Diamond DA40 Diamond Star

TCDS: A00011AT Max Weight: 2,535 lbs

Other

Certification
Normal

Aircraft Overview

Official TCDS specifications for Diamond DA40 Diamond Star per Type Certificate A00011AT

⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate A00011AT. Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
2,535 lbs
Max Landing
2,535 lbs
Typical Empty
1,785 lbs
Max Baggage
88 lbs
Useful Load
750 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tanks 90.6 in Main fuel tanks (standard configuration)
Rear Seats 118.1 in Rear passenger positions
Baggage Area 142.8 in Primary baggage compartment
Pilot Front Seats 85.0 in Pilot and front passenger positions

Center of Gravity Envelope

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

📊 normal category Category
Datum: Leading edge of wing root chord
🔧 Engine Specifications
Engine Model
Lycoming IO-360-M1A
Power Output
180 HP
Fuel Type
100LL
Total Fuel
50 gal
Usable Fuel
48 gal
📋 Key Specifications
TCDS Number A00011AT
Max Weight 2,535 lbs
Engine Lycoming IO-360-M1A
Power 180 HP
Category Normal
🏁 Speed Limits
VNE (Never Exceed) 188 KIAS
VNO (Normal) 147 KIAS
VFE (Flaps) 108 KIAS
VS (Stall Clean) 58 KIAS
VS0 (Stall Landing) 54 KIAS
📈 Performance Notes

The Diamond DA40 features modern composite construction, exceptional fuel efficiency with 147 KTAS cruise speed, and excellent training characteristics with T-tail design.

⚠️ Important Disclaimers

Verification Required

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

TCDS Reference

This summarizes TCDS A00011AT 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.