Cessna 310L Pilot's Operating Handbook
CESSNA 310L · Pilot's Operating Handbook
Overview
This Pilot's Operating Handbook (POH) is designed for the Cessna 310L, a twin-engine aircraft known for its reliability and performance. The handbook provides essential information for pilots, including operating procedures, performance data, and safety guidelines. It serves as a comprehensive reference for both flight planning and in-flight operations, ensuring that pilots can operate the aircraft safely and efficiently. The POH includes detailed specifications, weight and balance information, and emergency procedures, making it an indispensable tool for Cessna 310L pilots.
- Wingspan: 36 ft 0 in
- Max Takeoff Weight: 5,200 lbs
- Cruise Speed: 170 knots
- Service Ceiling: 20,000 ft
- Rate of Climb: 1,200 ft/min
Document
Source
Originally published by www.myhra.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 84
- File size
- 27 MB
- Publisher
- www.myhra.org
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 260
- Height (ft)
- 8.83
- Length (ft)
- 28.75
- 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)
- 1,200
- Service ceiling (ft)
- 20,000
- Max takeoff weight (lb)
- 5,200
Performance
- Takeoff distance (ft)
- 2,500
Weight & balance
- Useful load (lb)
- 2,000
- Max ramp weight (lb)
- 5,200
- Baggage allowance (lb)
- 300
- 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
The Cessna 310L features a wingspan of 36 feet 0 inches, a length of 28 feet 9 inches, and a height of 8 feet 10 inches. The empty weight is approximately 3,200 lbs, with a maximum takeoff weight of 5,200 lbs. The fuel capacity is 80 gallons, allowing for extended flight range.
Performance Data
The Cessna 310L has a maximum speed of 200 knots and a cruise speed of 170 knots. The aircraft can achieve a service ceiling of 20,000 feet and has a rate of climb of 1,200 feet per minute. Takeoff distance over a 50-foot obstacle is approximately 2,500 feet.
Weight and Balance
The basic empty weight of the Cessna 310L is 3,200 lbs, with a maximum ramp weight of 5,200 lbs. The useful load is 2,000 lbs, and the baggage allowance is 300 lbs. The center of gravity (CG) range is from 35 to 45 inches.
V-Speeds
Key V-speeds for the Cessna 310L include: VSO (stalling speed in landing configuration) at 60 knots, VS1 (stalling speed in clean configuration) at 70 knots, VY (best rate of climb speed) at 90 knots, and VNE (never exceed speed) at 200 knots.
Emergency Procedures
The handbook outlines critical emergency procedures, including engine failure during takeoff, electrical failure, and emergency landing techniques. Pilots are advised to familiarize themselves with these procedures to ensure safety in flight.
Safety notes
- Always perform a preflight inspection before each flight.
- Ensure weight and balance are within limits before takeoff.
- Be familiar with emergency procedures and V-speeds.
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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