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>7290 MECAER AVIATION GROUP S.P.A. <strong>EASA</strong>.R.S.<strong>01</strong>545 REV. 1 AB139/ AW139 AW139 VIP 221 Interiors, P/N 6AB1AD<strong>01</strong>3- The VIP 221 interiors can only be installed on Prior to installation of this modification it 09.06.2<strong>01</strong>0<br />
0<strong>01</strong>. This STC supersedes <strong>EASA</strong> STC AB/AW 139 helicoptersequipped with Agusta must be determined thatthe<br />
<strong>EASA</strong>.R.S.<strong>01</strong>545.<br />
provision P/N 4G2520F0<strong>04</strong>11.<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 />
10030095 MECAER AVIATION GROUP S.P.A. AB139 / AW139 AW139 VIP 305 INTERIORSP/N 6AB1AD<strong>01</strong>5- As per the approved Rotorcraft Flight Manual<br />
0<strong>01</strong><br />
Supplement quoted above<br />
10030280 MECAER AVIATION GROUP S.P.A. <strong>EASA</strong>.R.S.0<strong>04</strong>84 REV. 1 AB139/ AW139 Cabin Configuration VIP-4 P/N 6-A02<strong>01</strong>KI<strong>01</strong><strong>01</strong>- Approval of this change in type design applies<br />
003. This STC supersedes <strong>EASA</strong> STC only to those AB 139rotorcraft previously<br />
<strong>EASA</strong>.R.S.0<strong>04</strong>84.<br />
equipped with <strong>EASA</strong> approved installation of<br />
AgustaKit Vip Cabin interior (Namibia) P/N<br />
3G2520F0<strong>04</strong>11.<br />
Prior to installation of this modification it 21.05.2<strong>01</strong>0<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 />
Prior to installation of this modification the<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 />
10030281 MECAER AVIATION GROUP S.P.A. <strong>EASA</strong>.R.S.0<strong>04</strong>85 REV. 1 AB139/ AW139<br />
product.<br />
Cabin Configuration VIP-3 P/N 6-A02<strong>01</strong>KI<strong>01</strong><strong>01</strong>- Approval of this change in type design applies Prior to installation of this modification the 09.06.2<strong>01</strong>0<br />
0<strong>01</strong>. This STC supersedes <strong>EASA</strong> STC only to those AB 139rotorcraft previously installer must determinethat the<br />
<strong>EASA</strong>.R.S.0<strong>04</strong>85.<br />
equipped with <strong>EASA</strong> approved installation of interrelationship between this modification<br />
AgustaKit Vip Cabin interior (Namibia) P/N and any otherpreviously installed<br />
3G2520F0<strong>04</strong>11.<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.<br />
10030339 MECAER AVIATION GROUP S.P.A. <strong>EASA</strong>.R.S.0<strong>04</strong>86 REV. 1 AB139/ AW139 Cabin Configuration VIP-2 P/N 6-A03<strong>01</strong>KI<strong>01</strong><strong>01</strong>- Approval of this change in type design applies Prior to installation of this modification it 09.06.2<strong>01</strong>0<br />
003. This STC supersedes <strong>EASA</strong> STC only to those AB 139rotorcraft previously must be determined thatthe<br />
<strong>EASA</strong>.R.S.0<strong>04</strong>86.<br />
equipped with <strong>EASA</strong> approved installation of interrelationship between this modification<br />
AgustaKit Vip Cabin interior (UAE) P/N and any other previouslyinstalled<br />
3G2520F00511.<br />
modification and/or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10030340 MECAER AVIATION GROUP S.P.A. <strong>EASA</strong>.R.S.0<strong>04</strong>87 REV. 1 AB139/ AW139 Cabin Configuration VIP-1 P/N 6-A03<strong>01</strong>KI<strong>01</strong><strong>01</strong>- Approval of this change in type design applies<br />
0<strong>01</strong>. This STC supersedes <strong>EASA</strong> STC only to those AB 139rotorcraft previously<br />
<strong>EASA</strong>.R.S.0<strong>04</strong>87.<br />
equipped with <strong>EASA</strong> approved installation of<br />
AgustaKit Vip Cabin interior (UAE) P/N<br />
3G2520F00511.<br />
10030342 MECAER AVIATION GROUP S.P.A. <strong>EASA</strong>.R.S.<strong>01</strong>226 REV. 2 AB139/ AW139 FWD Bulkhead P/N 6AB1AD005-0<strong>01</strong><br />
Installation. This STC supersedes <strong>EASA</strong> STC<br />
<strong>EASA</strong>.R.S.<strong>01</strong>226.<br />
10030371 MECAER AVIATION GROUP S.P.A. <strong>EASA</strong>.R.S.<strong>01</strong>534 REV. 1 AB139/ AW139 AW139 "Liners" Silens P/N 6AB1AD<strong>01</strong>0-0<strong>01</strong>.<br />
This STC supersedes <strong>EASA</strong> STC<br />
<strong>EASA</strong>.R.S.<strong>01</strong>534.<br />
10031938 MECAER AVIATION GROUP S.P.A. AW139 / AB139 IFEEL Entertainment System Installation P/N<br />
6AB1AD<strong>01</strong>6-0<strong>01</strong><br />
09.06.2<strong>01</strong>0<br />
Prior to installation of this modification it 09.06.2<strong>01</strong>0<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 />
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 />
09.06.2<strong>01</strong>0<br />
This STC requires the installation of the Kit Prior to installation of this modification it 09.06.2<strong>01</strong>0<br />
Hinged Passengers DoorsP/N 4G5212F0<strong>01</strong>11. 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 />
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 />
23.09.2<strong>01</strong>0<br />
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