STC
FAA
Cessna
|
Cessna
170, 172 &175
with Lycoming 0-360 and 2-blade
MTV-15-B/210-58
|
SA02245CH
|
(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 |
SA01220WI
|
| |
Cessna
172R, 172 S
Lyc.
IO-360-L2A
3-blade (electric) MTV-18-B/183-17 |
SA00926WI
|
|
Cessna
180, 182, 185, 206, T206, 207, T207, 210, T210
Continental engines
3-blade MTV-9-D/210-58 and
2-blade MTV-15-D/210-58 |
SA02294CH
(March
23, 2007)
Executive Sales and Leasing
Phone:
866-717-1117
715-924-4410
|
| |
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
|
SA
00927WI
(Nov.
30, 2000) |
| |
Cessna
182Q, -R
TCM O-470-U
3-blade MTV-9-D/195-18b
|
SA
00927WI
(Nov.
30, 2000) |
(picture
not
available yet..) |
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 |
SA01438WI
(June
14, 2007)
|
| |
Cessna
A185E, -F
TCM IO-520-D
2-blade MTV-15-D/210-58
more
information (pdf 79k) |
SA01296WI
|
| |
Cessna
A185E, -F
TCM IO-520-D
3-blade MTV-9-D/210-58
more
information (pdf 74k) |
SA
01296 WI
|
| |
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) |
SA
01604SE
(Sept
29, 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)
|
SA01439WI
(June
14, 2007)
|
|
In Flight Test:
Cessna
206 SOLOY Mark II with
our 5 bladed scimitar composite
MTV-5-1-D-C-F-R(A)/CFR210-56
meets the newest and highest European
noise requirements.
The installation provides improved performance and additionally
sounds like a jet. |
i.p. |
|
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) |
SA
00925WI
|
|
Cessna
310
with Continental IO-470D, U, V, and IO-470VO and 3-blade
MTV-9-D-C-F/CF198-52
more
information |
|
|
Cessna
336, 337-A, -B, -C, -D, -E, -F,
M337-B
TCM IO-360- C, -G, -CB, -GB
3-blade
MTV-12-D-C-F/CF192-119a (front) +
3-blade MTV-12-D-C-F/CFLD192-119a (rear)
more
information
(pdf 69k) |
SA
02460AT
Coastal Planes, Inc.
(April
01, 2002) |
|
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) |
SA01284WI
(Nov. 23, 2004) |
|
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)
|
SA02510NY
(Feb.
20, 2008)
|
|
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) |
SA01294WI
(Nov. 23, 2004) |
| |
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.
|
i.p. |
 |
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)
|
SA02550NY
(July 2008) |
|