Piper PA-31T Cheyenne II — Checklist
1 checklist reference for the Piper PA-31T Cheyenne II.
Overview
PIPER CHEYENNE II PA-31
This document serves as a checklist for the Piper PA-31T Cheyenne II, detailing operational limitations, emergency procedures, and critical performance data. It is intended for pilots operating this aircraft model, providing essential information to ensure safe and efficient flight operations. The checklist includes speed limitations, weight specifications, fuel requirements, and emergency procedures for various scenarios, including engine failure and electrical issues. This reference is crucial for pre-flight preparations and in-flight decision-making, ensuring pilots are well-informed about the aircraft's capabilities and limitations.
- Maximum take-off weight: 9,000 lbs
- Total fuel capacity: 374 U.S. gallons
- Usable fuel capacity: 366 U.S. gallons
- Va (maneuvering speed): 177 Kias
- Vne (never exceed speed): 242 Kias
- Emergency procedures for engine failure include specific power lever and prop control actions
- Single engine go-around requires MCP of 620 SHP as needed
1 document