Cessna 310L Pilot's Operating Handbook
CESSNA 310L · Pilot's Operating Handbook
Overview
The Cessna 310L Pilot's Operating Handbook (POH) provides essential information for the operation of the Cessna 310L aircraft. It is designed for pilots and aviation enthusiasts, offering detailed guidance on the aircraft's systems, performance, and operational procedures. This handbook includes critical data such as weight and balance, performance specifications, and emergency procedures, ensuring safe and efficient flight operations. The POH serves as a comprehensive reference for preflight planning, in-flight operations, and post-flight procedures, making it an indispensable tool for anyone flying the Cessna 310L.
- Wingspan: 36 ft 0 in
- Max Takeoff Weight: 5,200 lbs
- Fuel Capacity: 80 gallons
- Takeoff Distance: 2,500 ft
- Stall Speed Clean: 70 knots
Document
Source
Originally published by www.inflightpilottraining.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 72
- File size
- 43 MB
- Publisher
- www.inflightpilottraining.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 1,000
- Engine (hp)
- 285
- Height (ft)
- 8.83
- Length (ft)
- 27.75
- Propeller
- McCauley 3-blade
- Wingspan (ft)
- 36
- Engine model
- Continental IO-520
- Empty weight (lb)
- 3,200
- Fuel capacity (gal)
- 80
- Rate of climb (fpm)
- 1,000
- Service ceiling (ft)
- 20,000
- Max takeoff weight (lb)
- 5,200
Performance
- Landing distance (ft)
- 2,200
- Takeoff distance (ft)
- 2,500
Weight & balance
- Useful load (lb)
- 2,000
- Max ramp weight (lb)
- 5,250
- Basic empty weight (lb)
- 3,200
- Max takeoff weight (lb)
- 5,200
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 310L.
- 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
This section outlines the key specifications of the Cessna 310L, including dimensions, weight limits, and fuel capacity. The aircraft features a wingspan of 36 feet 0 inches, a length of 27 feet 9 inches, and a height of 8 feet 10 inches. The maximum takeoff weight is 5,200 lbs, with an empty weight of approximately 3,200 lbs and a fuel capacity of 80 gallons.
Performance Data
The performance section details the aircraft's capabilities, including takeoff and landing distances, stall speeds, and climb rates. The Cessna 310L has a takeoff distance of 2,500 feet and a landing distance of 2,200 feet. The stall speed in a clean configuration is 70 knots, while the landing stall speed is 60 knots.
Weight and Balance
This section provides guidelines for calculating weight and balance to ensure safe flight operations. The maximum ramp weight is 5,250 lbs, and the useful load is approximately 2,000 lbs. The center of gravity (CG) range is specified to maintain stability during flight.
Emergency Procedures
Emergency procedures are critical for ensuring pilot and passenger safety. This section includes steps for engine failure, electrical failure, and other in-flight emergencies, providing pilots with the necessary actions to take in various scenarios.
V-Speeds
The V-speed section lists important airspeeds for the Cessna 310L, including VSO (stalling speed in landing configuration) at 60 knots, VS1 (stalling speed in clean configuration) at 70 knots, and VNE (never exceed speed) at 200 knots.
Safety notes
- Always perform a weight and balance calculation before flight.
- Be aware of the VNE speed to avoid structural damage.
What's in the CESSNA 310L TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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