STC - Data
- Type of Aircraft: P.68( )
- EASA: 10014445 Rev. 3 (issued Nov. 30, 2017)
- FAA: SA03420AT (issued Jan. 05, 2007)
- Applicable Aircraft: Vulcanair P.68, P.68B, P.68C, P.68 Observer,
P.68 Observer 2, P.68R
- Engines: Lycoming IO-360-A1B, IO-360-A1B6
- Propeller: MTV-12-B-C-F/CF183-59b or
MTV-12-B-C-F/CF183-53 (wide chord)
- Advantages:
- Best vibration damping characteristics for
almost vibration free propeller operation!
- Bonded on stainless steel leading edge for
best erosion protection of the blades!
- Take-off distance over 50 ft remains unchanged
with the CF183-59b blades!
- Take-off distance shortened by 55 m
with the wide chord CF183-53 blades!
- Enhanced climb by approx. 3% (SL, ISA conditions, MTOW)
increasing by altitude!
- Enhanced cruising speeds by approx. 2 to 3 kts
(ISA, FL160, 4550 lbs GW)
with the CF183-59b blades
- Plus 5 kts with the wide chord CF183-53 blades!
- Approx. 12 lbs less total weight than the original propellers!
- Unlimited blade life!
- Significant inside and outside noise reductions!
- ICAO Annex 16, Vol I, Part II, Chapter X EASA approved noise levels!
- FOD repairable blades!
- Some models equipped with the CF183-53 blades (wide chord)
comply with the strict German noise regulations
2010– „Landeplatz-Lärmschutz-Verordnung“
for unrestricted airport operations in Germany
and other European Countries in conjunction
with the LIESE exhaust!
more
information about the STC (.pdf 70k)