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 />
10036196 MT-PROPELLER ENTWICKLUNG GmbH 200,200C,200CT,200T,A200 (12A) Installation of 5 blade MTV-27-1-E-C-F- none Prior to installation of this modification it 19.08.2<strong>01</strong>1<br />
A200 (C-12C),A200CT (C-12D) R(P)/CFR225-55f propellers<br />
must be determined thatthe<br />
A200CT (C-12F),A200CT (RC-<br />
interrelationship between this modification<br />
12D)<br />
and any other previouslyinstalled<br />
A200CT (FWC-12D)<br />
modification and/ or repair will introduce<br />
A200CT (RC-12G)<br />
no adverse effectupon the airworthiness<br />
A200CT (RC-12H),B200,B200C<br />
B200CGT,B200CT,B200GT,B200<br />
T<br />
of the product.<br />
10038174 MT-PROPELLER ENTWICKLUNG GmbH REV. 1 PA-31T, PA-31T1, PA-31T2 Installation of 5-blade MTV-27-1-E-C-F-<br />
PA-31T*, PA-31T1*, PA-31T2*<br />
-135A ENGINES PER FAA STC<br />
(*)MODIFIED WITH PT6A-135 OR<br />
SA00863SE<br />
R(P)/CFR210-58d propellers<br />
10038512 MT-PROPELLER ENTWICKLUNG GmbH REV. 1 CESSNA 425 Installation of 5-blade MTV-27-1-E-C-F-<br />
R(P)/CFR210-58d propellers.Cessna 425<br />
aircraft and models modified by <strong>EASA</strong> STC<br />
<strong>EASA</strong>.IM.A.02944 (FAASA5786SW) to install<br />
PT6A-135 (A) engine(s).<br />
10038566 MT-PROPELLER ENTWICKLUNG GmbH REV. 1 SR22, SR22T Installation of 4-blade MTV-14-D/195-30b<br />
propellers.<br />
10038720 MT-PROPELLER ENTWICKLUNG GmbH REV. 1 LBA STC SA 1063 P210N, P210R<br />
T210M, T210N, T210R<br />
This <strong>EASA</strong> STC is a revision of LBA SSTC<br />
(EMZ) SA1063, dated 21.09.1999.Installation<br />
of Propeller MTV-14-D/195-30b is included in<br />
the scope ofthe STC in addition to the already<br />
approved -30a blades.<br />
10039107 MT-PROPELLER ENTWICKLUNG GmbH TAIFUN 17 E & E II Installation of a 2-blade MTV-1-A/L165-06<br />
propeller on powered sailpnaeTaifun 17 E and<br />
Taifun E II with Limbach L2400 EB1.AB or<br />
L2400 EF1/DF1engine<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>01</strong>.02.2<strong>01</strong>2<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 />
02.03.2<strong>01</strong>2<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 />
02.03.2<strong>01</strong>2<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 />
15.03.2<strong>01</strong>2<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 />
10.<strong>04</strong>.2<strong>01</strong>2<br />
10039667 MT-PROPELLER ENTWICKLUNG GmbH CESSNA 208, 208B Installation of 5-blade MT-Propeller ModelMTV- According limitation section of AFM-S Prior to installation of this modification it 16.05.2<strong>01</strong>2<br />
27-1-E-C-F-R(P)/CFR245-55a<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.If the<br />
10<strong>04</strong>2832 MT-PROPELLER ENTWICKLUNG GmbH M-6-235, M-7-235, M-7-235B<br />
MX-7-235, MT-7-235<br />
Installation of 3-blade MT-Propeller Model MTV- according limitation section of AFM-S Prior to installation of this modification it 20.12.2<strong>01</strong>2<br />
9-B/198-52<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.If the<br />
10<strong>04</strong>2833 MT-PROPELLER ENTWICKLUNG GmbH M20R, M20S Installation of 4-blade MT-Propeller Model MTV- according limitation section of AFM-S Prior to installation of this modification it 20.12.2<strong>01</strong>2<br />
14-D/188-30b<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.If the<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 340/<strong>462</strong>
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