Cessna 188

Piston • single engine • Low Wing • Fixed gear

Range Visualization

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

Payload vs. Range

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Avg. pax weight (lbs)

Default: 190 lbs (FAA standard)

Luggage per pax (lbs)

Default: 30 lbs

Passengers

lbs @ lbs / pax

Select payload

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

KTAS

Cruise Speed

Occupants

256

Max Range

lbs

Wet Payload

Estimated Ownership Costs

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About the Cessna 188

The Cessna 188 is a family of light agricultural aircraft produced by Cessna Aircraft Company between 1966 and 1983. The aircraft was designed based on feedback from pilots and operators, and its initial version borrowed heavily from the Cessna 180. The 188’s airframe is made of aluminum and fiberglass, and it was certified and entered production in 1966. Over its 17-year production run, the aircraft underwent minor changes, with a total of 3976 units built in four variants.

Technical Specifications

Dimensions

Wingspan: 41.7 ft
Length: 26.3 ft
Height: 7.7 ft

Weights

Max Takeoff Weight: 3,300 lbs
Max Landing Weight: 3,300 lbs
Fuel Capacity: 56 gal

Performance

Cruise Speed: 98 KTAS
Range: 256 NM
Service Ceiling: 11,100 ft
Rate of Climb: 690 fpm

Engines

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