Cessna 195

Piston • single engine • High Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

150
KTAS
Cruise Speed
5
Occupants
800
nm
Max Range
800
lbs
Wet Payload

Estimated Ownership Costs

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About the Cessna 195

Overview

The Cessna 195 Businessliner is a five-seat, single-engine, conventional-gear aircraft manufactured by Cessna between 1947 and 1954. It was Cessna’s most ambitious postwar general aviation offering — priced above a Bonanza at introduction and aimed squarely at the business market. The 195 was the first Cessna aircraft constructed entirely of aluminium and features a fully cantilever wing with no struts. Three variants were produced, distinguished by engine: the base 195 (Jacobs R-755A2, 300 HP), the 195A (Jacobs R-755-9, 245 HP), and the 195B (Jacobs R-755B2, 275 HP). Just over 1,000 were built; approximately half remain flying. The aircraft also served with the US Army and Air Force as the LC-126/U-20.

Key Features for GA Buyers

  • Radial engine character: The Jacobs R-755 is a seven-cylinder, 775 cu in radial turning at a maximum 2,200 RPM. Smooth, distinctive, and — when well-maintained — reliable. The R-755B2 (195B) is generally regarded as the most dependable variant.
  • Cabin size: The fuselage width was driven by the 42-inch engine diameter, resulting in a genuinely roomy five-seat interior that punches well above its weight class for a 1940s single.
  • Semi-cabin-class fit and finish: Cessna positioned the 195 as near-cabin-class transportation. Front seats travel 15 inches fore-aft; the interior quality was exceptional for its era.
  • Retractable landing lights: Electrically actuated, arcing down from the wings — a feature later adapted to the Cessna 421.
  • Engine accessibility: The Jacobs mount swings open sideways, giving unusually good access to magnetos, starter, and generator.
  • Tailwheel handling: Any competent taildragger pilot can transition, but the high nose and offset seating require adjustment. Ground loops are the main accident cause; insurance reflects this.

Trade-offs

  • Radial operating costs: TBO is 1,000–1,200 hours (versus 1,800–2,000 for modern flat engines). Overhaul runs approximately $31,000. Oil consumption of up to 1 qt/hr is normal; budget accordingly.
  • Fuel burn: 12–19 GPH depending on power setting and engine variant. At a typical 14 GPH cruise the 76-gallon usable fuel supply yields roughly 520–780 nm of range.
  • Specialist maintenance required: Radial experience is not universal. Air Repair, Inc. (type certificate holder) and Radial Engines, Ltd. are the key support resources. Parts availability is adequate but not trivial.
  • Overheating on taxi: The tight cowl traps heat. In hot conditions or at large airfields, extended ground operations require care; a secondary oil cooler is a common owner modification.
  • Insurance: Ground loop history makes the 195 a challenging insurance proposition, particularly for lower-time taildragger pilots. Premiums are elevated relative to equivalent fixed-gear aircraft.
  • No modern avionics factory support: Cessna provides minimal support; owners are on their own for avionics upgrades and airframe parts sourcing.

See Also

  • Cessna 190 – smaller sibling with Continental W670 radial (240 HP); smoother but less supported. (Not yet in catalogue.)
  • Beechcraft V35B Bonanza – direct contemporary competitor at a lower price point: retractable gear, flat engine, higher cruise speed. Compare
  • Cessna 180 Skywagon – later Cessna taildragger: simpler flat engine, lower operating cost, less cabin space. Compare

Technical Specifications

Dimensions

Wingspan
36.0 ft
Length
27.0 ft
Height
7.0 ft

Weights

Max Takeoff Weight
3,350 lbs
Max Landing Weight
3,350 lbs
Useful Load
1,250 lbs
Fuel Capacity
75 gal

Performance

Cruise Speed
150 KTAS
Range
800 NM
Service Ceiling
18,300 ft
Rate of Climb
1200 fpm

Engines

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