04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>4<strong>04</strong>5 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>126 REV 1 REVO LAKE 250 Installation of propeller- MTV-9-B/LD193-109<br />
or- MTV-9-B-C-R(M)/CRLD193-109<br />
02.12.2005<br />
10<strong>01</strong>4<strong>04</strong>6 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>128 REV. 1 CESSNA 208, 208B 1. Installation of the MTV-16-1-E-C-F- None Prior to installation of this modification it 12.<strong>04</strong>.2<strong>01</strong>1<br />
R(P)/CFR250-55 full feathering andreversible 4-<br />
must be determined thatthe<br />
blade constant speed propeller2. Extension of<br />
interrelationship between this modification<br />
Installation 1 on MTV-16-1-E-C-F-<br />
and any other previouslyinstalled<br />
R(P)/CFR250-55propellers equipped with fluid<br />
modification and/ or repair will introduce<br />
deice system.<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>4100 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>202 SOCATA TB 21 Installation of MTV-9-B/198-52 hydraulically<br />
controlled 3-blade constant speed propeller<br />
<strong>01</strong>.08.2005<br />
10<strong>01</strong>4107 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>212 MOONEY M20M Installation of propeller MTV-14-B/185-59b 02.11.2005<br />
10<strong>01</strong>4194 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>336 PITTS S-2C S-2B Installation of propeller MTV-9-B-C/C203-46 16.08.2006<br />
10<strong>01</strong>4203 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>354 AVIATION AIRCRAFT A-1<br />
AVIATION AIRCRAFT A-1A<br />
AVIATION AIRCRAFT A-1B<br />
Installation of propeller MTV-14-B/183-<br />
3<strong>01</strong>aTake-off- and max. Continuous-power:<br />
126 kw by 2500 min<br />
10<strong>01</strong>4238 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>402 REV. 2 1. DV20 & 2. DA20-A1 Extension of <strong>EASA</strong> STC<br />
<strong>EASA</strong>.A.S.<strong>01</strong>402Installation of the 2-blade<br />
MTV-21-A/170-05<br />
10<strong>01</strong>4239 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>403 CESSNA 182Q<br />
CESSNA 182R<br />
CESSNA F182-Q<br />
Installation of propeller MTV-9-D/203-52 This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>04</strong>.11.2005<br />
none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>04</strong>.11.2<strong>01</strong>0<br />
10<strong>01</strong>4240 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>4<strong>04</strong> DIAMOND DA-20-C1 Installation of Propeller MT 175 R 150-2Ca 14.03.2006<br />
10<strong>01</strong>4241 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.<strong>01</strong>406 1. CESSNA 182<br />
CESSNA 182A<br />
CESSNA 182B<br />
CESSNA 182C<br />
CESSNA 182D<br />
CESSNA 182E<br />
CESSNA 182F<br />
CESSNA 182G<br />
CESSNA 182H<br />
CESSNA 182J<br />
CESSNA 182K<br />
CESSNA 182L<br />
CESSNA 182M<br />
CESSNA 182N<br />
CESSNA 182P<br />
CESSNA F182-P<br />
Installation of propeller MTV-9D/203-52 08.06.2006<br />
10<strong>01</strong>4432 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.02480 PIPER PA-42-1000 Installation of propeller MTV-27-1-E-C-F-<br />
R(G)/CFRL250-103 (right),MTV-27-1-E-C-F-<br />
R(G)/CFR250-103 (left)<br />
-- 20.12.2006<br />
10<strong>01</strong>4441 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.02491 CIRRUS SR22 Installation of 3-blade MTV-9-D/198-52<br />
constant speed Propeller<br />
10<strong>01</strong>4445 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.02498 VULCANAIR P68<br />
VULCANAIR P68 B<br />
VULCANAIR P68 C<br />
VULCANAIR P68 C-TC<br />
VULCANAIR P68 OBSERVER<br />
VULCANAIR P68 OBSERVER 2<br />
VULCANAIR P68TC OBSERVER<br />
10<strong>01</strong>4491 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.02553 PIPER PA-34-200T<br />
PIPER PA-34-220T<br />
P.68 "Victor", P.68B "Victor", P.68C, P.68<br />
"Observer", P.68 "Observer 2":Installation of<br />
propeller MTV-12-B-C-F/CF183-59bP.68C-TC,<br />
P.68TC "Observer":Installation of propeller<br />
MTV-12-B-C-F/CF188-53<br />
Installation of Propeller MTV-12-D-C-<br />
F/CF(L)/188-53<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
18.11.2005<br />
10.07.2006<br />
-- 07.11.2006<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 337/<strong>462</strong><br />
13.03.2006
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