PIPER PA-28RT-201T Turbo Arrow — Systems Description
1 systems description reference for the PIPER PA-28RT-201T Turbo Arrow.
Overview
PIPER AIRCRAFT CORPORATION PA-28RT-201T TURBO ARROW IV DESCRIPTION/OPERATION · 1978
The document provides a detailed description and operational guidelines for the Piper PA-28RT-201T Turbo Arrow IV aircraft. It covers the aircraft's systems, including the airframe, engine, propeller, and landing gear, along with safety features and operational procedures.
- The Turbo Arrow IV is a single-engine aircraft with retractable landing gear.
- It features a turbocharged 200 HP engine and can seat up to four occupants.
- The airframe is primarily made of aluminum alloy, with some steel and plastic components.
- Aerobatics are prohibited due to structural limitations.
- The engine is a six-cylinder, horizontally opposed, fuel-injected type.
- The landing gear is hydraulically actuated and can be extended or retracted in about seven seconds.
- The aircraft includes a safety feature that warns of inadvertent gear-up landings.
- The propeller can be either two-bladed or three-bladed.
1 document
PIPER PA-28RT-201T Turbo Arrow — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the PIPER PA-28RT-201T Turbo Arrow?
Sprinkle has 1 Systems Description document on file for the PIPER PA-28RT-201T Turbo Arrow.
What year is the PIPER PA-28RT-201T Turbo Arrow Systems Description?
The PIPER PA-28RT-201T Turbo Arrow Systems Description on file is dated 1978.
Where does Sprinkle's PIPER PA-28RT-201T Turbo Arrow Systems Description come from?
This PIPER PA-28RT-201T Turbo Arrow Systems Description was originally published by fliegen.ch and is hosted on Sprinkle with full text and specs.