STC - Data
- Type of Aircraft: Piper PA31T, PA31T1, PA31T2
- EASA: 10038174 R2 (issued Jan. 09, 2013)
- FAA: SA03249NY (issued Feb. 13, 2013)
- ANAC Argentina: 1212.42 (A) (issued Dec. 06, 2012)
- ANAC Brazil: 2017S10-05 (issued Sept. 06, 2017)
- TCCA Canada: STC SA16-41 (issued April 04, 2016)
- Applicable Aircraft: PA31T (Cheyenne II),
PA31T1 (Cheyenne 1, 1A), PA31T2 (Cheyenne IIXL)
- Engines: PT6A-11, PT6A-28 or Blackhawk PT6A-135, 135A
modification per FAA STC No. SA00863SE
- Propeller: MTV-27-1-E-C-F-R(P)/CFR210-58d
- Best vibration damping characteristics for almost
vibration free propeller operations
- Bonded on nickel alloy leading edge for superior
erosion protection of the blades
- General performance improvement (5% take-off & climb,
3kts cruise with 1900 rpm)
- No propeller speed restrictions on ground while operationg in low idle
- Significant cabin noise and vibration reduction
- Unbeatable esthetic ramp appeal
- More ground clearance for less FODs
- Unlimited blade life
- FOD repairable blades
- 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 65k)
MT-Propeller