CESSNA 172S SKYHAWK SP — Systems Description
1 systems description reference for the CESSNA 172S SKYHAWK SP.
Overview
CESSNA 172SP Part I · 2011
This document serves as a systems description for the Cessna 172S Skyhawk SP, detailing various operational and technical aspects of the aircraft. It is designed for pilots and aviation enthusiasts, providing essential information on fuel capacity, weight limits, engine operation, and emergency procedures. The content includes questions and answers that cover critical systems, performance metrics, and operational guidelines, ensuring that users have a comprehensive understanding of the aircraft's capabilities and limitations. The document is structured in a quiz format, allowing for self-assessment of knowledge regarding the Cessna 172S.
- Total usable fuel capacity: 56 gallons
- Maximum weight in baggage area 1: 120 lbs
- Short field takeoff distance to clear a 50' obstacle: 2180 ft
- Landing distance over a 50' obstacle: 1430 ft
- Maximum demonstrated crosswind: 17 knots
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