04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<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>6389 SIERRACIN/SYLMAR <strong>EASA</strong>.IM.A.S.02718 FAA STC ST<strong>01</strong>840NY BOMBARDIER DHC-8-100 Installation of Sierracin/Sylmar Windshield Prior to installation of this modification the<br />
14.08.2008<br />
SERIES<br />
Assembly P/N 802600-11/-12, Ref.: FAA STC installer must determine that the<br />
BOMBARDIER DHC-8-200 ST<strong>01</strong>840NY.<br />
interrelationship between this modification and<br />
SERIES<br />
any other previously installed modification will<br />
BOMBARDIER DHC-8-300<br />
introduce no adverse effect upon the<br />
SERIES<br />
airworthiness of the product. The install<br />
10<strong>01</strong>6390 SIERRACIN/SYLMAR <strong>EASA</strong>.IM.A.S.02719 REV. 1 FAA STC ST<strong>01</strong>839NY BOMBARDIER DHC-8-100<br />
SERIES<br />
BOMBARDIER DHC-8-200<br />
SERIES<br />
BOMBARDIER DHC-8-300<br />
SERIES<br />
BOMBARDIER DHC-8-400<br />
SERIES<br />
10<strong>01</strong>6716 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong><strong>01</strong>0 FAA STC SR00836NY SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6717 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong><strong>01</strong>1 FAA STC SR<strong>01</strong>131NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6718 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong><strong>01</strong>2 FAA STC SR<strong>01</strong>593NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6733 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>057 FAA STC SR00033NY SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6734 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>058 SR<strong>01</strong>596NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6735 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>059 FAA STC SR<strong>01</strong>132NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6736 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>060 FAA STC SR<strong>01</strong>608NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
Installation of Sierracin/Sylmar Windshield<br />
Assembly P/N 802600-09/-10, Ref. FAA STC<br />
ST<strong>01</strong>839NY<br />
Installation of Cargo Compartment Baggage<br />
Liner.<br />
Installation of Luminescent Systems Helicopter<br />
Emergency Egress System (HEELS)<br />
Installation of Keystone Helicopter Utility<br />
Interior Panels<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
1. Keystone Helicopter Corp. Maintenance<br />
Manual S-76A, B&C Baggage Liner, Report<br />
No MM00081 dated February 17, 1997, as<br />
required.2. This STC is approved only for the<br />
product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph<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 />
1. Keystone Helicopter Instructions for<br />
Continued Airworthiness Report No IC00735<br />
Rev_dated June 11, 20<strong>04</strong> or later approved<br />
revision. 2. It is a prerequisite to have<br />
previously approved brackets installed for each<br />
individual panel installation as denoted i<br />
Installation of Grease Fittings. 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 />
Universal Avionics Systems Corporation UNS-<br />
1 Multi-Mission Management Systems (MMMS)<br />
with SCN 9<strong>01</strong>.X Software<br />
Honeywell KTA870 Traffic Advisory (TAS)<br />
displayes on a Honeywell KD550<br />
Multifunctional Display (MFD)Ass.:Report<br />
ER00566 Certification PlanRFM Supplement<br />
FM00566<br />
Installation of Aircell ST 3100 Satellite<br />
Telephone System<br />
10<strong>01</strong>6753 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>082 SR00688NY SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6773 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>108 FAA STC SR<strong>01</strong>958NY-D SIKORSKY S-76C Installation of Rockwell Collins TDR-94D<br />
Transponder with Elementary Surveillance<br />
10<strong>01</strong>6774 SIKORSKY GLOBAL HELICOPTERS Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>109 FAA STC SR<strong>01</strong>960NY-D SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
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 />
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 />
15.08.2008<br />
11.<strong>04</strong>.2005<br />
19.<strong>04</strong>.2005<br />
22.<strong>04</strong>.2005<br />
22.<strong>04</strong>.2006<br />
06.03.2006<br />
18.11.2005<br />
23.02.2006<br />
Installation of Medical Interior 12.05.2006<br />
Installation of baggage access panel (ground<br />
use only), forward facing seat, seat pan and<br />
wet floor.<br />
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 />
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>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 4<strong>04</strong>/<strong>462</strong><br />
13.03.2006<br />
13.03.2006
Change language