04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10038450 MITSUBISHI HEAVY INDUSTRIES<br />
FAA STC SA<strong>01</strong>594SE 1- MU-2B-20, -25, -26<br />
Fabrication and Installation of Stretched Acrylic None. The installer must determine whether this 17.02.2<strong>01</strong>2<br />
AMERICA<br />
2- MU-2B-30, -35, -36<br />
Cabin Windows inaccordance with FAA STC<br />
design change is compatiblewith<br />
3- MU-2B-20, -25, -26<br />
SA<strong>01</strong>594SE.<br />
previously approved modifications.If the<br />
3- MU-2B-30, -35, -36<br />
holder agrees to permit another person to<br />
4- MU-2B-25, -26, -26A<br />
use this certificate toalter a product, the<br />
4- MU-2B-35, -36, -36A,<br />
holder must give the other person written<br />
4- MU-2B-40, -60<br />
evidenceof th<br />
10<strong>01</strong>4115 MONARCH AIRCRAFT ENGINEERING<br />
LTD<br />
<strong>EASA</strong>.A.S.<strong>01</strong>221 BOEING 737-522 Installation of Honeywell EGPWS 06.<strong>04</strong>.2005<br />
10<strong>01</strong>4116 MONARCH AIRCRAFT ENGINEERING<br />
LTD<br />
<strong>EASA</strong>.A.S.<strong>01</strong>222 BOEING 737-522 Introduction of 131 Passenger Configuration <strong>01</strong>.<strong>04</strong>.2005<br />
10<strong>01</strong>4155 MONARCH AIRCRAFT ENGINEERING <strong>EASA</strong>.A.S.<strong>01</strong>277 BOEING 767-300 Monarch Aircraft Engineering Modification Subject AFM supplement is associated to<br />
29.06.2005<br />
LTD<br />
MON/767/258/2995 Installation of a 38 Dassault Aviation Mod M1632: "Installation<br />
Premium Class Cabin<br />
d'un hublot inférieur avec volet de<br />
protection",applicable to F20 GF SN 397 only<br />
10<strong>01</strong>3959 MOTORFLUG BADEN-BADEN GmbH <strong>EASA</strong>.A.S.00610 SOCATA TB 20 Installation of Transponder Garmin GTX 330 -<br />
Mode S<br />
10028137 MOTORFLUG BADEN-BADEN GmbH P-<strong>EASA</strong>.A.S.03954 REV. 2 P.180 AVANTI II Additional installation of Collins BCU-4000 and<br />
CMU-4000 to flightinspection system.<br />
10028394 MOTORFLUG BADEN-BADEN GmbH PIAGGIO P.180 AVANTI II Installation of TCAS top & bottom antennas.<br />
Installation of TCASprocessor in nose section.<br />
Interface to existing transponder and<br />
avionicsystem.<br />
1. 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>01</strong>.03.2005<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>01</strong>.10.2<strong>01</strong>2<br />
None Prior to installation of this modification the <strong>04</strong>.<strong>01</strong>.2<strong>01</strong>0<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.The installatio<br />
10033883 MOTORFLUG BADEN-BADEN GmbH 407 Installation of Antenna Mount on Tailboom 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 />
16.02.2<strong>01</strong>1<br />
100366<strong>04</strong> MOTORFLUG BADEN-BADEN GmbH REV. 1 228-212 Installation of Mission Equipment for Maritime<br />
Surveillance.<br />
10<strong>04</strong>1143 MOTORFLUG BADEN-BADEN GmbH 2<strong>04</strong>B Exchange of engine torque and temperature<br />
indicator.<br />
10<strong>01</strong>6537 MPM INC. <strong>EASA</strong>.IM.A.S.02914 FAA STC SA<strong>01</strong>033WI Replacement of original main landing gear 1. The attached AML is applicable only on<br />
doors with one piece monolithic machined gear aircraft serial numbers called out in MPM Inc<br />
doors.<br />
Drawing No AML-LG-DR002-1, -2, -3 and -4for<br />
installation and applicability.2. Prior to<br />
installation of this modification the installer must<br />
determine that the int<br />
10<strong>01</strong>6538 MPM INC. <strong>EASA</strong>.IM.A.S.02915 FAA STC SA00902WI Replacement of original main landing gear<br />
doors with monolithic machined gear doors.<br />
None. This installation is only applicable to<br />
Dornier 228-212 with flight deckupgrade<br />
according to RUAG CN-228-247.The<br />
following RUAG Changes/Options must<br />
have been already installed:- Mechanical<br />
mounting provisions for SLAR Antenna<br />
according,CN-228-214m. - Mech<br />
11.10.2<strong>01</strong>1<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 />
23.08.2<strong>01</strong>2<br />
1. The attached AML is applicable only on<br />
aircraft serial numbers called out in MPM Inc<br />
Drawing No. AML-LG-DR0<strong>01</strong>1. The attached<br />
AML is applicable only on aircraft serial<br />
numbers called out in MPM Inc Drawing No.<br />
AML-LG-DR0<strong>01</strong>.2. Prior to installation<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 336/<strong>462</strong><br />
05.06.2008<br />
10.06.2008
Change language