Cessna 152: Definition, Difference, Specifications, Design

Cessna 152 is a two-seat, single-engine aircraft designed for flight training purposes. The cockpit of the Cessna 152 provides an ergonomic layout optimized for pilot and instructor interaction. The engine delivers reliable performance to enable consistent takeoff and flight operations. A fixed-pitch propeller contributes to the aircraft's stability and efficiency during various phases of flight. Detailed information about the Cessna 152 exists in its official manual, detailing specifications and operational procedures. Understand the Cessna 152's design as a model specifically designed for trainer roles in aviation.

The Cessna 152 improves upon the earlier Cessna 150 model with key differences in performance and engine power. The Lycoming O-235-L2C engine powers the Cessna 152, producing 110 horsepower at 2,550 rpm. In contrast, the Cessna 150 relies on a Continental O-200-A engine generating 100 horsepower. The Cessna 152 achieves a maximum cruise speed of 105 knots compared to the Cessna 150's 95 knots. Climb rates differ, with the Cessna 152 reaching 715 ft/min (218 m/min) while the Cessna 150 achieves 670 ft/min (204 m/min). Maximum takeoff weight increases from 1,600 pounds (725.75 kilograms) in the Cessna 150 to 1,670 pounds (757.51 kilograms) in the Cessna 152.

Specifications of the Cessna 152 provide optimal performance during flight training and private flying. The aircraft measures 7.34 m (24.08 ft) in length, 10.16 m (33.33 ft) in wingspan, and 2.59 m (8.5 ft) in height. Two 13-gallon (49.21-liter) fuel tanks reside in each wing, providing a total fuel capacity of 26 gallons (98.42 liters). The fixed-pitch propeller enables a top speed of 127 mph (204.39 km/h) and a cruise speed of 123 mph (197.95 km/h). The service ceiling reaches 14,700 ft (4,480 m), and the range extends to 477 miles (767 km) or 795 miles (1,279 km) with long-range tanks. Stall speed measures 49 mph (78.9 kph) with flaps down and power off.

The cockpit of the Cessna 152 includes instruments and controls arranged for simplicity and reliability. The airspeed indicator displays speed in knots, while the altimeter measures altitude in feet. The attitude indicator shows pitch and roll orientation, and the turn coordinator provides rate of turn and slip/skid information. Engine instruments include a tachometer ranging from 500 to 2,500 rpm, an oil pressure gauge, and a fuel gauge displaying remaining fuel in gallons. Communication and navigation radios support VOR and ADF systems, and the transponder sends unique codes to air traffic control radar.

The cabin design of the Cessna 152 emphasizes efficient spatial arrangement. Cabin width measures 39 1/4 inches (99.7 cm), accommodating two occupants in a side-by-side seating configuration. The instrument panel features a clear "six-pack" layout, and controls: throttle, mixture, and carburetor heat are positioned within easy reach. Manually adjustable seats allow customization for varying pilot heights. The fixed tricycle gear system provides stability and facilitates ease of handling for novice pilots, making the aircraft suitable for short takeoff distances and small airfields.

What is the Cessna 152?

The Cessna 152 is a two-seat, single-engine, high-wing aircraft primarily designed for training and personal use, featuring a fixed tricycle gear system and renowned for its reliability and ease of handling. The Cessna 152 incorporates a fixed tricycle gear system, providing stability and ease of handling for novice pilots to learn. An upgraded 110 horsepower engine powers the Cessna 152 compared to its earlier model, the 150. The aircraft utilizes a fixed-pitch propeller, enabling a top speed of 127 mph (204.39 km/h), making it reliable for utility purposes. Aviation schools widely use the Cessna 152 due to its robust design equipped with minor changes from the earlier 150 series. The Cessna 152 serves as a popular choice for flight training due to its classic design and economical operation over a longer time between overhaul periods.

The Cessna 152 positions itself within the general aviation aviation sector as a versatile light aircraft category model. Flight training remains its primary function, with flight schools favoring it for initial flight training programs due to its stability and ease of handling. The Cessna 152 ensures reliability during operations while suiting the needs of private flying activities and sightseeing missions efficiently. Its lightweight design enables short takeoff distances, making it suitable for various airfields.

Key design features of the Cessna 152 include a high-wing configuration, fixed tricycle gear, and a cockpit emphasizing simplicity. The Lycoming O-235-L2C flat-four engine powers the aircraft, delivering 110 horsepower (82 kW). The Cessna 152 integrates two 13-gallon fuel tanks, one in each wing, and employs a 2-bladed fixed-pitch propeller system. Specifications highlight a maximum speed of 126 mph (203 km/h), a cruise speed of 123 mph (198 km/h), and a range of 477 miles (768 km), extendable to 795 miles (1,279 km) with long-range tanks. The service ceiling reaches 14,700 ft (4,500 m).

The Cessna 152 aircraft requires straightforward pre-flight checklist procedures, inspecting the engine, propeller, fuel system, and control surfaces. Pilots monitor speed, altitude, and fuel consumption during flight operations. The Cessna 152 simplifies operations with a basic cockpit layout, facilitating navigation for new pilots. Its stall speed measures 49 mph (79 km/h) with flaps down and power off, assuring safety during high-risk phases of flight.

The Cessna Aircraft Company manufacturer develops the Cessna 152, modernizing the earlier Cessna 150 model. The Lycoming O-235 engine enhances performance compared to the Cessna 150's Lycoming O-200 engine. Market considerations show the Cessna 152 price varying based on age, condition, and location. Older models cost $20,000, while newer or well-maintained models exceed $60,000. Reviews reflect its value and reliability, contributing to consistent Cessna 152 sales within the aviation network.

What are the differences between the C152 and C150 ?

The differences between the C152 and C150 are explained in the table below.

Performance differences speed favor the Cessna 152, achieving a max cruise speed of 105 knots compared to the Cessna 150's 95 knots. Performance differences in climb rate highlight the Cessna 152’s superiority, with a rate of 715 ft/min (218 meters/min) versus the Cessna 150's 670 ft/min (204 meters/min). Engine differences in powerplant distinguish the two aircraft . The Cessna 150 relies on a Continental O-200-A engine producing 100 horsepower, classified as a Cessna 150 baseline engine. In contrast, the Cessna 152 utilizes a Lycoming O-235 engine initially rated at 110 horsepower, later adjusted to 108 horsepower, representing a Cessna 152 upgraded engine. Engine differences horsepower directly influence performance metrics: speed and climb rate. Fuel efficiency differences in fuel consumption show the Cessna 150 consuming 5.6 gallons (21.2 liters) per hour, while the Cessna 152 burns 6.1 gallons (23.1 liters) per hour. Weight differences in empty weight and loaded weight vary between the two models. The Cessna 152 has a higher maximum takeoff weight of 1,670 pounds (757.5 kilograms), surpassing the Cessna 150's 1,600 pounds (725.7 kilograms). Despite this, there is no evidence of Cessna 152 reduced weight initiatives. Seating configuration and seat layout shows no changes, maintaining a standard arrangement typical of light training aircraft. Neither model features a Cessna 152 optimized seating configuration. Avionics differences in instrumentation between the Cessna 150 and Cessna 152 reflect their respective eras of production. The Cessna 152 does not include Cessna 152 advanced avionics as a standard feature but benefits from potential aftermarket upgrades. Avionics differences in navigation systems remain consistent, emphasizing simplicity and reliability for training purposes.

The differences between the C152 and C150 include variations in engine power, cruise speed, climb rate, fuel consumption, and maximum takeoff weight.

Can a Cessna 152 be used as a bush plane?

The Cessna 152 can be used as a bush plane, but its suitability depends on modifications, payload capacity, and STOL capability. The Cessna 152 lacks robust landing gear and STOL capability, requiring 1,410 feet (430 meters) for takeoff and 1,085 feet (331 meters) for landing over a 50-foot (15-meter) obstacle. Modifications like larger tundra tires enhance off-airport performance but do not fully address its design limitations. The aircraft's payload capacity of 589 pounds (267 kilograms) restricts its ability to carry heavy cargo vital for bush operations. A Lycoming O-235-L2C engine producing 110 horsepower provides adequate power but struggles with demanding short-field performance typical in bush flying. The Cessna 152’s range of 477 miles (767 kilometers) further limits its utility for extended bush missions requiring greater endurance.

The Cessna 152 weight distribution includes an empty weight of 1,081 pounds (490 kilograms) and a maximum takeoff weight of 1,670 pounds (757 kilograms), leaving a payload of only 589 pounds (267 kilograms). This limited Cessna 152 payload restricts the aircraft's ability to carry important cargo or passengers over extended distances typical in bush environments. The stock landing gear of the Cessna 152 lacks robustness required for rough terrain, featuring fixed tricycle gear with small tires and moderate shock absorption. Bush plane robust landing gear incorporates high-strength components and large-diameter tires designed for unprepared surfaces, which the Cessna 152 gear cannot replicate without extensive modifications.

The Cessna 152 landing distance under standard conditions requires 1,085 feet (331 meters) over a 50-foot (15-meter) obstacle, while the ground roll during landing measures 400 feet (122 meters). These figures exceed the capabilities of dedicated STOL aircraft, making the Cessna 152 unsuitable for confined areas common in bush operations. Stol capability short-field performance is not inherent to the Cessna 152 design, as the aircraft needs 1,410 feet (430 meters) for takeoff over a 50-foot obstacle and a ground roll of 690 feet (210 meters). The Cessna 152 wing offers stable handling for training but lacks high-lift devices necessary for extreme maneuverability in bush scenarios. Modifications like tundra tires, vortex generators, or reinforced landing gear boost off-airport capability but do not fully address the fundamental limitations of the airframe.

The Cessna 152’s larger tires and structural reinforcements enhance the ability to operate on soft or uneven surfaces but fail to match the all-terrain performance expected from true bush planes. The Cessna 152 range of 477 miles (768 kilometers) imposes further constraints on endurance during extended missions. Operators report issues with cargo capacity, as the limited payload restricts fuel and supplies needed for remote operations. The Cessna 152 wingspan of 33 feet 4 inches (10.16 meters) contributes to stability but does not compensate for the lack of specialized features found in purpose-built bush aircraft.

What are the specifications of the Cessna 152?

The specifications of the Cessna 152 are given in the table below.

These weight specifications provide optimal performance during flight training and private flying.

The specifications of the Cessna 152 include dimensions, engine details, performance metrics, and its significance as a popular aircraft for flight training. Powered by a Lycoming O-235-L2C engine producing 110 hp (82 kW), the aircraft achieves a maximum speed of 126 mph (203 km/h, 109 kn).

How fast does a Cessna 152 fly?

The Cessna 152’s cruise speed is 123 mph (198 km/h) and a maximum speed 126 mph (203 km/h). Factors like weight, weather, and altitude affect the airplane's performance.

The Cessna 152 achieves a maximum speed of 126 mph (202.77 km/h) - maximum speed at sea level, while maintaining a cruising speed of 123 mph (197.94 km/h) - cruising speed at 14,700 feet (4480.16 meters) at higher altitudes. Specifications note a cruising airspeed of 105 kts (198 km/h) - cruising airspeed per Cessna's specifications. During typical flight operations, the aircraft flies relative to the air at 115 mph (185.07 km/h) - typical flying speed relative to the air. Adhering to safe operational limits requires attention to key performance thresholds. The Cessna 152 enforces a "do not exceed" speed of 149 kias - do not exceed speed to prevent structural damage, along with a maximum structural cruising speed of 111 kias - max structural cruising speed for prolonged flights. Stall speeds vary based on configuration, with a power-off, flaps-down stall speed of 49 mph (78.85 km/h) - stall speed (power off, flaps down) and a clean stall speed of 48 knots (88.9 km/h) - stall speed clean. These values directly influence flight planning and safety margins. The aircraft achieves a typical takeoff speed of 55 kts - takeoff speed, providing efficient performance during important phases of flight.

What is the range of a Cessna 152?

The range of a Cessna 152 airplane depends on fuel capacity, altitude, and power settings. With long-range tanks, the Cessna 152 achieves a maximum range of 415 nautical miles (768 kilometers) at 10,000 feet (3,048 meters). Standard configurations provide a range of about 320 nautical miles (592.6 kilometers) at 8,000 feet (2,438.4 meters).

The standard range of a Cessna 152 equals 477 miles (767 kilometers) under optimal conditions, making it suitable for short cross-country flights. With optional long-range tanks installed, the ferry range extends to about 795 miles (1279 kilometers), allowing for longer-distance operations. The range at 3048 meters with 92.7 liters of usable fuel achieves 768 kilometers, while the same altitude with 142 liters of usable fuel increases the range to 1009 kilometers (The range at 10000 feet with 24.5 gallons of usable fuel achieves 415 nautical miles, while the same altitude with 37.5 gallons of usable fuel increases the range to 545 nautical miles). Pilots flying at 8,000 feet (2,438 meters) with 75% power achieve a range of about 350 nautical miles (648 kilometers), which aligns closely with the best range of 315 nautical miles (583 kilometers) under similar power settings.

The maximum range at 3,048 meters (10,000 feet) reaches 685 kilometers (370 nautical miles) under specific power settings, demonstrating the aircraft's adaptability to varying flight conditions. Modified aircraft achieve ranges up to 650 miles (1046 kilometers) under optimal conditions, while the theoretical maximum range with long-range tanks and ideal conditions extends to 690 nautical miles (1278 kilometers). The Cessna 152 serves as a popular aircraft for flight training due to its reliability, ease of handling, and cost-effectiveness. Several factors influence the range of the Cessna 152, including altitude, power settings, and fuel capacity.

What is the service ceiling of a Cessna 152?

The service ceiling of a Cessna 152 is 14,700 ft (4,480 m) under standard conditions. The service ceiling remains unaffected by optional fuel configurations, but the range increases with long-range tanks. Non-ideal atmospheric conditions reduce the service ceiling to 14,400 ft (4,389 m). Maximum takeoff weight lowers the service ceiling to around 13,500 ft (4,115 m). Reduced engine performance decreases the achievable altitude to about 14,000 ft (4,267 m). Pilots rarely operate above 9,500 ft (2,896 m) due to diminished climb performance and higher fuel consumption. Optional fuel configurations do not affect the service ceiling but increase the range. Reduced engine performance decreases achievable altitude to around 14,000 ft (4,267 m). Pilots avoid flying above 9,500 ft (2,896 m) due to diminished climb performance and increased fuel consumption.

What is the glide ratio of a Cessna 152?

The glide ratio of a Cessna 152 is 9:1 under standard atmospheric conditions in clean configuration. The aircraft glides 9 feet (2.74 meters) forward for every 1 foot (0.30 meters) of descent under ideal conditions. High-density altitude reduces the glide ratio to 8:1 in clean configuration. Optimal angle of attack in calm wind conditions improves the glide ratio to 10:1. Extended flaps and turbulent air reduce the glide ratio to 7:1. Experimental maximum glide ratio reaches 11:1 under theoretical ideal conditions.

High-density altitude reduces the glide ratio of the Cessna 152 to 8:1 in clean configuration. Less dense air at high altitudes decreases lift relative to weight, directly impacting glide performance. Optimal angle of attack in calm wind conditions improves the glide ratio to 10:1. Achieving this angle allows the aircraft to maintain efficient lift and forward motion. Extended flaps and turbulent air reduce the glide ratio to 7:1 due to increased drag and unpredictable airflow. Flaps create additional resistance while turbulence disrupts stable gliding. Experimental maximum glide ratio reaches 11:1 under theoretical ideal conditions with perfect aerodynamic efficiency. Real-world pilot performance during simulated engine-out scenarios lowers the glide ratio to 6:1. Turbulence and imperfect technique contribute to reduced glide performance in practical situations. The best glide speed of the Cessna 152 is 60 KIAS, influencing its optimal glide ratio under various conditions. Glide ratios vary based on aircraft weight, configuration, and atmospheric factors. Precise data requires consultation of specific flight manuals or conducting controlled flight tests.

What engine powers the C152?

The engine that powers the C152 is the Lycoming O-235. The Lycoming O-235-L2C engine produces 110 hp at 2,550 rpm. The Lycoming O-235-N2C engine generates 108 hp at a similar RPM. The Lycoming O-235 engine features a four-cylinder, horizontally opposed piston design. The Lycoming O-235 engine is air-cooled and utilizes a carburetor for fuel delivery. The Lycoming O-235 engine has a displacement of 233.3 cubic inches.

The Lycoming O-235 engine cylinders are arranged in two pairs opposite each other, supporting balance and reducing vibration. The engine incorporates a pushrod-actuated valvetrain and utilizes a carburetor for fuel delivery. Air-cooling ensures efficient temperature regulation during operation. The air-cooled system eliminates the need for complicated liquid cooling mechanisms, simplifying maintenance. Carburetor-based fuel delivery provides precise control over the air-fuel mixture. These attributes highlight the engine’s suitability for training and light touring aircraft. Maintenance considerations focus on regular inspections and timely part replacements to assure longevity.

The Lycoming O-235 engine displacement supports the engine’s ability to deliver consistent power output. The engine runs on 80/87 avgas, a common fuel type for aircraft engines of its class. Higher octane fuel is sometimes recommended to optimize performance under specific conditions. The Cessna 152 requires a minimum of 100 octane fuel in certain scenarios. Lycoming O-235 engine fuel type compatibility ensures reliable operation across various flight conditions.

What does a C152 cockpit include?

A C152 cockpit includes important flight instruments, engine controls, navigation systems, and communication tools designed for safe operation. The airspeed indicator displays the aircraft's speed in knots, assuring precise monitoring of flight speed relative to the air. The altimeter measures altitude above sea level in feet, providing essential data for safe navigation and terrain avoidance. The attitude indicator shows the aircraft's pitch and roll orientation, enabling pilots to maintain control during varying flight conditions. The turn coordinator indicates the rate of turn and slip/skid information, aiding in coordinated flight maneuvers. The vertical speed indicator measures climb or descent rates in feet per minute, allowing accurate altitude adjustments.

The engine instruments panel includes gauges monitoring RPM, cylinder head temperature, and oil pressure. The tachometer measures engine revolutions per minute, ranging from 500 to 2500 rpm for the Cessna 152’s engine, assuring optimal engine performance. The oil pressure gauge monitors pressure in pounds per square inch, preventing potential engine damage. The fuel gauge displays the remaining fuel quantity in gallons (94.64 liters), with the aircraft having a total capacity of 26 gallons (98.42 liters), aiding in effective fuel management.

The communication radio allows pilots to set frequencies for air traffic control and unicom stations, enabling clear communication. The navigation radio supports systems like VOR and ADF, enabling precise electronic navigation. The transponder squawk code and identification sends unique codes to air traffic control radar, facilitating accurate aircraft tracking during flight operations.

The control yoke flight control (aileron and elevator) interface is the primary mechanism for maneuvering the aircraft. The pedals rudder control mechanism manages yaw movement, pivotal for coordinated turns and directional stability. The trim wheel flight trim adjustment enables steady flight by reducing the need for constant control yoke input, to enhance pilot workload management. Additional features, including the clock provide timing functions for operational planning, while the parking brake secures the aircraft during ground operations. Circuit breakers protect electrical systems, and the suction gauge ensures proper vacuum pressure for gyroscopic instruments, maintaining reliable instrument readings.

What is the cabin design of a Cessna 152?

The cabin design of a Cessna 152 is a functional layout with a simplified configuration, emphasizing efficient spatial arrangement and user-friendly control placement. The cabin width measures 39 1/4 inches (99.7 cm), providing a compact yet functional space for training purposes. A side-by-side seating configuration accommodates two occupants, enabling communication and interaction during flight lessons. The instrument panel features a clear "six-pack" layout, optimizing accessibility and readability for pilots. Controls including throttle, mixture, and carburetor heat are positioned within easy reach, reducing pilot workload. Manually adjustable seats allow for customization to accommodate varying pilot heights, assuring comfort during operations.

What is the Cessna 152 spin recovery procedure?

The Cessna 152 spin recovery procedure is a sequential process involving precise pilot inputs to safely exit a spin. A spin occurs when the aircraft exceeds its vital angle of attack, around 16 to 18 degrees in the Cessna 152. The pilot immediately places the ailerons in a neutral position to prevent further roll input. Full rudder opposite to the direction of rotation counters the yawing motion caused by the spin. The control yoke moves briskly forward to reduce the angle of attack and break the stall, with full down elevator required at aft center of gravity loadings. Throttle adjustment to idle prevents engine power from complicating the recovery process.

The FAA-approved spin recovery procedure for the Cessna 152 begins with the pilot neutralizing the ailerons to prevent unintended roll inputs. Full rudder opposite to the direction of rotation counters the yawing motion, while brisk forward movement of the control yoke reduces the angle of attack and breaks the stall. The throttle must be set to idle during the spin recovery process to minimize complications from engine power. Pilots maintain these inputs until rotation ceases, then smoothly neutralize the rudder and recover from the dive by gently pulling back on the yoke. Altitude, airspeed, and aircraft configuration influence recovery effectiveness, with altitude being vital for completing the procedure safely. A minimum of 1,000 feet (304.8 meters) above ground level is required to execute the spin recovery procedure in accordance with instructions effectively.

Safety protocols emphasize maintaining neutral ailerons to avoid exacerbating the spin through aileron roll neutralization. Overcorrection with rudder or elevator inputs delays recovery and increases risk. Pilots monitor the angle of attack threshold, between 16 to 18 degrees in the Cessna 152, to detect stall lift loss early. Proper timing ensures that rudder yaw correction and elevator pitch down input align with the spin recovery procedure safety actions. Environmental factors like turbulence or wind affect spin dynamics, requiring adjustments to maintain control. Weather conditions demand heightened awareness during spin recovery procedure pilot inputs to assure consistent execution.

Does the Cessna 152 have an autopilot?

No, the Cessna does not have an autopilot in its standard configuration. The Cessna 152 lacks a factory-installed autopilot system in its standard configuration. Aftermarket autopilot options exist for retrofit installation in the Cessna 152. These systems reduce pilot workload during longer flights in the Cessna 152. The Trio Pro Pilot system is one such aftermarket autopilot option for the Cessna 152. Supplemental Type Certificates certify these systems for safety and performance compliance.

Autopilot systems in small aircraft like the Cessna 152 function by maintaining heading, altitude, and navigation tracking through incorporated servos and control inputs. These systems reduce pilot workload during flight operations, in scenarios requiring prolonged steady-state flying or precise navigation adjustments. The Trio Pro Pilot system offers altitude hold functionality, heading mode, and navigation tracking capabilities, providing stability and operational efficiency in the Cessna 152 autopilot system functionality.

The Cessna 152 cockpit design emphasizes simplicity and ease of operation for training purposes. The standard configuration includes basic flight instruments: an altimeter, airspeed indicator, heading indicator, and vertical speed indicator, all powered by a pitot-static system with heated or unheated pitot heads and static ports. The absence of factory-installed autopilot controls in the Cessna 152 panel highlights its focus on manual operation and pilot skill cultivation.

Aftermarket autopilot options exist for retrofit installation in the Cessna 152 systems. The Trio Pro Pilot system integrates into the Cessna 152 cockpit through a control head, servos, and a wiring harness, providing necessary switches and placards for seamless operation. Supplemental Type Certificates certify these systems for safety and performance compliance, assuring regulatory adherence in the Cessna 152 aftermarket compatibility process.

Installation of aftermarket autopilot systems requires careful integration with the Cessna 152's existing electrical and mechanical systems. The 28V, 60A alternator and 24V battery power distribution managed by the master switch and bus bar must align with the new system's demands. Modifications to the Cessna 152 panel and internal structures enable proper placement and functionality of components, addressing problems associated with retrofitting advanced automation into the Cessna 152's original design.

Where can I find a Cessna 152 for sale?

You will find a Cessna 152 for sale on platforms like Trade-a-Plane, Barnstormers, and AvBuyer Inventory. Trade-a-Plane updates its inventory daily, featuring up to 24 active listings for Cessna 152 aircraft. Barnstormers Online Classifieds includes detailed ads, for example, a 1978 Cessna 152 Aerobat II priced at $60,000. Controller.com provides market-leading data, listing prices for Cessna 152 models ranging from $44,219 to $115,000. GlobalAir connects buyers directly with sellers, offering access to global inventories. Local aviation dealerships allow in-person inspections of available Cessna 152 models.

AvBuyer listings and Controller Classifieds provide important resources for evaluating Cessna 152 models. AvBuyer inventory includes a range of aircraft, featuring the Cessna 152 among its options. Controller Classifieds highlights market-leading data with prices for the Cessna 152 ranging from $44,219 to $115,000. Trade-a-Plane Inventory updates daily, offering up to 24 active listings for the Cessna 152 at any given time. Trade-a-Plane Sale Data aggregates information from private sellers, offering a diverse selection of aircraft. Barnstormers Aircraft Listings and Barnstormers Online Classifieds feature detailed ads, including a 1978 Cessna 152 Aerobat II priced at $60,000. GlobalAir Global Inventory and GlobalAir Seller Contacts connect buyers directly with sellers, providing access to global inventories of the Cessna 152.

Local Aviation Dealerships Local Inventory allows buyers to inspect Cessna 152 models in person. Local Aviation Dealerships Dealer Network expands access to a broader selection of aircraft through affiliated dealers. Physical locations of Local Aviation Dealerships Physical Location enable thorough evaluations of the Cessna 152’s condition. Buyers assess factors like total time on the airframe (TTAF) and engine hours since overhaul when purchasing the Cessna 152. The Cessna 152 is widely recognized for its reliability and training capabilities, making it a popular single-engine aircraft. Prices and availability trends reflect current market conditions across platforms like Controller.com and Trade-a-Plane Listings.

What is the price of a Cessna 152?

The price of a Cessna 152 varies based on the aircraft's condition, location, and additional features or upgrades. A 1981 model in the Czech Republic was priced at $78,000. A 1980 model in England, known as the Cessna 152 Av30, was listed at $58,750. Recent listings show prices for fully functional models of Cessna 152s varying from $50,000 to $70,000. Top-of-the-line, well-maintained Cessna 152s fetch prices up to $115,000. Some sources indicate an average price of around $92,943 based on web listings over the last 12 months.

Prices for Cessna 152s in good condition reflect a broad spectrum. A 2010 model averaged $22,500, while market data indicates a low-end price of $44,219. Mid-range prices include a 1980 model in England listed at $58,750 and a 1981 model in the Czech Republic priced at $78,000. High-end models, well-maintained or upgraded, reach up to $115,000. Recent web listings show an average price of $92,943 over the last 12 months, though outliers as $129,000 appear on platforms like GlobalAir.com. Factors influencing price variations include the aircraft's condition, geographic location, and additional features or upgrades. Ownership costs extend beyond the purchase price. Engine overhauls for a Cessna 152 cost up to $20,000, while annual operational expenses approximate $1,100. These figures highlight the financial commitment required for maintaining and operating a Cessna 152.