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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.