DIAMOND DA42 TDI — Systems Description
1 systems description reference for the DIAMOND DA42 TDI.
Overview
Diamond DA42 Aircraft Systems Overview
The document provides an overview of the Diamond DA42 TDI aircraft systems, detailing its construction, limitations, and various systems including the powerplant and flight controls. It covers essential operational aspects and safety features of the aircraft.
- The DA42 is a low wing, twin-engine aircraft made primarily of carbon-fiber reinforced plastic.
- Maximum operating altitude is 18,000 feet.
- The aircraft features a fully integrated Garmin G1000 avionics system.
- It is powered by two turbocharged diesel engines generating 135hp each.
- The aircraft has a maximum takeoff weight of 3935 lbs.
- Flaps are electronically operated with three positions: Cruise, Approach, and Landing.
- The emergency locator transmitter can transmit for up to 72 hours.
- Cabin ventilation is controlled by multiple outlets and does not have an active cooling system.
1 document
DIAMOND DA42 TDI — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the DIAMOND DA42 TDI?
Sprinkle has 1 Systems Description document on file for the DIAMOND DA42 TDI.
Where does Sprinkle's DIAMOND DA42 TDI Systems Description come from?
This DIAMOND DA42 TDI Systems Description was originally published by squarespace.com and is hosted on Sprinkle with full text and specs.