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Piper PA-31T Cheyenne II ↗

The Cheyenne II’s pitch system includes a stability augmentation system that varies the elevator force.

Aircraft type

Engines

Two Pratt & Whitney PT6A-28

Early PA-31T / Cheyenne II reference; excludes Cheyenne I and PA-42 III.
Rated power

620 shp each

Early PA-31T / Cheyenne II reference; excludes Cheyenne I and PA-42 III.
Wingtip fuel tanks

30 US gal per side

Early PA-31T / Cheyenne II reference; excludes Cheyenne I and PA-42 III.
Pitch augmentation

Stability-augmentation system

Early PA-31T / Cheyenne II reference; excludes Cheyenne I and PA-42 III.
SIMULATORS

implementations
EXPLORE FURTHERManuals & resources →

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