MT Socata TBM 700 / 850

STC – Data

• Type of Aircraft: TBM 700 series – 700/850
• EASA: 10033038 (issued Dec. 15, 2010)
• FAA: SA02958NY (issued May 26, 2011)
• TCCA Transport Canada: Letter of acceptance to the EASA STC
  (issued April 17, 2012)
• ANAC (Brazil) CST: 2012S07-07 (issued July 05, 2012)
• Applicable Aircraft: Socata TBM 700 A, B, C1, C2, N
• Engines: P& WC PT6A-64, -66D
• Propeller: MTV-27-1-E-C-F-R(P)/CFR225-55f

Advantages:

• Provides best vibration damping characteristics for almost
  vibration free propeller operation
• Has bonded on nickel alloy leading edges for best erosion
  protection of the blades
• Reduces the weight by approx. 7 lbs compared with the
  original metal propeller
• Provides a cooler ITT on ground with condition lever at
  low and high idle position
• Has no propeller speed restrictions on ground while
  operating in low idle
• Gives more ground clearance for less FODs.
• Provides significant cabin noise and vibration reduction
• All models comply with the strict German noise regulations 2010–
  „Landeplatz Lärmschutz Verordnung“

more information about the STC (.pdf 80k)