MT-Propeller EASA STC Cessna

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June 7, 2010

STC EASA
Cessna

(picture not available yet..)	Cessna 152, A152, F152, FA152 Lycoming O-235 2-blade natural composite fixed pitch MT183R115-2C in combination with silencer system Liese R74x8x100	STC EASA.A.S.00578 (Feb. 09, 2005)
(picture not available yet..)	Cessna 152, F152 Lycoming O-235 3-blade (electric) MTV-7-F/170-09	STC SA0270 (April 27, 1992)
	Cessna 172K, -L, -M, F172L, -M Lycoming O-320 3-blade (electric) MTV-18-C/180-17f Reduction of max. continuous RPM to 2500 RPM Installation of muffler "System Gomolzig" 74-100 or muffler "Liese" R 74x8x100	STC SA0243 (Sept. 09, 1998)
(picture not available yet..)	Cessna 172N, -P, F172N, -P Lycoming O-320 3-blade (electric) MTV-18-C/180-17f Reduction of max. continuous RPM to 2500 RPM Installation of muffler "System Gomolzig" 74-100 or muffler "Liese" R 74x8x100A	STC SA0242 (Sept. 09, 1998)
(picture not available yet..)	Cessna 172D, -E, -F, -K, -L, -M, -N, -P, F172D, -F, -G, -H, -K, -L, -M, -N, -P Lycoming O-360-A1A (FAA STC SA807CE) 3-blade MTV-12-B/183-17	STC SA0706 (Mar. 19, 1996)
	Cessna 172R, 172 S Lyc. IO-360-L2A 3-blade (electric) MTV-18-B/183-17	STC SA1098 (Jan. 20, 2000)
(picture not available yet..)	Cessna 172RG Lycoming O-360 3-blade MTV-12-B/183-17 Installation of muffler Gomolzig Cessna 172 RG-606500	STC SA0425 (June 15, 1993)
(picture not available yet..)	Cessna R172K, FR172 K TCM IO-360 3-blade MTV-12-D/180-17 Installation of muffler "System Gomolzig" 74-0101 or muffler Liese R74x8x100	STC SA0275 (Jan. 17, 1996)
	Cessna FR172 -E, -F, -G, -H, -J TCM IO-360-D, -H, -J 3-blade MTV-12-D/180-17	STC SA0195 (Jan. 17, 1996)
	Cessna 182, -A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -L, -M, -N, -P, F182P TCM O-470-L, O-470-R, O-470-S, 3-blade MTV-9-D/195-18b Installation of muffler "System Gomolzig" C182-606500 or Liese R74x8x100	STC SA0587 (Feb. 06, 1996)
	Cessna 182Q, -R TCM O-470-U 3-blade MTV-9-D/195-18b Installation of muffler "System Gomolzig" C182-606500 or Liese R74x8x100	STC SA0585 (Feb. 06, 1996)
(picture not available yet..)	Cessna 182Q, -R TCM IO-550-D (with EMZ SA1115 and SA1120) 4-blade MTV-14-D/193-53 Max. RPM: 2500, Installation of muffler system "Gomolzig C182-606600" required.	STC SA1276 (Aug. 21, 2002)
	Cessna 182, -A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -L, -M, -N, -P, F182P TCM O-470-L, O-470-R, O-470-S, 3-blade MTV-9-D/203-52	EASA.A.S.01406 (June 8, 2006)
	Cessna A185E, -F TCM IO-520-D 2-blade MTV-15-D/210-58 more information (pdf 79k)	STC SA1391 (July 26, 2004)
	Cessna A185E, -F TCM IO-520-D 3-blade MTV-9-D/210-58 more information (pdf 74k)	STC SA1391 (July 26, 2004)
	Cessna U206G on floats with Soloy Turbine conversion 5-bld. w/reverse MTV-5-1-E-C-F-R(M)/CFR220-54 more information (pdf 76k)	EASA STC No. EASA.A.S.00749 (May 31.2005)
	Cessna U206G und TU206G powered by a Soloy Turbine Pac, landplane and amphibian, with and without reverse, MTV-5-1-E-C-F-R(M)/CFR220-54 and MTV-5-1-E-C-F/CF220-54 more information (pdf 76k) (reverse) more information (pdf 94k)	EASA STC No. EASA.A.S.00749 (May 31.2005)
	In Flight Test: Cessna 206 Mark II with our 5 blade scimitar composite MTV-5-1-D-C-F-R(A)/CFR210-56 Rolls-Royce 250-B17F/2 Series meets the newest and highest European noise requirements. The installation provides improved performance and additionally sounds like a jet. more information (pdf 77k)	EASA STC expected May 2010
	Cessna 208, 208A, 208B Caravan with 4-Blade MTV-16-1-E-C-F-R(P)/CFR250-55 Equal or better performance, perceptible noise reduction, 79.1 dB(A) according to ICAO Annex 16 Chapter X, less weight, less diameter thus more ground clearance thus less erosion, less vibration thus much smoother run more information (pdf 74k)	EASA STC No. EASA.A.S.01128 (July 28.2005)
	Cessna T210M, T210N, T210R, P210R, P210N TCM TSIO-520-R, TSIO-520-CE, TSIO-520-P, TSIO-520-AF 4-blade MTV-14-D/195-30a	STC SA1063 (Sept. 21, 1999)
	Cessna 340, 340A also included: RAM III and RAM IV conversion TCM TSIO-520-( ) 4-blade MTV-14-D-C-F/CF188-30g more information (pdf 71k)	STC SA1347 (Sept. 15, 2003)
	Cessna 340, 340A with RAM VII improved performance and drastically reduced vibration and inside - outside noise 4-blade MTV-14-D-C-F/CF188-30g more information (pdf 73k)	EASA.A.S.C.03290
	Cessna 414 also included: RAM III and RAM IV conversion TCM TSIO-520-( ) 4-blade MTV-14-D-C-F/CF188-30g more information (pdf 73k)	STC SA1318 (April 09, 2003)
	Cessna 414A with and without FAA STC SA4546SW MTV-14-D-C-F/CF188-30g. TCM TSIO-520-N, - NB, -NB modified by FAA STC SE4327SW. Improved overall performance with a turbine like noise and vibration signature.	EASA.A.S.02493 (Juli 21, 2009)
	Cessna C421C with 4 blade scimitar MTV-16-1-E-C-F/CF225-37a optional in combination with FAA STCs SA438NW, SA5193NM, SA8352SW, SA00015SE, SA5811SW more information (pdf 73k)	EASA.A.S.03114 (Dec 18, 2007)