MT-Propeller EASA STC Piper

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July 22, 2008

STC EASA
Piper

	Piper PA-28-160, -161, -161 Cadet Lycoming O-320 3-blade (electric) MTV-18-C/175-36 I nstallation of muffler Gomolzig PA28-606502 or Mecan Air PA-28 in model PA-28-161 or 161 Cadet	STC SA0525 (May 05, 1994)
(picture not available yet..)	Piper PA-28-180, -181 Lycoming O-360-A3A, -A4A 3-blade (electric) MTV-18-B/180-17	STC SA0230 (Nov. 18, 1991)
(picture not available yet..)	Piper PA-28-R201, -RT201, -R200, -R180 (200 HP Version) Lycoming IO-360 3-blade MTV-12-B/180-17	STC SA0401 (Oct. 15, 1996)
	Piper PA-28R-201T, -RT-201T TCM TSIO-360-FB 3-blade MTV-12-D/188-30d more information (pdf 78k)	STC SA1173 (May 29, 2000)
(picture not available yet..)	Piper PA-28-235 Lycoming O-540 3-blade MTV-9-B/195-45a Reduction of continuous speed to 2400 RPM	STC SA1093 (Oct. 13, 1998)
	Piper PA-32-R300 Lycoming IO-540-K1G5D 3-blade MTV-9-B/198-52 more information (pdf 80k)	EASA.A.S.00748
	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 112k)	EASA STC No. EASA.A.S.02553 (March 13, 2006)
(picture not available yet..)	Piper PA-38-112 Lycoming O-235 3-blade (electric) MTV-7-F/170-09	STC SA0272 (April 28, 1992)
	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 60k)	STC No. EASA.A.S.03604 (Oct 2008)
	PA42-1000 with 5 blade MTV-27-1-E-C-F-R(G)/CFR()250-103 props. World's fastest conventional turbo prop again faster by up to 6 kts and sounds like a Jet with dramatically reduced outside and inside noise plus improved ground clearance. more information (pdf 69k) optional available with HiGlo Spinner	STC No. EASA.A.S.02480 (Dec 20, 2006)
	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 141k)	STC SA0786 (April 07, 1998)
	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 141k)	STC SA0626 (May 20, 1998)
	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	STC SA1301 (Dec. 10, 2002)
	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 130k)	STC EASA # 2004-9882 EMZ SA1403 (Sept. 27, 2004)
	Piper Aerostar PA-60-602P and PA-60-602P with Machen Conversion Inc. Induction Air Intercoolers 4-blade MTV-14-B-C-F/CF188-30d	STC EASA.A.S.00579 (Feb. 9, 2005)
	Piper PA-60-700P Lycoming (L)TIO-540-U2A 4-blade MTV-14-B-C-F/CF(L)188-30d more information (pdf 124k)	STC SA1369 (Feb. 5, 2004)