Piper PA-28 Cadet — Performance Data
2 performance data references for the Piper PA-28 Cadet.
This document provides comprehensive performance data for the Piper PA-28-161 Cherokee Warrior II. It includes essential performance information required by FAA regulations, as well as additional performance details for optional systems and equipment. The performance data is based on measured flight test data corrected to ICAO standard day conditions and is analytically expanded for various parameters such as weight, altitude, and temperature. The document serves as a critical resource for pilots, offering performance graphs, flight planning examples, and detailed calculations necessary for safe and efficient flight operations. It emphasizes the importance of adhering to specified procedures to achieve the stated performance metrics and provides warnings against extrapolating data beyond chart limits.
- Maximum Takeoff Weight: 2325 lbs
- Basic Empty Weight: 1391 lbs
- Takeoff Distance Required (Headwind 15 KTS): 2100 ft
- Climb Rate: 420 ft/min
- Cruise Speed at 75% Power: 118 KTS TAS
- Total Fuel Required for Example Flight: 22.4 gal
- Endurance with 45 min reserve: 4.85 hrs