STC - Data
- Type of Aircraft: PC-12
- EASA: 10014953 R5 (issued July 23, 2021)
- FAA: SA02742NY (issued March 29, 2021)
- TCCA: Letter of Acceptance of the EASA STC (issued July 31, 2024)
- DGAC Mexico: Letter of acceptance of the EASA STC
- Applicable Aircraft: Pilatus PC-12, PC-12/45, PC-12/47,
PC-12/47E
- Engines: P&WC PT6A-67B, PT6A-67P (Note: PT6A-67P Engine Installation according to EASA STC 10065179 (FAA STC SA02266LA) only applicable in EASA region)
- 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)
FACTS for the latest PC12 props available:
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