DASSAULT FALCON 20F-5 — Systems Description
1 systems description reference for the DASSAULT FALCON 20F-5.
Overview
Falcon 20F-5BR · 1990
The document provides a detailed overview of the Dassault Falcon 20F-5 aircraft, highlighting its design, performance, and operational characteristics. It covers the aircraft's specifications, systems, and maintenance requirements, as well as its competitive advantages in the midsize jet market.
- Maximum range of 2,400 nautical miles.
- Cabin volume of 700 cubic feet with seating for 9 passengers.
- Powered by TFE731-5 turbofan engines.
- Cruising altitude up to FL 420.
- Typical BOW around 18,500 lb.
- MTOW of 29,100 lb., with an optional 30,350 lb. MTOW.
- Requires 6,500 ft. of runway when fully loaded.
- Features a 5-parallel buss DC electrical system.
1 document
DASSAULT FALCON 20F-5 — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the DASSAULT FALCON 20F-5?
Sprinkle has 1 Systems Description document on file for the DASSAULT FALCON 20F-5.
What year is the DASSAULT FALCON 20F-5 Systems Description?
The DASSAULT FALCON 20F-5 Systems Description on file is dated 1990.
Where does Sprinkle's DASSAULT FALCON 20F-5 Systems Description come from?
This DASSAULT FALCON 20F-5 Systems Description was originally published by flightsolution.com and is hosted on Sprinkle with full text and specs.