MT Piper PA-31T() Cheyenne

STC – Data

Type of Aircraft: Piper PA31T, PA31T1, PA31T2

EASA: 10038174 issued Jan. 25, 2012
FAA: SA03249NY (issued Feb. 13, 2013)
ANAC Argentina: 1212.42 (A) (issued Dec. 06, 2012)

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
Advantages:

• 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)