Piper PA-28 Archer — Specifications
1 specifications reference for the Piper PA-28 Archer.
Overview · 1998 PIPER ARCHER III SPECIFICATIONS · 1998
This document provides detailed specifications for the 1998 Piper Archer III, a four-seat, single-engine aircraft known for its reliability and performance. It includes information on the powerplant, dimensions, weights, fuel capacity, and performance metrics. The specifications are essential for pilots and aviation enthusiasts to understand the aircraft's capabilities and limitations. The document also outlines recommended airspeeds and performance figures under standard conditions, making it a valuable reference for flight planning and operations.
- 180-hp Lycoming O-360-A4M engine with a TBO of 2,000 hours.
- Maximum gross weight of 2,550 lb and useful load of 875 lb.
- Takeoff distance over a 50-ft obstacle is 1,610 ft.
- Cruise speed at 75% power at 8,000 ft is 128 KTAS with a fuel consumption of 63 pph.
- V Y (best rate of climb) is 76 KIAS.