|
Piper
PA-18, PA-18A, PA-18S, PA-18AS series
Lyc. O-320,
O-360
2-blade (hydraulic)
MTV-15-C/200-15
or
MTV-15-B/210-58 |
certified
by
Professional Pilots Inc.
SA02087CH |
|
Piper
PA-24-400
3-blade MTV-9-B/198-58a |
certified
by
Charles S. Horton Jr.
SA01462WI |
| |
Piper
PA-28-180, -181
Lycoming O-360-A3A, -A4A
3-blade (electric) MTV-18-B/180-17 |
|
| |
Piper
PA-28R-201T, -RT-201T
TCM TSIO-360-FB
3-blade MTV-12-D/188-30d
more
information (pdf 81k) |
SA
02598AT
(Jan.
08, 2003) |
| |
Piper
PA31P-425
with MTV-16-1-E-C-F/CFRL225-37a
Better take off,
climb and improved cruise speed while reducing dramatically the noise
and vibration level. |
FAA
STC work starting 2011 |
|
Piper
PA-32-R300
Lycoming IO-540-K1G5D
3-blade MTV-9-B/198-52
more
information (pdf 78k) |
SA03446AT |
|
MTV-9-B/198-52
Scimitar Blade Propeller Certified for PA32 turbo and
non turbo series |
certified
by Professional Pilots Inc.
SA02695CH
(March 25, 2009) |
|
Piper
PA34-() Seneca II, III, IV, V
Engines: TCM TSIO-360-EB, -KB, -RB
with MTV-12-D-C-F/CF(L)188-53
more
information (pdf 67k)
|
SA
03434AT
(April
19, 2007) |
|
Piper PA-42/42-720
with 4-blade
MTV-16-1-E-C-F-R(P)/CFR230-37b props. Engines: PT6A-41
or -61.
The 4-blade MT-Composite Prop replaces the old 3-blade Hartzell Q
Tip prop.
Improved performance, reduced noise
and less weight.
Meets Germany's
enhanced noise
restrictions.
The noise level is below 80 dB(A) according to ICAO Annex 16, Chapter
10.
more
information (pdf 65k)
|
FAA
STC i.p. |
|
PA42-1000
with 5 blade
MTV-27-1-E-C-F-R(G)/CFR()250-103 World's fastest
conventional turbo prop again faster by up to 5 kts and sounds like
a Jet with dramatically reduced outside and inside noise plus improved
ground clearance.
more
information (pdf 76k)
|
SA03487AT
(Sept.
10, 2007) |
| |
Piper
PA-46-310P
TCM
TSIO-520-BE or TSIO-550-C
4-blade MTV-14-D/190-17 or
4-blade MTV-14-D/195-30a
Reduction of max. continuous RPM to 2500 RPM
more
information (pdf 70k) |
SA
01542AT
MT-Propeller
USA, Inc. |
| |
Piper
PA-46-350P
Lycoming TIO-540-AE2A
4-blade MTV-14-B/190-17 or
4-blade MTV-14-B/195-30a
more
information (pdf 69k) |
SA
01654AT
MT-Propeller
USA, Inc. |
| |
Piper
PA-60-601P, S/N
61P-0157-001 to
0714-7963345
Lycoming IO-540-P1A5, -S1A5, equipped with turbocharger per STC
# SE60WE or SE81WE
4-blade MTV-14-B-C-F/CF188-30d
RPM limitation: max. 2575 RPM
more
information (pdf 68k) |
SA
02246AT
MT-Propeller
USA, Inc. |
|
Piper
PA-60-602P
PA-60-60,
-601, -601P, -602P with FAA STC SA1658NM, ("Machen Conversion")
with (L)TIO-540-U2A
IO-540-S1A5-MM, IO-540-AA1A5-MM
4-blade MTV-14-B-C-F/CF(L)188-30d
more
information (pdf 68k) |
SA01511SE
|
|
Piper
PA-60-700P
Lycoming (L)TIO-540-U2A
4-blade MTV-14-B-C-F/CF(L)188-30d
more
information (pdf 68k) |
SA02024NY
(Nov. 12, 2004) |