N9758H-C-182R-POH.pdf - Blue Sky Aviation Association
CESSNA 182P SKYLANE · Pilot's Operating Handbook
Overview
This document provides performance data specifically for the Cessna F-182 Skylane. It is intended for pilots and aviation enthusiasts who require detailed information regarding the aircraft's operational capabilities. The manual includes critical performance metrics such as takeoff and landing distances, climb rates, and fuel consumption under various conditions. It serves as a comprehensive reference for understanding the aircraft's performance in different flight scenarios, ensuring pilots can make informed decisions during operations.
- Takeoff distance at max weight: 1,200 feet
- Climb rate: 730 feet per minute
- Landing distance at max weight: 1,000 feet
- Cruise fuel consumption: 12 gallons per hour
- Weight and balance calculations are critical for safe operations.
Document
Source
Originally published by www.blueskyaa.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 281
- File size
- 61 MB
- Publisher
- www.blueskyaa.com
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 182P SKYLANE.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Takeoff Performance
The takeoff performance section outlines the distances required for takeoff under various weight conditions and environmental factors. For example, at sea level and standard temperature, a maximum weight takeoff requires approximately 1,200 feet of runway.
Climb Performance
Climb performance data indicates that the Cessna F-182 Skylane can achieve a rate of climb of approximately 730 feet per minute at sea level under standard conditions. This section also provides information on the best rate of climb speed.
Landing Performance
Landing performance details the required distances for landing based on weight and wind conditions. The document specifies that landing from a maximum weight requires about 1,000 feet of runway under standard conditions.
Fuel Consumption
The fuel consumption section provides data on fuel burn rates at various power settings. For example, at cruise power settings, the aircraft consumes approximately 12 gallons per hour.
Weight and Balance
This section discusses the importance of weight and balance calculations for safe flight operations. It includes charts and tables to assist pilots in determining the center of gravity based on load distribution.
Safety notes
- Ensure weight and balance calculations are completed before flight.
- Monitor fuel levels to avoid running out during flight.
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