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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

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

1 document
CESSNA 172S SKYHAWK SP — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the CESSNA 172S SKYHAWK SP?

Sprinkle has 1 Systems Description document on file for the CESSNA 172S SKYHAWK SP.

What year is the CESSNA 172S SKYHAWK SP Systems Description?

The CESSNA 172S SKYHAWK SP Systems Description on file is dated 2011.

How many pages is the CESSNA 172S SKYHAWK SP Systems Description?

The CESSNA 172S SKYHAWK SP Systems Description runs 13 pages.

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