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 />
10034098 C.A. FLOR FLORDELIS FAA STC ST<strong>01</strong>786LA B737-100, -200, -200C SERIES Upgrade Flight Data Recorder System Not Applicable Prior to installation of this modification it 08.03.2<strong>01</strong>1<br />
B737-300, -400, -500 SERIES Parameters<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 />
10<strong>01</strong>7158 CALEDONIAN AIRBORNE SYSTEMS<br />
LTD<br />
10<strong>01</strong>7222 CALEDONIAN AIRBORNE SYSTEMS<br />
LTD<br />
10<strong>01</strong>7223 CALEDONIAN AIRBORNE SYSTEMS<br />
LTD<br />
10035678 CALEDONIAN AIRBORNE SYSTEMS<br />
LTD<br />
10034473 CALIFORNIA SHOCK TRAUMA AIR<br />
RESCUE<br />
<strong>EASA</strong>.R.S.<strong>01</strong>266 SIKORSKY S-76 AF-ADELT improved installation on S-76 STC requires minor change F<strong>01</strong>2/208/0<strong>01</strong> to<br />
be incorporated.<br />
25.<strong>01</strong>.2007<br />
<strong>EASA</strong>.R.S.<strong>01</strong>386 REV. 2 AGUSTA-BELL 212 & 412 Installation of CAS CPT 900 ELT. None Prior to installation of this modification the 21.<strong>04</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 installati<br />
<strong>EASA</strong>.R.S.<strong>01</strong>388 REV. 2 BELL 212, BELL 412 Installation of CAS CPT 900 ELT None Prior to installation of this modification the 21.<strong>04</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 installati<br />
JETSTREAM 4100 Installation of Role Equipment for Maritime Serial numbers 41022 and 41025 only. Prior to installation of this modification it 11.07.2<strong>01</strong>1<br />
Patrol Training<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 />
FAA STC SR02160LA BO 105 LS A-3 Engine Upgrade:Removal of two (2) Rolls-<br />
Royce engine models 250-C28C and installing<br />
two(2) Rolls-Royce engine models 250-C30P<br />
in accordance with FAA STCSR02160LA,<br />
dated March 11, 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 />
11.<strong>04</strong>.2<strong>01</strong>1<br />
10<strong>01</strong>5309 CAMERON BALLOONS LIMITED <strong>EASA</strong>.BA.S.<strong>01</strong>0<strong>01</strong> GEFA AS 105 GD (HOT AIR<br />
AIRSHI<br />
Introduction of Liquid Pilot Lights. None. 30.<strong>04</strong>.2007<br />
10<strong>01</strong>6193 CANARD AEROSPACE CORPORATION <strong>EASA</strong>.IM.A.S.02430 FAA STC ST<strong>01</strong>106CH BOEING 747-100<br />
Installation of Digital Flight Data Recorder This STC is approved only for the product<br />
29.10.2007<br />
BOEING 747-100B SUD<br />
Expanded Parameters in accordance with configuration as defined in the approved design<br />
BOEING 747-200B<br />
Canard Aerospace Corporation Document data. Compatibility with other aircraft/engine<br />
BOEING 747-200C<br />
Control Drawing No. 30<strong>01</strong>0, Rev. G. dated 6 configurations shall be determined by the<br />
BOEING 747-200F<br />
October 2003, or later FAA approved revisions, installer.<br />
BOEING 747-300<br />
BOEING 747-SP<br />
BOEING 747-SR<br />
FAA STC number ST<strong>01</strong>106CH.<br />
10<strong>01</strong>6546 CANARD AEROSPACE CORPORATION <strong>EASA</strong>.IM.A.S.02925 FAA STC ST<strong>01</strong>117CH BOEING 747-100<br />
Option 1: Installation of Honeywell Classic 1. Prior to installation of this modification the<br />
12.11.2008<br />
BOEING 747-100B SUD<br />
Navigator system in accordance with Canard installer must determine that the<br />
BOEING 747-200<br />
Aerospace Corporation Control Drawing Nr. interrelationship between this modification and<br />
BOEING 747-200C<br />
30<strong>01</strong>1, Rev. NC, dated November 25, 2002, any other previously installed modification will<br />
BOEING 747-200F<br />
Appendix A, or later FAA approved<br />
introduce no adverse effect upon the<br />
BOEING 747-300<br />
revision.Option 2: Installation of a CMA-900 airworthiness of the product. The i<br />
BOEING 747-SP<br />
BOEING 747-SR<br />
Flight<br />
10028374 CANARD AEROSPACE CORPORATION P-<br />
FAA STC ST<strong>01</strong>331CH DHC-8-2<strong>01</strong>, -202 Installation of Honeywell Mark VII Enhanced Electronic Flight Information Systems (EFIS) The STC holder shall provide by 7th June 23.12.2009<br />
<strong>EASA</strong>.IM.A.S.03246<br />
Ground Proximity WarningSystem to replace symbol generator upgradedto Part Number 2<strong>01</strong>0 Instructions for<br />
existing Mark II Ground Proximity Warning (PIN) 70<strong>04</strong>544.314 in accordance with ContinuedAirworthiness on Electrical<br />
SystemFAA STC No ST<strong>01</strong>331CH, reissued 21 Honeywell ServiceBulletin (SB) 70<strong>04</strong>544.34-48 Wiring Interconnection System - EWIS<br />
May 2009<br />
(modification BC) is required prior to, ICA -in accordance with Special<br />
orconcurrent with, accomplishment of this Condition H-<strong>01</strong> "Enhanced<br />
modific<br />
AirworthinessProgramme for Aeroplane<br />
System - ICA on EWIS" Pri<br />
10<strong>01</strong>4684 CARGOLUX AIRLINES INTERNATIONAL <strong>EASA</strong>.A.S.02847 BOEING 747-400 SERIES Installation of an Artex B406-4 Automatic Fixed<br />
Emergency Locator Transmitter on B747-400F<br />
in accordance with Cargolux Service Bulletin<br />
CLX-SB-747-23-0<strong>01</strong> and Master Drawing list<br />
CLX-STC-06-<strong>01</strong>.<br />
14.03.2007<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 151/<strong>462</strong>
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