Piper Seneca PA-34-200T
TCDS: A16CE Max Weight: 4,750 lbs
Piper Aircraft Corporation
Aircraft Overview
Official TCDS specifications for Piper Seneca PA-34-200T per Type Certificate A16CE
Critical weight and balance data per Type Certificate A16CE. Verify against current aircraft records before flight operations.
Weight Limits
Loading Stations & Arms
| Station | Arm | Description |
|---|---|---|
| Third Row | 148.0 in | Standard loading position |
| Fuel Tanks | 95.0 in | Main fuel tanks (standard configuration) |
| Second Row | 118.0 in | Standard loading position |
| Front Seats | 85.5 in | Standard loading position |
| Baggage Area | 169.0 in | Primary baggage compartment |
Center of Gravity Envelope
CG must remain within these limits throughout all phases of flight.
The Piper Seneca provides six-seat twin-engine capability with 190 KTAS cruise speed, counter-rotating props, and excellent short-field performance.
⚠️ Important Disclaimers
Verification Required
Always verify against current aircraft records and equipment list before flight operations.
TCDS Reference
This summarizes TCDS A16CE 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.