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STC Diamond DA20-C1
  • Diamond DA20-C1 with MT fixed pitch
  • Diamond DA20-C1 with MT fixed pitch

STC - Data


  • Type of Aircraft: DA20-C1

  • EASA: EASA.A.S.01404 (issued March. 14, 2006)
  • FAA: SA03373AT (issued Jan. 8, 2007)
  • TCCA (Canada) STC: SA07-41 (issued June 08, 2007)
  • ANAC (Brazil) CST: 2012S06-09 (issued June 15, 2012)

  • Applicable Aircraft: Diamond DA20-C1
  • Engines: TCM IO-240-B
  • Propeller: MT 175 R 150-2Ca
    with/without Heggeman Silencer

  • Advantages:
  • Best vibration damping characteristics
  • Bonded on stainless steel leading edge for best erosion
    protection of the blades
  • Installed Propeller and Spinner total weight remain unchanged.
  • Enhanced cruising speeds by approx. 5 to 8 kts
    (ISA conditions, MTOW)
  • Significant inside and outside noise reduction
  • Unlimited blade life
  • FOD repairable blades

more information about the STC (.pdf 75k)