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LET L-410 UVP-E — Systems Description

1 systems description reference for the LET L-410 UVP-E.

Overview
LET L-410 UVP, UVP-E, LET L-420 "T URBO LE T"

The document provides technical information about the L-410 UVP-E aircraft, detailing its development history, specifications, and operational capabilities. It covers various aspects of the aircraft's design, including its engines, performance, and systems.

  • The L-410 UVP-E is a high-wing commuter aircraft.
  • It was developed in the 1960s by Let Kunovice for Aeroflot.
  • The first flight of the L-410 UVP-E occurred in 1984.
  • It features M601E engines and five-blade propellers.
  • The aircraft has a maximum take-off weight of 6400 kg.
  • Seating capacity ranges from 17 to 19 passengers.
  • Cruise speed is 170 KIAS with a maximum range of about 770 nautical miles.
  • It is certified for IFR operation and flights in icing conditions.
1 document
LET L-410 UVP-E — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the LET L-410 UVP-E?

Sprinkle has 1 Systems Description document on file for the LET L-410 UVP-E.

Where does Sprinkle's LET L-410 UVP-E Systems Description come from?

This LET L-410 UVP-E Systems Description was originally published by railwaymates.com and is hosted on Sprinkle with full text and specs.