Van's Aircraft RV-7A

TCDS: N/A (Experimental) Max Weight: 1,800 lbs

Other

Certification
Experimental

Aircraft Overview

Official TCDS specifications for Van's Aircraft RV-7A per Type Certificate N/A (Experimental)

⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate N/A (Experimental). Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
1,800 lbs
Max Landing
1,800 lbs
Typical Empty
1,090 lbs
Max Baggage
100 lbs
Useful Load
710 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tanks 60.5 in Main fuel tanks (standard configuration)
Front Seats 62.5 in Standard loading position
Baggage Area 84.0 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
Lycoming IO-360 (typical)
Power Output
180 HP
Fuel Type
100LL
Oil Capacity
8 qt
📋 Key Specifications
TCDS Number N/A (Experimental)
Max Weight 1,800 lbs
Engine Lycoming IO-360 (typical)
Power 180 HP
Category Experimental
🏁 Speed Limits
VNE (Never Exceed) 220 KIAS
VNO (Normal) 180 KIAS
VFE (Flaps) 87 KIAS
VS (Stall Clean) 51 KIAS
VS0 (Stall Landing) 47 KIAS
📈 Performance Notes

The RV-7A provides exceptional experimental aircraft performance with 200 KTAS cruise speed, aerobatic capability, and proven kit aircraft design.

⚠️ Important Disclaimers

Verification Required

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

TCDS Reference

This summarizes TCDS N/A (Experimental) 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.