Cessna 310R

TCDS: 3A16 Max Weight: 5,500 lbs

Cessna Aircraft Company

Certification
Normal

Aircraft Overview

Official TCDS specifications for Cessna 310R per Type Certificate 3A16

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⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate 3A16. Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
5,500 lbs
Max Landing
5,200 lbs
Typical Empty
3,605 lbs
Max Baggage
200 lbs
Useful Load
1,895 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tanks 85.0 in Main fuel tanks (standard configuration)
Rear Seats 118.0 in Rear passenger positions
Front Seats 80.5 in Standard loading position
Baggage Area 142.0 in Primary baggage compartment

Center of Gravity Envelope

CG must remain within these limits throughout all phases of flight.

📊 aft limit Category
📊 forward limit Category
🔧 Engine Specifications
Engine Model
Continental IO-520-M (2x)
Power Output
285 HP
Fuel Type
100LL
Oil Capacity
12 qt
📋 Key Specifications
TCDS Number 3A16
Max Weight 5,500 lbs
Engine Continental IO-520-M (2x)
Power 285 HP
Category Normal
🏁 Speed Limits
VNE (Never Exceed) 266 KIAS
VNO (Normal) 223 KIAS
VFE (Flaps) 160 KIAS
VS (Stall Clean) 89 KIAS
VS0 (Stall Landing) 81 KIAS
📈 Performance Notes

The Cessna 310R delivers reliable twin-engine performance with 220 KTAS cruise speed, counter-rotating propellers, and proven business aviation capabilities.

⚠️ Important Disclaimers

Verification Required

Always verify against current aircraft records and equipment list before flight operations.

TCDS Reference

This summarizes TCDS 3A16 but does not replace the official document.

Regulatory Compliance

Calculations must comply with 14 CFR Part 23 and applicable airworthiness directives.

Data Accuracy

Specifications may vary by serial number and modifications. Verify with aircraft documentation.