Piper PA-28 Cherokee 180 — Specifications
1 specifications reference for the Piper PA-28 Cherokee 180.
Overview
PIPER CHEROKEE 180 – PA-28-180 · 1963
This document provides specifications for the Piper PA-28 Cherokee 180, a four-seat aircraft powered by a 180-hp Lycoming engine. Introduced in 1963, the Cherokee 180 features a spacious cabin and improved handling characteristics compared to earlier models. The document outlines key performance metrics, including weight limits, fuel capacity, and operational performance. It serves as a reference for pilots and aviation enthusiasts interested in the capabilities and specifications of this particular model.
- Gross weight: 2,450 lbs
- Empty weight: 1,395 lbs
- Fuel capacity: 50 gallons
- Cruise speed: 129 knots
- Stall speed: 53 knots
- Initial climb rate: 725 feet per minute
- Range: 507 nautical miles
- Service ceiling: 14,150 feet
1 document