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 />
10027008 MT-PROPELLER ENTWICKLUNG GmbH P-<strong>EASA</strong>.A.S.02941 PA-46-310P (MALIBU)<br />
Installation of 4 blade MTV-16-1-E-C-F- Prerequisite for the installation of this STC is None. 28.08.2009<br />
PA-46-350P (MALIBU MIRAGE) R(P)/CFR206-58a on airplanePA-46-310P and the installation of aPratt & Whitney PT6A-21, -<br />
PA-46-350P modified with Pratt & Whitney<br />
PT6A-21, -34 or-35 engine per FAA STC<br />
ST00541SE.<br />
34 or -35 engine per FAA STC ST00541SE.<br />
10027439 MT-PROPELLER ENTWICKLUNG GmbH P-<strong>EASA</strong>.A.S.03889 BAE JETSTREAM 3100, 3200 Installation of 5-blade MTV-27-1-E-C-F- None The installation of this modification by 30.09.2009<br />
R(G)/CFRL250-103() propellers<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation. Prior to<br />
installation of this modification it must be<br />
determined thatthe interr<br />
10028096 MT-PROPELLER ENTWICKLUNG GmbH P-<strong>EASA</strong>.A.S.039<strong>01</strong> MX-7-180 B, MX-7-180 C, Installation of a 2-blade MTV-15-B/203-58 None None <strong>01</strong>.12.2009<br />
MX-7-180, MX-7-180 A,<br />
propeller on Maule M-4 ModelsMX-7-180, MX-<br />
MXT-7-180, MXT-7-180A 7-180A, MX-7-180B, MX-7-180C, MXT-7-180,<br />
and MX-7-180A<br />
10029676 MT-PROPELLER ENTWICKLUNG GmbH 206H, T206H Installation of 5-blade MTV-5-1-D-C-F- Prior to installation of this STC modification None 12.<strong>04</strong>.2<strong>01</strong>0<br />
R(A)/CFR210-56 propeller on CessnaModel i.a.w. <strong>EASA</strong> STC 10027209(Soloy Mark II<br />
206H, T206H equipped with Rolls-Royce 250-<br />
B17F/2 series engine perFAA STC No.<br />
SA<strong>01</strong>878SE<br />
Turbine Conversion) is required<br />
10030966 MT-PROPELLER ENTWICKLUNG GmbH <strong>EASA</strong>.A.S.00749 REV. 1 CESSNA U 206G, TU 206G Installation of Propeller MTV-5-1-E-C-F- 1. This STC is applicable to Cessna U 206G, None 19.07.2<strong>01</strong>0<br />
R(M)/CFR220-54 orMTV-5-1-E-C-F/CF220-54 TU 206G both equipped withR/R Allison 250-<br />
C20S (Soloy Turbine PAC) in accordance with<br />
LBA EMZ(STC) 0082/673a only. 2.This STC is<br />
approved only for the product configuration as<br />
defined inthe approved design data r<br />
10031167 MT-PROPELLER ENTWICKLUNG GmbH PC-6/B1-H2, PC-6/B2-H2<br />
PC-6/B2-H4<br />
Installation of 4-blade MTV-16-1-E-C-F-<br />
R(P)/CFR240-55() propeller onPilatus PC-6/B1-<br />
H2, PC-6/B2-H2, PC-6/B2-H4<br />
10032680 MT-PROPELLER ENTWICKLUNG GmbH REV. 1 PA-31P Installation of two 4-blade MTV-16-1-E-C-<br />
F/CFL225-37a propellers onPiper PA-<br />
31PChange of Certification Basis.<br />
10033038 MT-PROPELLER ENTWICKLUNG GmbH TBM 700 A, TBM 700 B,<br />
TBM 700 C1, TBM 700 C2,<br />
TBM 700 N<br />
10034434 MT-PROPELLER ENTWICKLUNG GmbH LBA STC (EMZ)<br />
SA0786 ISSUE 3<br />
10034435 MT-PROPELLER ENTWICKLUNG GmbH LBA STC (EMZ)<br />
SA0626 ISSUE 4<br />
Installation of 5-blade MTV-27-1-E-C-F-<br />
R(P)/CFR225-55f propeller<br />
REV. 2 PA-46-310P 1) Installation of MTV-14-D/190-17 on PA-46-<br />
310P2) Installation of MTV-14-D/195-30a on<br />
PA-46-310P3) Installation of MTV-14-D/195-<br />
30a on PA-46-310P equipped with TCMTSIO-<br />
550-C i.a.w. FAA STC SA00380AT4)<br />
Installation of MTV-14-D/195-30b on PA-46-<br />
310P5) Insta<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 />
29.07.2<strong>01</strong>0<br />
According limitation section of AFM-S and<br />
POH-S.<br />
Prior to installation of this modification it 10.08.2<strong>01</strong>1<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 />
according limitation section of AFM-S 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 productIf the h<br />
15.12.2<strong>01</strong>0<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 />
25.05.2<strong>01</strong>1<br />
REV. 1 PA-46-350P, PA-46R-350T 1) Installation of MTV-14-B/190-172)<br />
None Prior to installation of this modification it 07.<strong>04</strong>.2<strong>01</strong>1<br />
Installation of MTV-14-B/195-30a3) Installation<br />
must be determined thatthe<br />
of MTV-14-B/195-30b For installation 3 optional<br />
interrelationship between this modification<br />
reduction of take-off propeller speed to2400<br />
and any other previouslyinstalled<br />
rpm is included<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
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