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Diamond DA62 — Weight And Balance

3 weight and balance references for the Diamond DA62.

Overview · DA62 MPP Configuration for Geo Survey and Mapping · 2021

This document provides detailed specifications and operational data for the Diamond DA62 MPP, specifically tailored for geo surveying and mapping applications. It includes critical information on mass and balance, performance metrics, and operational capabilities. The document is intended for pilots, operators, and aviation enthusiasts interested in the DA62 MPP's performance in various mission profiles. Key features include maximum take-off mass, empty mass, payload capacities, and fuel consumption rates, ensuring users can effectively plan and execute their missions with the aircraft.

  • Maximum Take-Off Mass: 5,071 lbs (2,300 kg)
  • Empty Mass: 3,803 lbs (1,725 kg)
  • Payload Capacity: 1,268 lbs (575 kg)
  • Fuel Tank Capacity: 86 US gallons (326 liters)
  • Minimum Operation Speed: 76 KIAS (140 km/h)
  • Maximum Cruise Speed: 192 KTAS (356 km/h)
  • Certified Service Ceiling: 20,000 ft (6,096 m)

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