STC - Data
- Type of Aircraft: PC-12
- EASA: 10014953 R6 (issued March 28, 2023)
- FAA: SA02742NY (issued March 05, 2024)
- TCCA: Letter of Acceptance of the EASA STC (issued July 31, 2024)
- Applicable Aircraft: Pilatus PC-12, PC-12/45, PC-12/47,
PC-12/47E
- Engines: P&W PT6A-67B, P&W PT6A-67P, P&W PT6E-67XP
- Propeller: MTV-47-1-N-C-F-R(P)/CFR260-361
- Advantages:
- Best vibration damping characteristics
- Bonded on nickel alloy leading edge for best erosion
protection of the blades
- No engine modifications
- Certified Ground roll distance reduced by approx. 10%; AFMS amended
- Certified Take-off distance over 50 ft obstacle reduced by approx. 15%; AFMS amended
- Climb performance improved
- Unlimited blade life
- More ground clearance for less FODs
- FOD repairable blades
- Significant inside and outside noise reduction
- 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
- 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 250k)