Piper Cherokee PA-28-180
TCDS: 2A13 Max Weight: 2,400 lbs
Piper Aircraft Corporation
Aircraft Overview
Official TCDS specifications for Piper Cherokee PA-28-180 per Type Certificate 2A13
Critical weight and balance data per Type Certificate 2A13. Verify against current aircraft records before flight operations.
Weight Limits
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.
The Piper Cherokee PA-28-180 achieves a maximum speed of 150 KTAS at 75% power, service ceiling of 15,500 feet, and range of 640 nautical miles. The 180 HP Lycoming O-360 provides excellent climb performance and load-carrying capability.
⚠️ 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.