Cessna-210N-VH-TQC-POH.pdf - Flight Tech Australia
CESSNA 210 · Pilot's Operating Handbook
Overview
This Airplane Flight Manual (AFM) is specifically designed for the Cessna P-210 Pressurized Centurion II. It serves as a comprehensive guide for pilots, providing essential information regarding the aircraft's operation, performance, and safety procedures. The manual includes detailed sections on aircraft specifications, operating limitations, emergency procedures, and performance data, ensuring that pilots have the necessary knowledge to operate the aircraft safely and efficiently. It is an essential resource for both new and experienced pilots flying the P-210, offering insights into the unique features and capabilities of this pressurized aircraft.
- Maximum takeoff weight: 3,600 lbs (1,632 kg)
- Cruise speed: 175 knots
- Stall speed: 60 knots
- Maximum altitude: 25,000 feet
- Fuel capacity: 80 gallons (303 liters)
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at flighttech.com.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- Pages ·
- 465
- File size ·
- 40 MB
- Copy found at ·
- flighttech.com.au
What is the Cessna-210N-VH-TQC-POH.pdf - Flight Tech Australia?
The Cessna-210N-VH-TQC-POH.pdf - Flight Tech Australia is a pilot's operating handbook for the CESSNA 210.
How many pages is the Cessna-210N-VH-TQC-POH.pdf - Flight Tech Australia?
The copy of the Cessna-210N-VH-TQC-POH.pdf - Flight Tech Australia on file runs 465 pages.
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In this document
Aircraft Specifications
The Cessna P-210 features a maximum takeoff weight of 3,600 lbs (1,632 kg) and a useful load of approximately 1,200 lbs (544 kg). The aircraft is powered by a Continental TSIO-520-U engine, producing 300 horsepower. The maximum cruise speed is around 175 knots, with a stall speed of 60 knots.
Operating Limitations
The manual outlines critical operating limitations, including a maximum altitude of 25,000 feet and a maximum speed of 200 knots. Pilots must adhere to specific weight and balance requirements to ensure safe flight operations.
Emergency Procedures
Emergency procedures are detailed for various scenarios, including engine failure, cabin depressurization, and electrical system malfunctions. Pilots are instructed on immediate actions to take in these situations to ensure safety.
Performance Data
Performance data includes takeoff and landing distances under various weight conditions and environmental factors. For example, at maximum weight and standard conditions, the takeoff distance is approximately 1,500 feet.
Fuel Requirements
The P-210 requires 100LL aviation gasoline, with a total fuel capacity of 80 gallons (303 liters). The manual specifies fuel management practices to optimize performance and range.
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Safety notes
- Ensure weight and balance are within limits before flight.
- Follow emergency procedures as outlined in the manual.
- Monitor engine performance during flight.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.