Pilatus PC-12

STC – Data

• Type of Aircraft: PC-12
• EASA: EASA.A.S.03217 (issued March 2009)
• FAA: SA02742NY
• TCCA (Canada) STC: Letter of acceptance to the EASA STC
• Applicable Aircraft: Pilatus PC-12, PC-12/45, PC-12/47,
  PC-12/47E
• Engines: P&WC PT6A-67B, PT6A-67P
• Propeller: MTV-27-1-N-C-F-R(P)/CFR260-65a
• Advantages:

• Best vibration damping characteristics
• Bonded on nickel alloy leading edge for best erosion
  protection of the blades
• No engine modifications
• Ground roll distance reduced by approx. 15%
• Take-off distance over 50 ft obstacle reduced by approx. 5%
• Climb performance improved
• Cruise performance improved by up to 5 kts
  versus the PC-12 POH/AFM
• More ground clearance for less FODs
• Approx. 4 lbs less weight than the original metal propeller
• Significant inside and outside noise reductions
• Aircraft noise level is about 4 dB(A) less than
  with the original metal propeller
• Cabin noise is reduced by 6 to 7 dB(A) depending on location
• Unlimited blade life
• FOD repairable blades

more information about the STC (.pdf 75k)