CESSNA 320C — Systems Description
1 systems description reference for the CESSNA 320C.
This document provides a detailed systems description for the CESSNA 320C aircraft, specifically focusing on the exhaust system and its components. It outlines the necessary inspections, maintenance procedures, and part numbers for various exhaust system components associated with the TCM TSIO-470 engine. This information is crucial for maintenance personnel and pilots to ensure the safety and airworthiness of the aircraft. The document emphasizes the importance of regular inspections and the replacement of certain components at specified intervals to prevent failures and maintain optimal performance.
- Visual inspection of the exhaust system every 50 hours or 30 days.
- Remove and inspect tailpipes for cracks and corrosion annually.
- Replace multi-segment V-band clamps every 500 hours of operation.
- Inspect exhaust system every 12 months with a pressure test.
- Remove exhaust system for inspection every 2500 hours or 12 years.
How many Systems Description documents does Sprinkle have for the CESSNA 320C?
Sprinkle has 1 Systems Description document on file for the CESSNA 320C.
How many pages is the CESSNA 320C Systems Description?
The CESSNA 320C Systems Description runs 1 pages.
Where does Sprinkle's CESSNA 320C Systems Description come from?
This CESSNA 320C Systems Description was originally published by www.acornwelding.com and is hosted on Sprinkle with full text and specs.