Piper PA-28RT Arrow IV Turbo — Systems Description
1 systems description reference for the Piper PA-28RT Arrow IV Turbo.
This document serves as a systems description for the Piper PA-28RT-201T Turbo Arrow IV, detailing various components and systems integral to the aircraft's operation. It includes part numbers and descriptions for critical engine and exhaust components, as well as maintenance notes. The intended audience includes pilots, maintenance personnel, and aviation enthusiasts who require detailed knowledge of the aircraft's systems. The document emphasizes the importance of proper assembly and inspection of components to ensure safe operation.
- Part numbers for right front cylinders range from 640964-101 to 640964-106.
- Inspect joints for freedom of movement and distortion in the exhaust system.
- Ensure proper rigging of nose landing gear proxy switches as per IPC 753-582.
- Tailpipe shroud forward part number is 641911-110.
- The document includes part numbers for various engine mounts and induction boxes.
How many Systems Description documents does Sprinkle have for the Piper PA-28RT Arrow IV Turbo?
Sprinkle has 1 Systems Description document on file for the Piper PA-28RT Arrow IV Turbo.
What year is the Piper PA-28RT Arrow IV Turbo Systems Description?
The Piper PA-28RT Arrow IV Turbo Systems Description on file is dated 2010.
How many pages is the Piper PA-28RT Arrow IV Turbo Systems Description?
The Piper PA-28RT Arrow IV Turbo Systems Description runs 1 pages.
Where does Sprinkle's Piper PA-28RT Arrow IV Turbo Systems Description come from?
This Piper PA-28RT Arrow IV Turbo Systems Description was originally published by www.acornwelding.com and is hosted on Sprinkle with full text and specs.