Piper Dakota: Definition, Specs, Performance, Difference, Interior

Piper Dakota is a single-engine, four-seat aircraft designed for general aviation purposes. The specifications of Piper Dakota include its engine type, performance capabilities, and physical dimensions. The interior of Piper Dakota provides comfort and functionality for pilots and passengers. Piper Dakota achieves superior performance through efficient design and engineering. The takeoff characteristics and range of Piper Dakota define its operational versatility. Learn about Piper Dakota's specifications, interior, engine, performance, takeoff, and range.

Piper Dakota integrates the Lycoming O-540-J3A5D engine rated at 235 horsepower. The aircraft measures 24 feet 7 inches (7.49 meters) in length, spans 35 feet 4 inches (10.77 meters) in wingspan, and reaches a height of 7 feet 2 inches (2.18 meters). Maximum takeoff weight is 3,000 pounds (1,360 kilograms) with an empty weight of 1,610 pounds (730 kilograms). Fuel capacity reaches 72 gallons (272.8 liters), allowing for a range of up to 740 nautical miles (1370.4 kilometers). Cruise speed averages 144 knots, while maximum speed reaches 148 knots. These specifications highlight the aircraft's efficiency and practicality for diverse missions.

Utility load capacity of Piper Dakota reaches 1,400 pounds (635 kilograms), encompassing passengers, cargo, and fuel. Gross weight supports 3,000 pounds (1,360 kilograms), while empty weight measures around 1,600 pounds (725 kilograms). Fuel tanks hold 72 to 77 gallons (272.5 to 291.5 liters), providing a range of 650 to 740 nautical miles (1203.8 to 1370.6 kilometers) with reserves. Internal baggage volume accommodates up to 26 cubic feet, balancing utility and endurance effectively. Theoretical payload with full fuel decreases to 960 pounds (435.45 kilograms), emphasizing the tradeoff between range and carrying capacity. Operators optimize load distribution based on mission priorities.

The difference between Piper Dakota and Cherokee lies in Dakota's extra engine power, achieved through the 235-horsepower Lycoming O-540-J3A5D engine. Dakota adopts a semi-tapered wing design, enhancing aerodynamic efficiency and reducing drag. This design enhances climb rate and payload capacity. Dakota achieves a top speed of 170 mph (273.584 km/h) and cruises at 166 mph (267.148 km/h), surpassing Cherokee 235's top speed of 160 mph (257.494 km/h). Takeoff distance over a 15-meter (50-foot) obstacle requires 396 meters (1,300 feet), and fuel capacity holds 292 liters (77 gallons), with 276 liters (73 gallons) usable. Dakota offers superior performance metrics compared to earlier Cherokee models.

The interior of Piper Dakota reflects functional upgrades over Piper Cherokee, featuring a stretched fuselage that enhances cabin comfort. Cabin dimensions measure 42 inches (106.68 cm) wide, 49 inches (124.46 cm) high, and accommodate one crew member and up to four passengers. Seating includes two front seats for pilot and co-pilot and a rear bench for three passengers. Dark red fabric upholstery contributes to a modest yet warm ambiance. Baggage capacity accommodates up to 200 pounds (90.72 kilograms), stored in an aft compartment. Climate control ensures consistent airflow and heating, while cockpit instrument panels feature clear labeling for effective operation.

Piper Dakota serves general aviation flights, including private and recreational flying. Low wing design and benign handling characteristics make it suitable for flight training and air taxi operations. Speed capability reaches 144 knots at 75% power for efficient travel. Climb rate achieves 1,110 feet (338.33 meters) per minute, and fuel consumption averages 11.8 gallons (44.67 liters) per hour at 65% power. Operational capability allows use on 1,000-foot strips, making it ideal for regional connectivity in areas with limited infrastructure. Utility operations include surveillance or specialized missions in remote regions, leveraging robust short-field performance.

What is the Piper Dakota plane?

The Piper Dakota plane is a four-seat, fixed-gear aircraft with a Lycoming engine, known for reliability and stability. The flight center fleet includes the Dakota due to its economical operation and robust design, making it suitable for training and leisure flying.

The Piper Dakota belongs to the Piper Cherokee family of aircraft, a lineage known for robust design and economical operation. The Piper Dakota features a longer fuselage compared to other Cherokee models, improving its capacity and comfort. A 235 hp Lycoming O-540 engine powers the Piper Dakota, providing more power than other fixed-gear variants in the Piper Cherokee series. The Piper Dakota achieves higher cruise speeds and offers greater hauling capacity, making it suitable for personal and business transportation.The aircraft incorporates an unpressurized cabin with good visibility and comfort. The Piper Dakota maintains solid airframe construction with stable handling, making it ideal for training and leisure flying. The aircraft carries full loads of passengers and baggage on longer flights, demonstrating its versatility across various general aviation missions. Fixed tricycle landing gear ensures stability during takeoff and landing while maintaining simple and efficient operations. Later models of the Piper Dakota offer a glass cockpit option with modern avionics.

The Piper Dakota has a maximum takeoff weight of 2,750 lb (1,247 kg) and achieves a cruise speed of around 140 knots (259 km/h). The fuel capacity of the Piper Dakota reaches about 50 gallons (189 liters), enabling a range of roughly 800 nautical miles (1482 kilometers). These specifications highlight the Piper Dakota's efficiency and practicality within the four-seat, fixed-gear single-engine market segment. The Piper Dakota competes directly with the Cessna Skylane, offering pilots a combination of reliability, performance, and cost-effectiveness.

What are the specifications of the Piper Dakota?

The specifications of the Piper Dakota include a length of 24 feet 7 inches (7.49 meters), wingspan of 35 feet 4 inches (10.77 meters), and maximum takeoff weight of 3,000 lbs (1,360.78 kilograms). The cabin measures 42 inches (106.68 cm) wide and 49 inches (124.46 cm) high, accommodating comfortable seating for 1 pilot and 4 passengers.

The specifications of the Piper Dakota are given in the table below.

The Piper Dakota model PA-28-236 integrates a Lycoming O-540-J3A5D engine with 235 horsepower, achieving a maximum speed of 148 knots and a cruise speed of 144 knots. The climb rate reaches 1,110 feet (338.33 meters) per minute, and the service ceiling extends to 17,500 feet (5,334 meters). Aviation gasoline fuels the engine, which holds a capacity of 72 gallons (272.8 liters). Fuel consumption averages 12-15 gallons (45.4-56.8 liters) per hour under typical cruise conditions. The empty weight measures 1,610 pounds (730 kilograms), and the gross weight supports a maximum takeoff weight of 3,000 pounds (1,360 kilograms). The useful payload equals around 1,401 pounds (635 kilograms), accommodating four adults plus full fuel.

The Piper Dakota achieves a maximum range of 740 nautical miles with endurance enabling several hours of flight. Takeoff distance requires 886 feet (270 meters), while landing distance needs about 825 feet (251 meters). The aircraft operates effectively on short to medium-length runways, making it suitable for small airfields. The wingspan spans 35 feet 4 inches (10.77 meters), the length measures 24 feet 7 inches (7.49 meters), and the height reaches 7 feet 2 inches (2.18 meters).

The interior features seating for one crew member and up to four passengers, with a cabin layout providing 42 inches (106.68 cm) in width and 49 inches (124.46 cm) in height. Comfort features include reasonable rear seat space and a luggage area within the cabin. Avionics specifications include VOR and GPS navigation systems, a VHF communication radio, and basic flight instruments as standard equipment. Modern upgrades integrate glass cockpit displays into the system.

What is the utility load capacity of the Piper Dakota?

The utility load capacity of the Piper Dakota is 1,400 lbs (635 kg), encompassing passengers, cargo, and fuel. The Piper Dakota features a gross weight of 3,000 lbs (1,360 kg) and an empty weight around 1,600 lbs (725 kg) defining the operational envelope, enabling the aircraft to carry loads while maintaining stability and performance. The aircraft offers a fuel capacity of 72-77 gallons (272.8-291.5 liters), providing a range of 650-740 nm (1203.8-1370.6 kilometers) with reserves. Internal baggage volume reaches up to 26 cubic feet, accommodating both passengers and cargo efficiently. Equipped with a Lycoming O-540-J3A5D engine rated at 235 horsepower, the aircraft achieves robust performance for its class. The theoretical payload with full fuel is 960 lbs (435.45 kg), balancing utility and endurance effectively.

The Piper Dakota exhibits a standard useful load of 1,401 lbs (635.5 kg), a comparably equipped load of 1,236 lbs (560.6 kg) when matched against the Cessna Skylane, and an average useful load of 1,403 lbs (636.4 kg). This range highlights the aircraft's ability to accommodate diverse mission requirements within its weight limits. The useful load encompasses the combined weight of passengers, cargo, and fuel, to ensure efficient operations under varying conditions.

The utility of the Piper Dakota extends to its capacity for balancing payload and endurance effectively. With full fuel tanks holding 72-77 gallons (272.8-291.5 liters), the theoretical payload decreases to 960 lbs (435.4 kg), emphasizing the tradeoff between range and carrying capacity. Operators can optimize load distribution based on mission priorities, whether prioritizing passenger count, cargo volume, or extended flight durations. The internal baggage space of 26 cubic feet further enhances versatility, allowing pilots to configure loads for both comfort and functionality.

What is the Dakota's maximum takeoff weight?

The Dakota's maximum takeoff weight is 31,000 pounds (14,061 kilograms). The Douglas C-47, known as the Dakota, has a maximum takeoff weight of 26,000 pounds (11,793 kilograms) for gross weight. The maximum takeoff weight ensures safe operation based on the aircraft's capacity to carry payloads while maintaining structural integrity.

The Dakota's standard maximum takeoff weight equals 31,000 pounds (14,061 kilograms), assuring safe flight operations under normal conditions. Structural and performance considerations dictate this limit to maintain balance between payload capacity and airframe integrity. Overload modifications extend the maximum takeoff weight to 33,000 pounds (14,968.5 kilograms), allowing increased cargo or fuel loads for specialized missions. Rocket-assisted short takeoffs enable the Dakota to achieve a maximum takeoff weight of 35,000 pounds (15,876 kilograms), improving operational flexibility in challenging environments. High-altitude airfields reduce the effective takeoff weight to 26,000 pounds (11,793 kilograms), reflecting adjustments necessary for reduced air density and engine performance.

Rocket-assisted takeoffs extend the Dakota's payload capacity by compensating for runway lengths shorter than 2,000 feet (610 meters) or adverse terrain conditions. This capability proves in remote or austere locations where traditional takeoff methods fall short. The Dakota achieves its highest maximum takeoff weight of 35,000 pounds (15,876 kilograms) during these operations, demonstrating adaptability to diverse mission requirements. Tropical climate operations further modify the maximum takeoff weight to 28,500 pounds (12,927 kilograms), accounting for heat and humidity effects on engine efficiency.

A comparison of standard and assisted takeoff weights highlights the Dakota's versatility across varying operational contexts. The standard configuration supports a maximum takeoff weight of 31,000 pounds (14,061 kilograms), while specific conditions allow deviations within defined limits. Structural reinforcements and engine performance optimizations support compatibility with higher weights during overload or rocket-assisted scenarios. Each configuration reflects precise engineering adapted to mission demands and environmental factors.

What is the Dakota's best climb rate at sea level?

The Dakota's best climb rate at sea level is 1,000 ft/min (304.8 m/min). The Piper PA-28-236 Dakota achieves a maximum climb rate of 1,110 ft/min (338.3 m/min) at sea level. The Douglas C-47 Dakota reaches a rate of climb of 1,041 ft/min (317.3 m/min) under similar conditions. The best angle of climb speed for the Piper PA-28-236 measures 73 knots, optimizing altitude gain over distance and enabling pilots to maximize altitude gain over horizontal distance during critical phases of flight. Optimal climb performance depends on excess power to overcome drag and increase altitude efficiently. Climb rates for average single-engine aircraft remain lower at around 500 ft/min (152.4 m/min).

The Dakota's maximum climb rate at sea level reflects its performance, with a benchmark of 1,000 ft/min (304.8 m/min) achievable under optimal conditions. The Piper PA-28-236 Dakota surpasses this figure, achieving a climb rate of 1,110 ft/min (338.328 m/min) due to its efficient single-engine design and lightweight structure. In contrast, the Douglas C-47 Dakota, a twin-engine military variant of the DC-3, achieves a climb rate of 1,041 ft/min (317.3 m/min) at sea level. The difference in climb performance stems from variations in engine power, aerodynamic design, and gross weight between the two models. Excess power is significant in climb efficiency, as it directly impacts the aircraft's ability to overcome drag and gain altitude. Average single-engine aircraft achieve climb rates of 500 ft/min (152.4 m/min), underscoring the superior performance of both Dakota variants.

Using takeoff flaps ameliorates climb performance by reducing drag, adding an additional 110 ft/min (33.53 m/min) to the climb rate. Twin-engine aircraft like the Douglas C-47 Dakota prioritize operational versatility, optimizing climb rates for endurance missions rather than rapid ascent. Stall speeds of 60 knots with full flaps and 75 knots without flaps further define the Dakota's performance envelope. Climb rates exceeding 67,250 ft/min (20,500 m/min) remain unrealistic for conventional aircraft, emphasizing the practical limits of current aviation technology.

What is the fuel burn rate of a Piper Dakota?

The fuel burn rate of a Piper Dakota is 13.5 (51 liters) to 14 (53 liters) gallons per hour during cruise conditions. Fuel efficiency depends on engine condition, altitude, and weather. Pilots manage fuel consumption based on power settings, achieving rates as low as 9 gph at 55% power.

Fuel burn rates range from 14 gph block to block during taxiing and ground operations to 12-13 gph running on auto fuel or avgas in flight. Lean of peak operation with GAMI injectors reduces fuel consumption to 10.5 gph by optimizing fuel distribution. Pilots achieve further efficiency by adjusting power settings, with fuel burn at 12.0 gph at 75% power and 8.8 gph at 65% power, 2350 rpm for economy cruise. A similar configuration at 75% power and 2450 rpm results in a burn rate of 10 gph. At 55% power, the Piper Dakota burns 9 gph, balancing speed and efficiency for longer flights. Real-world scenarios prioritize fuel efficiency by reducing power settings and utilizing lean of peak operations. These methods extend endurance, allowing pilots to maximize the aircraft's 72-gallon usable fuel capacity for extended cross-country flights.

Fuel burn rates differ under various conditions: avgas versus auto fuel or peak versus lean operations. The Piper Dakota achieves higher performance capabilities with increased fuel consumption compared to smaller piston singles. Operating costs reflect this balance, as the Lycoming O-540 engine provides robust performance with cruise speeds around 139 knots. The aircraft’s fuel efficiency supports practical missions requiring both payload capacity and range.

What is the difference between the Piper Dakota and Cherokee?

The difference between the Piper Dakota and Cherokee is due to the Dakota's extra engine power with a 235 horsepower Lycoming O-540-J3A5D engine. Both aircraft share a two-seat pilot configuration and a wingspan of 30 feet (9.14 meters). The Dakota's semi-tapered wing design improves efficiency.

The difference between the Piper Dakota and Cherokee is explained in the table below.

The Dakota achieves a top speed of 170 mph (273.584 km/h) and cruises at 166 mph (267.136 km/h), surpassing the Cherokee’s top speed of 160 mph (257.496 km/h) and cruising range of 140-150 mph (225.312-241.4 km/h). The Dakota requires 1,300 feet (396.24 meters) for takeoff over a 50-foot (15.24 meters) obstacle and offers a range of about 800 miles (1287.48 kilometers), holding 77 gallons (291.48 liters) of fuel with 73 usable gallons (276.33 liters). The Cherokee 235 holds 84 gallons (318 liters) of fuel but delivers shorter range due to less aerodynamic efficiency. The Dakota’s semi-tapered wing design reduces drag, upgrading climb rate and payload capacity. With a gross weight of 3,000 lbs (1,360 kg) and an empty weight of 1,633 lbs (741 kg), the Dakota provides a useful load superior to earlier Cherokee models.

The Piper Dakota interior reflects late 1970s styling trends while incorporating functional upgrades over the Piper Cherokee. The Dakota stretches the fuselage to enhance cabin comfort, providing more legroom compared to earlier Cherokee models. Additional windows enhance visibility, complementing the wider stance of the aircraft. The Cherokee interior focuses on comfort and versatility for flight training and personal use, but the Dakota introduces modernized features, like updated avionics and refined seating arrangements. Both aircraft cater to utility and personal missions, yet the Dakota’s modifications create a more spacious and visually appealing cabin atmosphere.

Piper Aircraft engineering showcases the evolution from the PA-28 series to the Dakota, refining designs for efficiency and capability. The Piper Cherokee debuts in 1960 as a four-place, fixed-gear single-engine aircraft with a 160 HP engine, later advancing to the 235 HP Lycoming engine in the Cherokee 235. The Dakota builds upon this lineage, adopting the semi-tapered wing from the Warrior model and incorporating a more efficient 235 HP Lycoming O-540-J3A5D engine. The Dakota modifies the fuel system to hold 77 gallons (291.4 liters) with 73 usable gallons (276.3 liters), optimizing fuel efficiency and reducing noise and vibration. Piper Aircraft positions the Dakota as the top-of-the-line Cherokee variant introduced in the late 1970s, marking a culmination of decades of innovation within the PA-28 series.

What is the interior of the Piper Dakota cabin like?

The interior of the Piper Dakota cabin measures 3 ft 6 in (1.07 m) height, 3 ft 6 in (1.07 m) width, and 8 ft 2 in (2.49 m) length, accommodating one crew member and up to four passengers. The Piper Dakota cabin features a width of 42 inches (106.68 cm), providing more space than the Piper Cherokee 180's 40 inches (101.6 cm). Owners appreciate the roomy interior that balances passenger space with payload capacity. The seating arrangement includes two front seats for the pilot and co-pilot and a rear bench accommodating three passengers.

The Piper Dakota cabin comfort relies on its seating arrangement ergonomics, featuring four fully adjustable seats that provide ample legroom and support for all occupants. The front seats accommodate the pilot and co-pilot, while the rear bench offers seating for three passengers, assuring a balanced distribution of space. The seating arrangement configuration maximizes usability within the compact dimensions of 3 ft 6 in (1.07 m) height, 3 ft 6 in (1.07 m) width, and 8 ft 2 in (2.49 m) length. Owners value the ergonomic layout user-friendly design, which allows for easy access to controls and enhances overall functionality.

Interior design aesthetics in the Piper Dakota emphasize durability and practicality over luxury. Dark red fabric upholstery enhances the modest yet warm ambiance of the cabin, creating an inviting atmosphere for travelers. Cabin materials quality prioritizes longevity, with smooth finishes for a pleasant flying experience. Optional upgrades include refinishing seat frames and reupholstering seats, allowing customization to modern preferences.

Storage compartments functionality in the Piper Dakota includes accessible spaces. The baggage capacity accommodates 200 lbs (90.72 kg), stored in an aft compartment designed for convenience during short trips. Climate control system efficiency ensures consistent airflow and heating throughout the cabin, maintaining comfort during various weather conditions. The cockpit instrument panel readability benefits from clear labeling and intuitive placement. Ergonomic layout space optimization makes the most of the available cabin dimensions without compromising passenger comfort or usability.

Is the Dakota equipped with modern avionics?

Yes, the Dakota is equipped with modern avionics, including advanced glass cockpit systems like the Garmin G1000. Upgraded systems enable the Dakota to achieve full IFR operational capability. Digital displays replace traditional analog instruments in the Dakota’s modernized cockpit. Real-time weather updates and digital autopilot capabilities boost navigation accuracy.

The Garmin G1000 system in the Piper Dakota includes navigation, communication, and integration technologies, providing pilots with advanced GPS for accurate route execution, real-time weather updates, and autopilot functionality. Specific models of the Dakota, retrofitted variants, incorporate these upgrades to align with contemporary aviation standards.

The practical implications of the Dakota's modern avionics encompass upgraded operational safety and full IFR capability. Modern avionics advanced navigation systems like the Garmin GTN 750 upgrade route planning accuracy. Piper Dakota communication systems integrate King KX 165 NAV/COM radios and the Garmin GTX 335 transponder for precise location tracking and reliable exchanges with air traffic control. Glass cockpit digital displays replace outdated analog gauges, offering high-resolution screens that enhance situational awareness.

Avionics suite system integration ensures all components work harmoniously, reducing technical risks. Glass cockpit elevates situational awareness and allows pilots to maintain a clear understanding of their surroundings. The Century 21 autopilot system stabilizes flight trajectories and reduces pilot workload. Real-time flight data provided by the glass cockpit supports safe and efficient operations. Pilots benefit from customizable avionics packages adapted for specific needs, whether for private or commercial purposes. The Dakota panel design prioritizes user-friendliness for easy access to necessary controls. Upgraded Dakotas achieve economical operation while meeting current aviation standards. The robust airframe retains its historical versatility with technological evolution.

Is the Piper Dakota certified for IFR operations?

Yes, the Piper Dakota is certified for IFR operations if it meets avionics and equipment requirements. The aircraft requires specific avionics, including a certified altimeter, transponder, and navigation systems like VOR or GPS. Regular inspections guarantee compliance with FAA regulations for IFR operations. Garmin GPS/nav/com systems and autopilot systems are installed to meet certification standards. The Dakota's heavier engine and propeller combination demands additional pilot training for safe IFR flight. Pilots must hold an instrument rating and complete at least 15 hours of instrument flight training.

FAA certification guidelines govern the Piper Dakota certification status. The aircraft must meet specific avionics and equipment requirements to achieve IFR operations instrument flight rules compliance. Aircraft certification approval criteria include rigorous testing of the Piper Dakota avionics suite to guarantee all instruments function correctly. The altimeter, transponder, and navigation systems like VOR or GPS undergo calibration to provide precise readings. Piper Aircraft adheres to manufacturer standards aligned with FAA regulatory authority, assuring the Dakota meets airworthiness criteria. Certification testing procedures involve ground evaluations and in-flight assessments to validate performance metrics.

IFR operations operational requirements mandate that pilots hold an instrument rating and complete at least 15 hours of instrument flight training. The Piper Dakota flight characteristics demand additional training due to its heavier engine and propeller configuration. High-performance endorsement is required for pilots operating the Dakota under IFR conditions. Compliance with FAR 91 and FAR 135 ensures the aircraft's avionics and instrumentation meet IFR standards. Regular inspections maintain the Dakota's airworthiness and ascertain ongoing adherence to FAA regulations.

The heading indicator, turn coordinator, vertical speed indicator, and attitude indicator comprise the avionics suite. Communication equipment like VHF radios enables interaction with air traffic control. Piper Aircraft ensures compliance with manufacturer specifications for avionics installation, maintaining the Dakota's reliability for both VFR and IFR operations.

The aircraft's engine and propeller configuration impacts maintenance demands, requiring thorough checks during annual and IFR certification inspections. Avionics compliance ensures the Dakota meets IFR requirements, while regular updates address potential problems like aging components. The POH provides detailed guidance on maintaining the aircraft's systems for safe operation under diverse conditions. Piper aircraft certification history reflects a commitment to meeting or exceeding industry benchmarks for safety and performance.

Does the Dakota have a nose wheel steering system?

Yes, the Dakota has a nose wheel steering system. The Piper PA-28 Dakota incorporates a nose wheel steering system as part of its tricycle landing gear configuration. The system connects the rudder pedals to the nose wheel via a mechanical linkage, including components like a steering horn and torque links. Pilots achieve precise directional control during taxiing, takeoff, and landing operations. The nose wheel steering travel extends 30 degrees on either side of the centerline. Maintenance of components including the damper and steering rod brackets ensures safe and reliable ground handling.

The nose wheel steering system steering mechanism connects directly to the rudder pedals, facilitating directional control during taxiing, takeoff, and landing. Pilots rely on this mechanical linkage to achieve precise ground handling, a hallmark of Piper aircraft manufacturer specification. The system allows 30 degrees of steering travel on either side of the centerline, promoting the aircraft's ability to navigate tight spaces and maintain alignment in crosswind conditions. The Dakota aircraft achieves optimal maneuverability through its robust integration of torque links and steering arms. These elements contribute to seamless aircraft steering mechanism operational integration for safe and efficient ground handling.

Maintenance of the nose wheel steering system control assembly is performed for sustaining airworthiness and reliability. Components like the damper and steering rod brackets require regular inspection and potential replacement to prevent issues: shimmy or failure. Upgrades or modifications to these parts align with Piper aircraft design standard for prolonged system longevity and consistent performance. The landing gear wheel assembly benefits from adherence to rigorous maintenance protocols, preserving the integrity of the landing gear steering configuration.

Does the Piper Dakota have a spin-resistant design?

Yes, the Piper Dakota has a spin-resistant design that enhances stability but complicates spin recovery in certain situations. The Piper Dakota incorporates a semi-tapered wing design from the Piper Warrior model, improving its spin-resistant characteristics. Spin-resistant design elements include wing washout and a balanced tail section to optimize airflow and reduce spin likelihood. Federal Aviation Administration certification ensures the aircraft meets stringent safety standards for stall and spin recovery. Aerodynamic design focuses on stability, with deliberate engineering to prevent unintended spins during flight. Piper Aircraft's testing validates the Dakota's predictable stall behavior and straightforward recovery procedures.

What is the Piper Dakota typically used for?

The Piper Dakota is used for general aviation flights, including private and recreational flying, due to its low wing design and benign handling characteristics. The Piper Dakota serves as a single-engine piston aircraft with fixed landing gear, designed for personal and utility use, for example flight training and air taxi operations. The aircraft achieves speeds of up to 144 knots at 75% power, making it suitable for efficient travel. The Piper Dakota's 235 hp Lycoming engine enhances lifting power, making it ideal for family travel and utility. A climb rate of 1,110 feet (338.3 meters) per minute ensures robust performance in various conditions. The aircraft burns about 11.8 gallons (44.7 liters) per hour at 65% power, offering a balance between performance and economy.

The Piper Dakota commuter transport serves regional passenger service operations, for short-haul flights. The aircraft's ability to operate from 1,000-foot strips makes it suitable for regional connectivity in areas with limited infrastructure. Air taxi services on-demand flights leverage the Piper Dakota's reliability and versatility, providing efficient transport for private groups or individuals. The aircraft achieves speeds of up to 144 knots at 75% power, assuring timely travel for corporate aviation business travel or executive transport within smaller markets. The Piper Dakota's payload capacity supports light cargo transport, demonstrating its utility in niche applications.

The Piper Dakota general aviation flights include private flight and recreational aviation activities. A climb rate of 1,110 feet (338.3 meters) per minute and fuel consumption of 11.8 gallons (44.7 liters) per hour at 65% power establish a balance between performance and economy. Specific configurations of the Piper Dakota cater to surveillance or specialized missions in remote regions. Geographic factors, like high-density altitudes, influence its deployment in mountainous or hot climates, necessitating robust short-field performance.

Operational costs of the Piper Dakota reflect its efficiency, with a 235 hp Lycoming engine reducing maintenance expenses compared to higher-performance engines. Market demand favors the aircraft for roles requiring moderate range and payload without excessive operating costs. Regulatory frameworks emphasize its use in general aviation recreational aviation due to its benign handling characteristics and stall speed of 56 knots with flaps deployed. The Piper Dakota maintains relevance in commuter air transport regional connectivity by addressing gaps left by larger aircraft unsuited for small-scale operations.

How does the Dakota handle in crosswind conditions?

The Dakota handles crosswind conditions effectively due to its robust design and demonstrated crosswind capability of 15-16 knots. The Dakota's dihedral angle of the wings enhances roll stability, providing level flight in crosswind conditions. A maximum demonstrated crosswind limit of 17 KIAS reflects its ability to handle strong winds during takeoff and landing. The longer wingspan improves lift efficiency and roll response, contributing to precise control in challenging winds. Rudder effectiveness supports directional control, while the new aileron design reduces effort for lateral adjustments. Moderate wing loading ensures stability without compromising maneuverability in gusty conditions.

The Piper Dakota, specifically the PA-28-236 variant, demonstrates superior handling during takeoff, landing, and taxiing. During takeoff, the aircraft's moderate wing loading ensures stability while the dihedral angle of the wings enhances roll stability. Pilots maintain directional control through effective rudder inputs, aided by the Dakota's yaw stability. Crosswind landings require precise technique, including lowering the upwind wing and aligning the aircraft with the runway centerline using aileron and rudder adjustments.In-flight stability remains consistent due to the longer wingspan and efficient lift generation, which minimizes drag and enhances aerodynamic performance lift efficiency.

Aircraft handling in crosswind conditions depends on metrics like roll rate, yaw stability, and control surface responsiveness. The Dakota's new aileron design reduces effort for lateral adjustments, enhancing crosswind performance and lateral control. Rudder effectiveness ensures directional stability, during taxiing where crosswinds exert side forces. Pilots experience reduced workload due to the aircraft's balanced wing design dihedral angle and moderate wing loading. Gusts and varying wind angles challenge stability, but the Dakota maintains level flight through its robust roll stability and flight characteristics. Aerodynamic performance drag reduction contributes to efficient handling even in gusty environments.

Crosswind conditions vary in intensity, with wind speeds ranging from 15 to 17 knots and gusts adding complexity. Pilots must respect these thresholds for safe operations. The Dakota's handling characteristics maneuverability allows quick adjustments during unexpected gusts or shifts in wind direction. Control surfaces aileron responsiveness and rudder effectiveness enable smooth corrections throughout the landing roll. Heavier aircraft like the Dakota exhibit less susceptibility to gust effects compared to lighter models. The combination of a 235 HP engine and optimized wing design enhances overall handling characteristics and responsiveness, making the Dakota reliable in challenging wind scenarios.

What are the common problems with the Piper Dakota?

The Piper Dakota has common problems with the following details.

• Landing gear: The oleo struts wear out quickly, causing a rough ride even on smooth surfaces, and rough runway operations can lead to frequent damage.
• Fuel system: Fuel gauges in low-wing models provide inaccurate readings during flight, and aging components can cause leakage or blockage, increasing fuel burn rates to 55 liters (14.5 gallons) per hour.
• Seating discomfort: The seating position is fairly low with seat backs pitched too far back, causing discomfort for pilots and passengers.
• Engine control concerns: The carbureted Continental TSIO-360-FB engine experiences carburetor icing and reliability issues due to the fixed-wastegate controller, potentially causing detonation problems. The Piper Dakota is prone to engine wear causing engine failure without proper maintenance.
• Structural fatigue: Airframe cracks, in low-wing models, particularly in wing spars, require regular inspections and airworthiness directives to guarantee integrity and prevent worsening damage from hard landings or inadequate maintenance.
• Corrosion risks: Moisture-prone areas, for example the pitot/static system, are susceptible to corrosion, necessitating protective measures and frequent checks.
• Hydraulic system failures: Neglected hydraulic systems can lead to malfunctions, though specific issues remain undocumented, contributing to temporary groundings.
• Electrical system faults: Aging wiring causes short circuits, leading to avionics malfunctions or failures that demand robust maintenance protocols.
• Avionics malfunctions: Electrical system issues contribute to recurring avionics failures, requiring regular checks to prevent operational disruptions.
• Maintenance challenges: Preventing recurring issues like airframe corrosion, engine wear, landing gear damage, monitoring fuel levels, inspecting hydraulic systems, and addressing structural fatigue, demands diligent inspection schedules and adherence to airworthiness directives.

Where to find a Piper Dakota for sale?

To find a Piper Dakota for sale, search listings on platforms like Controller.com and Trade-A-Plane, where sellers offer various models at prices ranging from $107,900 to over $275,000 depending on condition, year, and specifications. Controller.com and Trade-A-Plane feature advanced search filters to refine results by price, location, and aircraft specifications. Buyers find listings with detailed descriptions, including a 1980 Piper Dakota priced at $154,950 and a 1985 model advertised for its updated interior. Sellers provide direct contact information for inquiries and inspections. Aviation brokers assist in connecting buyers with trusted sellers through platforms like Aircraft Brokers International. Auction sites occasionally list Piper Dakota models for competitive bidding.

Aircraft dealerships inventory includes Piper Dakota models for sale across the United States. Dealership locations vary, with notable presence in states like Florida and Texas. Aircraft dealerships contact-information is accessible through platforms like Controller.com and Trade-A-Plane. Online aircraft marketplaces listings provide extensive options for buyers seeking a Piper Dakota model. Aircraft marketplaces location spans international markets, offering global access to Piper Dakota specifications and pricing. Aviation brokers network connects buyers with trusted sellers specializing in the Piper Dakota. Aviation brokers contact-information is available through firms like Aircraft Brokers International. Aircraft auction sites auctions occasionally feature Piper Dakota models for competitive bidding. Aircraft auction sites listings include rare or vintage Piper Dakota aircraft with detailed seller advertisements. Online used aircraft listings pricing ranges from $107,900 to over $275,000, reflecting variations in condition and specifications. Online used aircraft listings seller details provide direct communication with owners or brokers. Classifieds for aircraft sales advertisements highlight key features of Piper Dakota aircraft, including engine performance and interior updates. Classifieds for aircraft sales contact-details facilitate inquiries and inspections.