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CESSNA A185F FLOATPLANE · Pilot's Operating Handbook
Overview
This document is a Pilot Operating Handbook (POH) for the Cessna 414A, covering various model years from 1979 to 1985. It serves as a comprehensive guide for pilots operating this twin-engine aircraft, providing essential information on performance, operating procedures, and safety. The POH includes specifications, limitations, and emergency procedures, ensuring that pilots have the necessary knowledge to operate the aircraft safely and efficiently. This handbook is crucial for both training and reference during flight operations, making it an indispensable resource for pilots and aviation enthusiasts alike.
- Maximum takeoff weight: 4,800 lbs (2,177 kg)
- Cruise speed: approximately 200 knots
- Range: about 1,200 nautical miles
- Maximum altitude: 25,000 feet
- Fuel capacity: 110 gallons (416 liters)
Document
Source
Originally published by www.aircraftspruce.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Year
- 1985
- Pages
- 1
- File size
- 86 KB
- Publisher
- www.aircraftspruce.com
Most owners only have the POH. Here's the essential set for the CESSNA A185F FLOATPLANE.
- 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
Aircraft Specifications
The Cessna 414A is a twin-engine aircraft with a maximum takeoff weight of 4,800 lbs (2,177 kg). It features a cruise speed of approximately 200 knots and a range of about 1,200 nautical miles. The aircraft is powered by two Continental TSIO-520-U engines, each producing 300 horsepower.
Operating Limitations
Pilots must adhere to specific operating limitations, including a maximum altitude of 25,000 feet and a stall speed of 70 knots in landing configuration. The POH outlines weight and balance requirements, emphasizing the importance of proper loading to maintain aircraft performance.
Emergency Procedures
The emergency procedures section details critical actions for various in-flight emergencies, including engine failure, electrical failure, and cabin depressurization. Pilots are instructed on how to handle these situations to ensure passenger safety and aircraft integrity.
Performance Data
Performance data includes takeoff and landing distances under various weight conditions and environmental factors. For example, at sea level and standard temperature, the takeoff distance is approximately 2,200 feet.
Fuel Requirements
The Cessna 414A requires 100LL aviation fuel, with a total fuel capacity of 110 gallons (416 liters). The POH provides guidance on fuel management and consumption rates during flight.
Safety notes
- Always perform a weight and balance calculation before flight.
- Follow emergency procedures as outlined in the POH to ensure safety.
- Ensure proper fuel type is used to avoid engine damage.
Full document text
1033 CM WP ME HA AP LG EP CS IN EL AV TO PS BV WWW.AIRCRAFTSPRUCE.COM Prices Subject to Change without Notice - Valid as of June 1, 2025. Please view our website for current prices. 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