Piper Super Cub PA-18

TCDS: A-759 Max Weight: 1,750 lbs

Piper Aircraft Corporation

Certification
Normal

Aircraft Overview

Official TCDS specifications for Piper Super Cub PA-18 per Type Certificate A-759

⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate A-759. Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
1,750 lbs
Max Landing
1,750 lbs
Typical Empty
1,030 lbs
Max Baggage
100 lbs
Useful Load
720 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tanks 95.0 in Main fuel tanks (standard configuration)
Rear Seats 121.0 in Rear passenger positions
Baggage Area 142.8 in Primary baggage compartment
Pilot Front Seats 85.5 in Pilot and front passenger positions

Center of Gravity Envelope

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

📊 normal category Category
← Forward Limit: 78.0 in
Aft Limit: 86.0 in →
Variable Limits by Weight:
@ 1,500 lbs 78.0 in → 86.0 in
@ 1,750 lbs 78.0 in → 86.0 in
Max Weight: 1,750 lbs
Datum: Leading edge of wing root chord
🔧 Engine Specifications
Engine Model
Lycoming O-320-B2B
Power Output
150 HP
Fuel Type
100LL
Total Fuel
36 gal
Usable Fuel
35 gal
📋 Key Specifications
TCDS Number A-759
Max Weight 1,750 lbs
Engine Lycoming O-320-B2B
Power 150 HP
Category Normal
🏁 Speed Limits
VNE (Never Exceed) 163 KIAS
VNO (Normal) 100 KIAS
VFE (Flaps) 87 KIAS
VS (Stall Clean) 43 KIAS
VS0 (Stall Landing) 40 KIAS
📈 Performance Notes

The Piper Super Cub PA-18 is legendary for STOL performance with a maximum speed of 130 KTAS, exceptional climbing ability, and outstanding short-field capabilities.

⚠️ Important Disclaimers

Verification Required

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

TCDS Reference

This summarizes TCDS A-759 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.