaust system cracking (replace every 500-1,000 hours)
  • Continental IO-520 cylinder issues (ring wear, valve guide wear) -- monitor compressions carefully

Insurance Profile

The 185 falls into the same tailwheel/high-performance insurance category as the cessna-180-skywagon, with slightly higher premiums reflecting the higher hull values and 300 HP rating. See insurance-underwriting.

Typical Annual Premiums:

  • Qualified pilot (500+ TT, 100+ tailwheel, 50+ make/model): $1,945-$2,440 for $200K hull, $1M liability
  • National Cessna 180/185 Insurance Program (BWI): $1,845-$2,140 for qualified pilots
  • Low-time tailwheel pilot (200-500 TT, <50 tailwheel): $2,500-$3,500
  • New tailwheel pilot (<200 TT): $3,500-$6,500+; some carriers will decline

Underwriting Notes:

  • The IO-520-D's 300 HP rating triggers high-performance underwriting at most carriers. Insurers want to see demonstrated high-performance time.
  • Float endorsement and float time significantly affect rates for float-equipped aircraft. Expect 20-35% premium increase for float operations.
  • Commercial use (air taxi Part 135) requires commercial policies at substantially higher rates.
  • Make/model time is the single biggest premium reducer. The BWI National Cessna 180/185 program rewards experience with significant discounts.
  • Hull values on 185s have risen sharply. Ensure your hull coverage keeps pace -- an under-insured total loss is financially devastating at current market prices.
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