Mooney M20J 201

TCDS: A21SO Max Weight: 2,740 lbs

Other

Certification
Normal

Aircraft Overview

Official TCDS specifications for Mooney M20J 201 per Type Certificate A21SO

⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate A21SO. Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
2,740 lbs
Max Landing
2,740 lbs
Typical Empty
1,640 lbs
Max Baggage
120 lbs
Useful Load
1,100 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tanks 25.5 in Main fuel tanks (standard configuration)
Rear Seats 31.5 in Rear passenger positions
Front Seats 13.2 in Standard loading position
Baggage Area 50.5 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
Lycoming IO-360-A3B6D
Power Output
200 HP
Fuel Type
100LL
Oil Capacity
8 qt
📋 Key Specifications
TCDS Number A21SO
Max Weight 2,740 lbs
Engine Lycoming IO-360-A3B6D
Power 200 HP
Category Normal
🏁 Speed Limits
VNE (Never Exceed) 196 KIAS
VNO (Normal) 174 KIAS
VFE (Flaps) 132 KIAS
VS (Stall Clean) 61 KIAS
VS0 (Stall Landing) 57 KIAS
📈 Performance Notes

The Mooney M20J delivers exceptional speed and efficiency with 201 KTAS cruise speed, retractable landing gear, and distinctive forward-swept tail design.

⚠️ Important Disclaimers

Verification Required

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

TCDS Reference

This summarizes TCDS A21SO 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.