PA-31-350 Chieftain — Piper Aircraft PA-31-350 Chieftain
Fleet & certification
- Origin
- US
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
PA31 PA31 | — | 3,100 kg | 880 nm | 183 kt | 8 |
Other models in this family
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Piper Aircraft PA-31-350 Chieftain manuals & documents
12 documents for the Piper Aircraft PA-31 family — Avionics Manual · Weight And Balance · Performance Data · Pilot's Operating Handbook · Checklist · Training Manual · Parts Catalog · Service Bulletins · Specifications · Other Documents. PDFs served from cdn.sprinkle.com.
No documents are catalogued for the PA-31-350 Chieftain specifically; these are the Piper Aircraft PA-31 family documents.
This document serves as a comprehensive overview of the Piper PA-31P Pressurized Navajo, detailing its specifications, performance, and operational characteristics. It is aimed at pilots and aviation enthusiasts who are interested in understanding the capabilities and maintenance considerations of this aircraft model. The document discusses the aircraft's design, engine specifications, fuel consumption, and operational costs, providing valuable insights for potential owners and operators. The PA-31P is highlighted for its powerful performance, spacious cabin, and the complexities associated with its maintenance and operation.
- Gross weight: 7800 lbs
- Engine: Lycoming TIGO-541-E1A, 425 hp
- Cruise speed: 220 knots at 75% power
- TBO: 1200 hours
- Usable fuel capacity: 236 gallons
Weight And Balance
Performance Data
Pilot's Operating Handbook
Checklist
Service Bulletins
Specifications
Documents are sourced from publicly available references. Sprinkle does not host OEM-restricted materials; if you are a rights-holder and want a document removed, email .