Cessna 150 and 152 Performance: Compare the Conditions

Performance research begins by choosing the question. Cruise speed, range, climb rate and runway distance measure different aspects of an aircraft's capability. A single headline figure cannot answer all of them, and a model comparison becomes misleading when it mixes incompatible conditions.

View through a Cessna 152 windscreen on final approach to Wedderburn
A Cessna 152 on final approach to Wedderburn Airport. The cockpit view connects the instruments with the view toward the runway. Photo: Seaplane silly · Wikimedia Commons · CC BY-SA 4.0. Resized, WebP.

Choose the relevant performance measure

Use the focused references below to find the source records and their limitations. Cruise speed keeps power, altitude and units visible. Range preserves tank and reserve distinctions. Climb rate and service ceiling answer different altitude-performance questions.

Cessna 150 airborne just above a runway
A Cessna 150 taking off. This photograph illustrates the flight phase; it is not a source of takeoff distances or operating speeds. Photo: Navigator-avia · Wikimedia Commons · CC BY-SA 3.0. Resized, WebP.

Runway measurements need their own basis

Takeoff distance separates ground roll from obstacle clearance. Landing distance makes the same measurement distinction for the arrival. Do not compare a roll figure on one side with a total obstacle distance on the other.

Historical evidence and today's aircraft

The Cessna 150 family reference and Cessna 152 family reference retain the broader historical series. Published model-year specifications are useful research evidence, but the actual aircraft needs its applicable handbook, supplements and current configuration information.

Missing source conditions remain unresolved. The site does not infer fuel burn or endurance from a range headline, and it does not assign U.S. figures to Reims variants without explicit support. Aircraft loading, installed equipment and operational conditions must be established before using performance information for a flight.

For a purchase decision, connect this research with useful load and the buying guide. The aim is to compare the intended mission under compatible documented assumptions, rather than select the most favorable number from several unrelated configurations.

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Cessna 152 cockpit with two control wheels and a central radio stack
A Cessna 152 training cockpit with the instrument panel and both control wheels visible. This is one aircraft configuration. Photo: BestOnLifeform · Wikimedia Commons · CC BY-SA 4.0. Resized, WebP.

Fuel Flow, Endurance and Stall-Speed Conditions

Use the applicable aircraft handbook for fuel flow, endurance and stall speeds. Fuel consumption needs its power and altitude conditions; stall speed needs its weight, configuration and airspeed definition. The range summaries below answer a different question and cannot supply those missing operating conditions. Keep the stated fuel, reserve and obstacle assumptions with each figure when comparing aircraft.

The performance-reading guide explains which conditions must match before a numerical comparison supports a conclusion.

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