PA-28-180: Specifications, Features, and Buying Guide

Discover the iconic Piper PA-28-180, a remarkable single-engine aircraft that has shaped general aviation history. Whether you’re a prospective buyer, aviation enthusiast, or pilot in training, this comprehensive guide will walk you through everything you need to know about this versatile aircraft.

The Piper PA-28-180, commonly known as the Cherokee 180, stands as a testament to reliable aircraft design. This single-engine piston aircraft features fixed landing gear, making it an ideal choice for pilots across skill levels. Since its introduction in the 1960s, it has maintained its reputation for stable flight characteristics, straightforward maintenance, and versatile performance in various roles from training to personal transportation.

History and Development of the Piper PA-28 Series

The early 1960s marked the birth of the PA-28 series, with Piper Aircraft’s vision to create a modern, all-metal aircraft. The inaugural PA-28 Cherokee’s successful flight in 1960 paved the way for numerous variants. By 1965, the series expanded to include the larger PA-32 Cherokee Six, accommodating six passengers and addressing market demands for increased capacity.

Overview of the Piper PA-28-180 Model

The PA-28-180E variant, particularly from 1970, exemplifies Piper’s engineering excellence. This four-seat aircraft combines performance and efficiency through its single piston engine design. While Piper later developed retractable gear variants like the PA-28R-201 Arrow III, the PA-28-180’s fixed gear design remains popular for its operational simplicity and cost-effectiveness.

Specifications and Features of the Piper PA-28-180

Technical Specifications

  • Engine: Lycoming O-360 series producing 180 horsepower
  • Maximum takeoff weight: 2,400 lbs (1,089 kg)
  • Useful load: Approximately 1,000 lbs (454 kg)
  • Fuel capacity: 50-72 gallons (189-273 liters)
  • Seating capacity: 4 people (including pilot)

Design and Construction

The PA-28-180 features an all-metal construction, ensuring durability and easy maintenance. Its distinctive low-mounted wing design provides exceptional stability and visibility. The unpressurized cabin, while limiting high-altitude operations, contributes to the aircraft’s reliability and simplified maintenance requirements.

Performance and Capabilities

Performance Metric Specification
Cruise Speed 124 knots (230 km/h)
Service Ceiling 14,000 feet (4,267 meters)
Range 665 nautical miles (1,232 km)
Climb Rate 740 feet per minute (3.8 m/s)

Cockpit and Interior of the Piper PA-28-180

The PA-28-180’s cockpit exemplifies practical design, balancing functionality with comfort. While compact compared to larger Piper models, the interior layout maximizes available space, creating an optimal environment for both training and personal transportation. The fixed landing gear configuration simplifies operation and maintenance, particularly beneficial in training scenarios where operational simplicity is paramount.

Cockpit Layout and Controls

The PA-28-180’s cockpit showcases thoughtful design focused on pilot efficiency. The 1968 upgrade brought significant improvements to the Cherokee series, replacing traditional ‘push-pull’ engine controls with modern quadrant levers that enhanced operational ease and sophistication.

  • Wide, accommodating instrument panel with clean, uncluttered layout
  • Essential flight instruments positioned directly in front of pilot
  • Engine gauges strategically placed for easy monitoring
  • Ergonomically designed control yokes for extended flight comfort
  • Adjustable rudder pedals to suit various pilot heights

A distinctive feature is the unique placement of propeller RPM and manifold pressure/fuel flow gauges above the pilot’s right knee. While this layout may require initial adjustment, it provides quick reference during critical flight phases. The multiengine-style throttle quadrant, inherited from earlier Cherokee models, adds professional sophistication to this single-engine aircraft.

Comfort and Interior Design

The PA-28-180’s interior balances functionality with comfort in its four-seat configuration. The 1968 enhancement added a third window on each side, modernizing the fuselage appearance while significantly improving visibility and natural light for all occupants.

  • Comfortable seats with adjustable positions for various body types
  • Strategic storage space behind rear seats
  • Accessible storage areas for charts and headsets
  • Durable, low-maintenance interior finishes
  • Enhanced natural lighting through additional windows

Variants and Comparisons

The Piper PA-28 series has continuously evolved to meet diverse aviation needs. Each variant builds upon the original design while incorporating technological advancements and market demands, maintaining the Cherokee series’ popularity through ongoing improvements in performance, comfort, and efficiency.

Different Variants of the Piper PA-28

Variant Key Features
Archer TX/LX Updated avionics, improved performance
Archer DX/DLX Diesel-powered, better fuel efficiency
Pilot 100i Cost-effective flight training solution

Comparison with Competitors

Feature PA-28-180 Cessna 172
Wing Design Low-wing High-wing
Cruise Speed Higher Lower
Short-field Performance Good Better
Useful Load Higher Lower

Buying Guide for the Piper PA-28-180

The PA-28-180 Cherokee 180 represents a reliable investment for both novice and experienced pilots. Its enduring market presence reflects its quality and performance capabilities, making it a popular choice in general aviation.

Factors to Consider When Buying

  • Comprehensive pre-buy inspection by a qualified Cherokee-series mechanic
  • Current market value assessment and price comparison
  • Total airframe hours and engine time since overhaul
  • Avionics upgrades and overall condition
  • Detailed maintenance history documentation
  • Market trends and comparable model pricing

Maintenance and Operating Costs

The PA-28-180’s fixed landing gear design contributes significantly to its cost-effective maintenance profile. This straightforward configuration eliminates the complexity and associated expenses typically found in retractable gear systems, though regular maintenance remains essential for safety and longevity.

  • Engine maintenance – reliable Lycoming O-360 with reasonable service costs
  • Fuel efficiency – approximately 10 gallons per hour at cruise power
  • Regular inspections – annual checks required by regulations
  • Insurance costs – competitive rates within its class
  • Hangar fees – standard storage expenses
  • Avionics updates – periodic modernization requirements
Cost Category Frequency
Annual Inspection Yearly
Engine Maintenance As per hours flown
Avionics Updates As needed/required
Insurance Annual renewal

Conclusion

The Piper PA-28-180 Cherokee 180 stands as a testament to reliable and versatile aircraft design in general aviation. Its enduring popularity stems from an effective combination of solid performance characteristics, straightforward maintenance requirements, and overall value proposition.

  • Proven track record in flight training and personal use
  • Fixed landing gear contributing to lower maintenance costs
  • Stable flight characteristics ideal for various skill levels
  • Strong resale value and market presence
  • Extensive support network for parts and service

For prospective buyers, conducting thorough pre-purchase inspections remains crucial for ensuring a sound investment. The aircraft’s combination of reliability, efficiency, and practical design features continues to make it a compelling choice in the ever-evolving general aviation market, whether for training purposes or private ownership.

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About Author

Dan Mercer

Dan Mercer, retired air traffic controller with 35 years of service at Chicago O’Hare International Airport. After graduating from the FAA Academy in Oklahoma City in 1978, he guided thousands of aircraft safely through some of America’s busiest airspace. During his distinguished career, Dan received multiple commendations for his calm handling of several potential disaster scenarios, including a severe weather crisis in 1994 that required rerouting over 200 flights. A respected mentor who trained dozens of controllers, he now spends his time volunteering at aviation museums and occasionally guest lecturing at flight schools. “The sky never gave me a day’s work—it gave me a lifetime of purpose; every safe landing was my reward.”

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