The Complete Guide to the PIPER PA32-260 Cherokee Six Specs

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The Complete Guide to the PIPER PA32-260 Cherokee Six Specs


PIPER PA32-260 Cherokee Six Specs refer to the specifications and technical details of the Piper PA32-260 Cherokee Six aircraft, a popular six-seat, single-engine airplane manufactured by Piper Aircraft.

Understanding the specifications of the PA32-260 Cherokee Six is crucial for pilots, aircraft engineers, and aviation enthusiasts to operate, maintain, and appreciate the aircraft’s capabilities and limitations. These specs encompass various aspects, including dimensions, performance, engine characteristics, fuel capacity, and avionics systems.


Main article topics that delve deeper into the PIPER PA32-260 Cherokee Six Specs may include:

  • Dimensions and Weight
  • Performance Characteristics
  • Engine Specifications
  • Fuel System and Capacity
  • Avionics and Instrumentation
  • Historical Development and Variants
  • Safety Features and Maintenance
  • Operational Procedures and Limitations

PIPER PA32-260 Cherokee Six Specs

The PIPER PA32-260 Cherokee Six is a popular six-seat, single-engine aircraft renowned for its versatility, performance, and safety. Understanding its specifications is essential for pilots and aviation enthusiasts. Here are seven key aspects that define the PA32-260 Cherokee Six:

  • Dimensions: 28 ft 4 in length, 35 ft wingspan
  • Weight: 2,650 lbs empty, 4,400 lbs max takeoff
  • Performance: 143 mph cruise speed, 750 nm range
  • Engine: Lycoming IO-540-K1G5D, 260 hp
  • Fuel: 80 gallons usable capacity
  • Avionics: Garmin G1000 NXi avionics suite
  • Safety: Garmin GFC 700 autopilot, angle of attack indicator

These specifications highlight the aircraft’s compact size, impressive performance, reliable engine, generous fuel capacity, advanced avionics, and robust safety features. The PA32-260 Cherokee Six is a versatile aircraft suitable for various missions, including private flying, flight training, and air taxi operations. Its combination of comfort, efficiency, and safety makes it a popular choice among pilots worldwide.

Dimensions

The dimensions of an aircraft, including its length and wingspan, are crucial specifications that define its physical size and aerodynamic characteristics. In the context of the PIPER PA32-260 Cherokee Six, these dimensions play a significant role in determining the aircraft’s handling, performance, and overall capabilities.

  • Maneuverability: The relatively compact size of the PA32-260 Cherokee Six, with a length of 28 ft 4 in and a wingspan of 35 ft, contributes to its excellent maneuverability. This makes it responsive and agile in flight, allowing for precise handling, especially during takeoff, landing, and in-flight maneuvers.
  • Aerodynamic Efficiency: The aircraft’s dimensions also influence its aerodynamic efficiency. The 35 ft wingspan provides a balance between lift and drag, enabling the PA32-260 Cherokee Six to achieve optimal cruise performance and fuel economy. The sleek fuselage design further minimizes drag, contributing to its overall efficiency.
  • Cabin Space: While the PA32-260 Cherokee Six is relatively compact, its dimensions still allow for a comfortable cabin that can accommodate up to six people. The cabin is designed to provide ample headroom, legroom, and visibility for all occupants, making it suitable for both short and long-distance flights.
  • Hangar and Transportation: The dimensions of the aircraft also impact its hangar and transportation requirements. The PA32-260 Cherokee Six’s compact size makes it easier to store and transport, allowing it to fit into smaller hangars and be transported on standard aircraft trailers, reducing logistical challenges and costs.

In summary, the dimensions of the PIPER PA32-260 Cherokee Six, including its length of 28 ft 4 in and wingspan of 35 ft, are integral to its overall design and performance. These dimensions contribute to its maneuverability, aerodynamic efficiency, cabin space, and hangar and transportation requirements, making it a versatile and capable aircraft for various aviation applications.

Weight

The weight specifications of an aircraft, including its empty weight and maximum takeoff weight (MTOW), are critical components of the PIPER PA32-260 Cherokee Six Specs. These specifications have a significant impact on the aircraft’s performance, safety, and operational capabilities:

  • Performance: The weight of an aircraft directly affects its performance characteristics. The empty weight, which represents the weight of the aircraft without any passengers, cargo, or fuel, is a key factor in determining the aircraft’s power-to-weight ratio. A lower empty weight generally results in better performance, including faster climb rates, shorter takeoff distances, and higher cruise speeds.
  • Safety: Weight is also a crucial factor in ensuring the safety of an aircraft. The maximum takeoff weight represents the maximum allowable weight at which the aircraft is certified to safely take off. Exceeding the MTOW can compromise the aircraft’s structural integrity, handling characteristics, and takeoff performance, potentially leading to dangerous situations.
  • Operational Capabilities: The weight specifications influence the aircraft’s operational capabilities. The maximum takeoff weight determines the maximum payload capacity, which includes passengers, cargo, and fuel. A higher MTOW allows for greater flexibility in mission planning, as the aircraft can carry more weight without exceeding its structural or performance limitations.

In summary, the weight specifications of “2,650 lbs empty, 4,400 lbs max takeoff” are integral to the PIPER PA32-260 Cherokee Six Specs, as they directly impact the aircraft’s performance, safety, and operational capabilities. Understanding these specifications is essential for pilots and aviation professionals to operate the aircraft safely and efficiently.

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Performance

The performance specifications of “143 mph cruise speed, 750 nm range” are integral components of the PIPER PA32-260 Cherokee Six Specs, directly influencing the aircraft’s capabilities and suitability for various missions.


Cruise speed measures the aircraft’s speed when flying at a constant altitude and power setting. A cruise speed of 143 mph is relatively fast for a single-engine aircraft, indicating the Cherokee Six’s efficient design and powerful Lycoming IO-540 engine. This speed allows for quick and comfortable long-distance travel, reducing travel time and increasing overall efficiency.


Range measures the distance an aircraft can travel on a single fuel tank. The Cherokee Six’s range of 750 nm provides significant flexibility and autonomy, enabling non-stop flights between many cities and destinations. This extended range allows pilots to plan longer journeys without the need for refueling stops, making it suitable for cross-country flights, scenic tours, or accessing remote locations.

The combination of a 143 mph cruise speed and 750 nm range makes the PIPER PA32-260 Cherokee Six an ideal aircraft for private pilots, flight schools, and air taxi operators. Its performance capabilities enable efficient and versatile operations, meeting the demands of various aviation activities.

Engine

The engine specifications are a crucial aspect of the PIPER PA32-260 Cherokee Six Specs, as they define the power and performance capabilities of the aircraft. The Lycoming IO-540-K1G5D engine, with its 260 horsepower, plays a significant role in determining the aircraft’s flight characteristics, efficiency, and overall performance.

  • Power and Performance: The 260 horsepower generated by the Lycoming IO-540-K1G5D engine provides ample power for the Cherokee Six, enabling it to achieve a maximum cruise speed of 143 mph and a range of 750 nm. This combination of power and efficiency makes the aircraft suitable for various missions, including private flying, flight training, air taxi operations, and scenic tours.
  • Reliability and Durability: Lycoming engines are renowned for their reliability and durability, and the IO-540-K1G5D is no exception. This engine incorporates advanced engineering and manufacturing techniques to ensure longevity and minimize maintenance requirements, contributing to the overall dependability of the Cherokee Six.
  • Fuel Efficiency: The Lycoming IO-540-K1G5D engine is designed to operate efficiently, optimizing fuel consumption without compromising power or performance. This fuel efficiency is particularly advantageous for long-distance flights and cost-conscious operations, reducing operating expenses and extending the aircraft’s range.
  • Maintenance and Support: The Lycoming IO-540-K1G5D engine is widely used in aviation, ensuring ready availability of spare parts and maintenance support. This extensive support network contributes to the ease of maintenance and minimizes downtime, keeping the Cherokee Six operational and airworthy.

In summary, the engine specifications of “Lycoming IO-540-K1G5D, 260 hp” are integral to the PIPER PA32-260 Cherokee Six Specs, directly influencing the aircraft’s power, performance, reliability, fuel efficiency, and maintenance requirements. Understanding these specifications is essential for pilots, engineers, and aviation professionals to operate and maintain the Cherokee Six safely and efficiently.

Fuel

The fuel specification of “80 gallons usable capacity” is a crucial aspect of the PIPER PA32-260 Cherokee Six Specs, directly influencing the aircraft’s range, endurance, and operational flexibility.

  • Range and Endurance: The 80-gallon usable fuel capacity provides the Cherokee Six with a range of approximately 750 nm, enabling it to undertake extended cross-country flights or remain airborne for longer durations. This extended range enhances the aircraft’s suitability for long-distance travel, scenic tours, and missions requiring extended endurance.
  • Operational Flexibility: The generous fuel capacity allows pilots to plan flights with greater flexibility. They can depart with full fuel tanks, providing peace of mind and reducing the need for, especially when flying over remote areas or in conditions where fuel availability may be limited.
  • Payload and Range Optimization: The aircraft’s fuel efficiency and 80-gallon fuel capacity allow pilots to optimize payload and range based on mission requirements. For shorter flights, less fuel can be carried, increasing the available payload for passengers or cargo. Conversely, for longer flights, the full fuel capacity can be utilized to maximize range.
  • Fuel Management and Planning: The fuel specifications necessitate careful fuel management and planning by pilots. They must consider factors such as wind conditions, altitude, and fuel consumption rates to ensure they have sufficient fuel for the intended flight and any potential contingencies.

In summary, the fuel specification of “80 gallons usable capacity” is integral to the PIPER PA32-260 Cherokee Six Specs, as it directly influences the aircraft’s range, endurance, operational flexibility, and payload optimization. Understanding these specifications is essential for pilots to plan and execute safe and efficient flights.

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Avionics

The integration of the Garmin G1000 NXi avionics suite into the PIPER PA32-260 Cherokee Six Specs represents a significant advancement in the aircraft’s capabilities and safety features.

  • Enhanced Situational Awareness: The G1000 NXi suite provides pilots with an unparalleled level of situational awareness. Its high-resolution displays and intuitive interface present critical flight information, navigation data, and weather updates in an easily digestible format, reducing pilot workload and enhancing decision-making.
  • Improved Navigation and Communication: The G1000 NXi system seamlessly integrates navigation and communication functions, enabling pilots to access and manage flight plans, charts, and radios with ease. Its advanced navigation capabilities, coupled with GPS and WAAS technology, ensure precise and efficient navigation, even in challenging conditions.
  • Reduced Pilot Workload: By automating many routine tasks, such as flight planning, navigation, and communication, the G1000 NXi suite significantly reduces pilot workload. This allows pilots to focus on critical aspects of flight operations, such as monitoring the aircraft’s performance and managing the flight path, enhancing overall safety.
  • Increased Safety Features: The G1000 NXi avionics suite incorporates a range of safety features, including terrain awareness and warning systems (TAWS), traffic collision avoidance systems (TCAS), and stability augmentation systems (SAS). These systems provide pilots with real-time alerts and assistance, helping to prevent accidents and improve overall flight safety.

In summary, the Garmin G1000 NXi avionics suite is a cornerstone of the PIPER PA32-260 Cherokee Six Specs, offering enhanced situational awareness, improved navigation and communication, reduced pilot workload, and increased safety features. These advancements contribute to the overall capabilities and reliability of the aircraft, making it a preferred choice for pilots and aviation enthusiasts alike.

Safety

The integration of the Garmin GFC 700 autopilot and angle of attack (AOA) indicator in the PIPER PA32-260 Cherokee Six Specs significantly enhances the aircraft’s safety and overall flight characteristics. These advanced systems work in tandem to provide pilots with greater control, situational awareness, and protection against hazardous flight conditions.

  • Autopilot Functionality:

    The Garmin GFC 700 autopilot provides enhanced flight stability and reduces pilot workload, especially during long flights or demanding maneuvers. It can automatically maintain altitude, heading, and airspeed, freeing up the pilot to focus on other critical tasks, such as navigation and situational monitoring.

  • Angle of Attack Indicator:

    The angle of attack (AOA) indicator provides real-time information about the aircraft’s angle of attack, which is the angle between the aircraft’s wings and the oncoming airflow. Monitoring AOA is crucial for preventing stalls and maintaining optimal flight performance. The AOA indicator provides visual and audible alerts when the aircraft approaches critical angles of attack, helping pilots avoid dangerous situations.

  • Enhanced Safety Features:

    The combination of the autopilot and AOA indicator contributes to the Cherokee Six’s overall safety by reducing the risk of pilot error and increasing situational awareness. The autopilot can assist in maintaining a stable flight path, while the AOA indicator provides timely warnings of impending stalls. These systems work together to enhance the aircraft’s safety envelope and protect against hazardous flight conditions.

  • Improved Pilot Confidence:

    The presence of these safety systems instills greater confidence in pilots, allowing them to operate the aircraft more effectively and handle challenging flight situations with increased assurance. The autopilot’s ability to maintain stable flight reduces pilot fatigue, while the AOA indicator provides peace of mind by constantly monitoring the aircraft’s angle of attack.

In summary, the Garmin GFC 700 autopilot and angle of attack indicator are vital components of the PIPER PA32-260 Cherokee Six Specs, working together to enhance the aircraft’s safety, stability, and overall flight characteristics. These systems provide pilots with increased control, situational awareness, and protection against hazardous flight conditions, contributing to the aircraft’s reputation as a reliable and capable aircraft.

FAQs on PIPER PA32-260 Cherokee Six Specs

This section addresses frequently asked questions (FAQs) regarding the specifications of the PIPER PA32-260 Cherokee Six aircraft. These questions aim to provide a comprehensive understanding of the aircraft’s key technical details and their implications for pilots and aviation enthusiasts.

Question 1: What is the maximum takeoff weight of the PA32-260 Cherokee Six?

The maximum takeoff weight (MTOW) of the PA32-260 Cherokee Six is 4,400 lbs. This weight limit includes the aircraft’s empty weight, fuel, payload (passengers and cargo), and any additional equipment or modifications.

Question 2: What is the fuel capacity of the PA32-260 Cherokee Six?

The PA32-260 Cherokee Six has a usable fuel capacity of 80 gallons. This fuel capacity provides the aircraft with a range of approximately 750 nautical miles, making it suitable for long-distance flights.

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Question 3: What type of engine powers the PA32-260 Cherokee Six?

The PA32-260 Cherokee Six is powered by a Lycoming IO-540-K1G5D engine. This six-cylinder, air-cooled engine produces 260 horsepower, providing ample power for takeoff, climb, and cruise flight.

Question 4: What is the cruise speed of the PA32-260 Cherokee Six?

The PA32-260 Cherokee Six has a cruise speed of approximately 143 mph (124 knots). This speed allows for efficient and comfortable long-distance travel.

Question 5: What avionics suite is typically installed in the PA32-260 Cherokee Six?

The PA32-260 Cherokee Six is commonly equipped with the Garmin G1000 NXi avionics suite. This advanced avionics system provides pilots with enhanced situational awareness, navigation capabilities, and safety features.

Question 6: What safety features are included in the PA32-260 Cherokee Six?

The PA32-260 Cherokee Six incorporates several safety features, including a Garmin GFC 700 autopilot, angle of attack (AOA) indicator, and stall warning system. These features assist pilots in maintaining stable flight, preventing stalls, and enhancing overall safety during flight operations.

In summary, the PIPER PA32-260 Cherokee Six Specs provide detailed information about the aircraft’s dimensions, performance, engine specifications, fuel capacity, avionics, and safety features. Understanding these specifications is essential for pilots, engineers, and aviation professionals to operate and maintain the Cherokee Six safely and efficiently.

For further information and technical details, refer to the official aircraft specifications and manuals provided by the manufacturer.

Tips on Utilizing “PIPER PA32-260 Cherokee Six Specs”

Understanding the specifications of the PIPER PA32-260 Cherokee Six aircraft is crucial for safe and efficient operation. Here are several tips to effectively utilize these specifications:

Tip 1: Familiarize Yourself with the Specifications

Thoroughly review the aircraft’s specifications, including its dimensions, performance data, engine characteristics, fuel capacity, and avionics capabilities. This knowledge will provide a solid foundation for understanding the aircraft’s capabilities and limitations.

Tip 2: Use Specifications for Pre-Flight Planning

When planning a flight, consider the aircraft’s performance specifications to determine factors such as takeoff distance, climb rate, and cruise speed. This information will enable you to plan your flight route, calculate fuel requirements, and anticipate potential performance limitations.

Tip 3: Utilize Specifications for Weight and Balance Calculations

Accurately calculate the aircraft’s weight and balance before each flight. Refer to the weight and balance specifications to ensure that the aircraft is loaded within its allowable limits and that the center of gravity is within the prescribed range.

Tip 4: Monitor Performance during Flight

During flight, monitor the aircraft’s performance against the specified parameters. Observe engine temperatures, fuel consumption, and airspeed to ensure that the aircraft is operating within its normal operating range.

Tip 5: Refer to Specifications for Maintenance and Inspection

Use the aircraft’s specifications as a guide for maintenance and inspection schedules. Adhere to the recommended intervals for inspections, overhauls, and component replacements to maintain the aircraft’s airworthiness and safety.

Summary:

Effectively utilizing the “PIPER PA32-260 Cherokee Six Specs” requires a thorough understanding of the aircraft’s capabilities and limitations. By following these tips, pilots and aviation professionals can ensure safe and efficient operation of the Cherokee Six.

Conclusion

The PIPER PA32-260 Cherokee Six aircraft stands out with its impressive specifications, combining performance, versatility, and safety. Its dimensions, performance capabilities, engine characteristics, fuel capacity, avionics, and safety features have been meticulously engineered to meet the diverse needs of pilots and aviation enthusiasts alike.

Understanding these specifications is not only crucial for safe and efficient operation but also empowers pilots to unlock the full potential of the Cherokee Six. By adhering to the specified parameters and utilizing the aircraft’s capabilities to their advantage, pilots can maximize performance, ensure safety, and experience the joy of flying this exceptional aircraft.