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 />
10030066 NAYAK AIRCRAFT SERVICE GMBH &<br />
ATR 72-1<strong>01</strong>/-2<strong>01</strong>/-102/-202 Installation of single HF-9000 Communication This STC may only be embodied into ATR72- After application of CRI H-0<strong>01</strong> Issue <strong>01</strong>, 18.05.2<strong>01</strong>0<br />
CO. K<br />
ATR 72-211/-212/-212A<br />
Transceiver System inATR72's as per Nayak's 1<strong>01</strong>/102/2<strong>01</strong>/202/211/212/212Aaircraft additional specific EWIS ICAStasks to<br />
Master Document List ATR72-NY-02155 previously modified for the installation of ATR- those for the original aircraft configuration<br />
Revision 4 dated 18thMay 2<strong>01</strong>0 or later <strong>EASA</strong> GIE Mod 02028"Fuselage-Provide basic has been definedfor this Nayak STC and<br />
approved revisions<br />
provisions for HF antenna strap insulator" they are detailed on Nayak's<br />
andMod 03138 "Communications-HF system MaintenanceProcedures ATR72-NYinstallatio<br />
02155-07 Revision 2, dated 18th<br />
10031264 NAYAK AIRCRAFT SERVICE GMBH &<br />
CO. K<br />
10033154 NAYAK AIRCRAFT SERVICE GMBH &<br />
CO. K<br />
10033946 NAYAK AIRCRAFT SERVICE GMBH &<br />
CO. K<br />
10033970 NAYAK AIRCRAFT SERVICE GMBH &<br />
CO. K<br />
10034483 NAYAK AIRCRAFT SERVICE GMBH &<br />
CO. K<br />
10034925 NAYAK AIRCRAFT SERVICE GMBH &<br />
CO. K<br />
10037575 NAYAK AIRCRAFT SERVICE GMBH &<br />
CO. K<br />
1. C90A,C90GT,C90GTI<br />
2. C90<br />
Installation of an Avidyne Traffic Advisory<br />
System TAS 600/610/620<br />
SA226-AT, SA226-T(B), SA226- Dual Installation of GNS 430 WAAS in<br />
TC<br />
SA226/227 Series<br />
SA227-AT<br />
SA227-TT, SA227-AC, SA227-DC<br />
SA26-T, SA26-AT, SA226-T,<br />
4<strong>01</strong>, 4<strong>01</strong>A, 4<strong>01</strong>B,<br />
402, 402A, 402B, 402C,<br />
411, 411A, 414, 414A,<br />
421, 421A, 421B, 421C, 425.<br />
REV. 2 4<strong>01</strong>, 4<strong>01</strong>A, 4<strong>01</strong>B,<br />
402, 402A, 402B, 402C,<br />
411, 411A, 414, 414A,<br />
421, 421A, 421B, 421C, 425<br />
Installation of a Traffic Advisory System<br />
Avidyne TAS610/620.<br />
Single installation of Garmin GNS 430<br />
(A)W/GNS 530 (A)W and optionalinstallation<br />
of Roll Steering Converter GDC31.<br />
560XL Installation of HID/LED LDG/REC/TAXI<br />
lightReplacement of existing conventional<br />
LDG/REC/TAXI lights by low powerHID/LED<br />
lights<br />
REV. 1 T303 Installation of1. Dual GPS/NAV/COMM Garmin<br />
GNS430/530(A)W2. E-HSI Sandel SN3308<br />
with Directional Gyro Century NSD360A3.<br />
Various other NAV/COMM related Avionic<br />
Components<br />
REV. 1 EMB-135BJ<br />
EMB-135ER, EMB-135LR<br />
EMB-145EP, EMB-145MP<br />
EMB-145ER, EMB-145LR<br />
EMB-145LU<br />
EMB-145MK, EMB-145EU<br />
Installation of HID Taxi/Landing light, inspection<br />
light on EMB-145aircraft.<br />
10<strong>01</strong>6258 NEW FLIGHT COOPERATION <strong>EASA</strong>.IM.A.S.02537 FAA STC SA4954NM CITATION 550-00<strong>01</strong> TO -0800 Gross Weight Increases based on Banson<br />
Aircraft Corp. STC.LBA STC Nr. 2<strong>04</strong>8, 05<br />
June1996;Spanish STC No. S325-I, 06 Febr.<br />
2003.<br />
10<strong>01</strong>5648 NEW SYSTEMS ENGINEERING <strong>EASA</strong>.IM.A.S.<strong>01</strong>622 FAA STC ST09384SC SAAB 340<br />
SAAB 340B<br />
Installation of a single Universal Avionics Flight<br />
Management System in SAAB SF340A and<br />
SAAB 340BFAA STC ST09384SC, Rev. 2<br />
none The installation of this modification by<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
disposal of the approvedappropriate<br />
documentation.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship b<br />
None Installation of 3rd dissimilar and<br />
independent COM system required<br />
froIFR operation Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
06.08.2<strong>01</strong>0<br />
21.12.2<strong>01</strong>0<br />
None A compatible Multi Function Display<br />
(MFD) must have been alreadyinstalled.<br />
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 wi<br />
21.02.2<strong>01</strong>1<br />
None An independent COMM or NAV/DME or 14.03.2<strong>01</strong>1<br />
ADF/DME must have been<br />
alreadyinstalled. Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repair wi<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 />
07.<strong>04</strong>.2<strong>01</strong>1<br />
None This STC consists of three blocks (see<br />
title) which may be installedindependently<br />
from each other. The components of the<br />
third block (seeEquipment List) may also<br />
be installed independently. The third<br />
block of this STC includes the installation<br />
of:Honeywell<br />
16.05.2<strong>01</strong>1<br />
Not Applicable 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 />
09.12.2<strong>01</strong>1<br />
19.11.2007<br />
None 19.<strong>04</strong>.2006<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 343/<strong>462</strong>
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