Cessna 152 — Performance Data

This document presents a performance analysis of the Cessna 152, focusing on its drag characteristics and performance metrics. The analysis compares calculated values against those provided in the aircraft's Pilot Operating Handbook. Key findings indicate discrepancies in maximum speed and rate of climb due to conservative assumptions in drag coefficient calculations. The report is intended for educational purposes, particularly for students and professionals interested in aircraft performance evaluation.

• Maximum speed of Cessna 152 is calculated at 97 knots, compared to the manufacturer’s 110 knots.
• Rate of climb is calculated at 1436 ft/min, significantly higher than the rated 715 ft/min.
• The analysis indicates that assumptions in drag coefficient calculations can lead to discrepancies in performance metrics.
• The drag coefficient for the Cessna 152 was calculated to be 0.0142285.
• Future analyses should incorporate more precise measurements for improved accuracy.