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DIAMOND DA40 — Systems Description

1 systems description reference for the DIAMOND DA40.

Overview
Diamond DA 40-TDI- G1000 Systems Version 1.0

The document provides technical specifications and details about the Diamond DA40-NG aircraft, including its dimensions, weight, speeds, and various systems. It serves as a reference for understanding the aircraft's capabilities and operational limits.

  • The Diamond DA40-NG has a glide ratio of 1:9.7.
  • The maximum takeoff weight is 1310 kg.
  • The maximum landing weight is 1216 kg.
  • The empty weight of the aircraft is 944.9 kg.
  • The aircraft features multiple antennas for communication and navigation.
  • The stall speed varies with weight, ranging from 58 KIAS to 66 KIAS.
  • The VNO speed is 130 KIAS and VNE is 172 KIAS.
  • The baggage compartment can hold a maximum of 45 kg.
1 document
DIAMOND DA40 — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the DIAMOND DA40?

Sprinkle has 1 Systems Description document on file for the DIAMOND DA40.

Where does Sprinkle's DIAMOND DA40 Systems Description come from?

This DIAMOND DA40 Systems Description was originally published by salt.aero and is hosted on Sprinkle with full text and specs.

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