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:
- Best vibration damping characteristics for almost
vibration free propeller operations
- Bonded on nickel alloy leading edge for best erosion
protection of the blades
- General performance improvement
(5% take-off & climb, 3-5 kts cruise with 1800 rpm)
- Same weight than the original 4-blade metal propeller
- Cooler ITT on ground with condition lever at
low and high idle position
- No propeller speed restrictions on ground
while operating in low idle
- Unlimited blade life
- More ground clearance, less FODs
- FOD repairable blades
- Significant cabin noise and vibration reduction
- All models comply with the strict German noise regulations
2010– „Landeplatz Lärmschutz Verordnung“ for unrestricted airport
operations in Germany and other European Countries.
more
information about the STC (.pdf 80k)