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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.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

1 document

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