Piper Archer PA-28-181

TCDS: 2A13 Max Weight: 2,550 lbs

Piper Aircraft Corporation

Certification
Normal

Aircraft Overview

Official TCDS specifications for Piper Archer PA-28-181 per Type Certificate 2A13

⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate 2A13. Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
2,550 lbs
Max Landing
2,550 lbs
Typical Empty
1,478 lbs
Max Baggage
200 lbs
Useful Load
1,072 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tanks 95.0 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 85.5 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: 83.0 in
Aft Limit: 93.0 in →
Variable Limits by Weight:
@ 1,950 lbs 83.0 in → 93.0 in
@ 2,325 lbs 87.0 in → 93.0 in
@ 2,550 lbs 87.0 in → 93.0 in
Datum: Leading edge of wing
🔧 Engine Specifications
Engine Model
Lycoming O-360-A4M
Power Output
180 HP
Fuel Type
100LL
Total Fuel
50 gal
Usable Fuel
48 gal
📋 Key Specifications
TCDS Number 2A13
Max Weight 2,550 lbs
Engine Lycoming O-360-A4M
Power 180 HP
Category Normal
🏁 Speed Limits
VNE (Never Exceed) 154 KIAS
VNO (Normal) 125 KIAS
VFE (Flaps) 102 KIAS
VS (Stall Clean) 63 KIAS
VS0 (Stall Landing) 58 KIAS
📈 Performance Notes

The Piper Archer PA-28-181 features a maximum speed of 145 KTAS at 75% power, service ceiling of 13,650 feet, and range of 696 nautical miles. Enhanced with improved interior and modern avionics capabilities.

⚠️ Important Disclaimers

Verification Required

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

TCDS Reference

This summarizes TCDS 2A13 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.