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>7203 FISCHER + ENTWICKLUNGEN <strong>EASA</strong>.R.S.<strong>01</strong>352 BELL 427 Installation of floor mounted F+E Medical Seats<br />
230/305 into Bell 427 cabin by use of<br />
installation racks attached to forward and aft<br />
cabin bulkhead fittings<br />
20.07.2007<br />
10<strong>01</strong>5484 FLIGHT ENVIRONMENTS INC <strong>EASA</strong>.IM.A.S.<strong>01</strong>244 FAA STC SA<strong>01</strong>318LA BEECH 390 Installation of thermal/accoustic insulation kit 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 />
26.07.2005<br />
10<strong>01</strong>5709 FLIGHT STRUCTURES, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>702 FAA STC ST02944AT B777-200, B777-300 Installation of Cabin Wireless Local Area Airworthines Limitations Section of the<br />
20.07.2006<br />
Network (CWLAN) Distribution System Instruction for Continuous Airworthiness,<br />
document numbers F44-0246, revision A,<br />
dated 20thOctober 20<strong>04</strong> or R44-<strong>04</strong>06, revision<br />
IR, dated 23rd June 2005 or later FAA<br />
approved revisions<br />
10<strong>01</strong>5719 FLIGHT STRUCTURES, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>717 FAA STC ST<strong>01</strong>729SE B747-400 Business Class Seat Installation Boeing Service Bulletin 747-25-3420 dated<br />
June 13 2006 must be installed concurrently<br />
with this STC.<br />
17.<strong>01</strong>.2007<br />
10<strong>01</strong>5720 FLIGHT STRUCTURES, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>719 REV. 3 FAA STC NO. ST<strong>01</strong>849SE 777-200 Business Class Seat Installation Boeing Structural Compliance summary Prior to installation of this modification it 02.02.2<strong>01</strong>2<br />
Report Document DLR-36718 revisionNew must be determined thatthe<br />
dated 17 March 2008 must be accomplished interrelationship between this modification<br />
concurrently with this STCBoeing Structural and any other previouslyinstalled<br />
Compliance Summary Report Document DLR- modification and/ or repair will introduce<br />
36718 RevisionNew dated 17 March 2008 no adverse effectupon the airworthiness<br />
must be accomplishe<br />
of the product.<br />
10<strong>01</strong>6319 FLIGHT STRUCTURES, Inc. <strong>EASA</strong>.IM.A.S.02627 REV. 3 FAA STC ST<strong>01</strong>950SE B777-200 Remove EWIS limitation for <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.IM.A.S.02627 Rev 1 - Door 1Overhead<br />
Flight Crew Rest Installation<br />
The Boeing Service Bulletin 777-25-<strong>04</strong>29<br />
dated 15 October 2008 must beaccomplished<br />
concurrently with this STC for the serial<br />
numbers listed onthe FSI top Collector<br />
A700000-0<strong>01</strong> revision C dated 8 December<br />
2008The Main deck seat arrangement must be<br />
installed<br />
10<strong>01</strong>6564 FLIGHT STRUCTURES, Inc. <strong>EASA</strong>.IM.A.S.02955 FAA STC ST00386SE BOEING 747-200 This design change relocates the E/E Bay This STC can only be installed in aircraft with<br />
Acces Hatch on the main deck floor and FAA STC SA2725CE-D or STC ST00255WI-D<br />
Installs Gari o Handling System Provisions for a or STC ST00252WI-D or STC ST00214SE<br />
30pallet main deck cargo configuration per<br />
Flight Structures, Inc.<br />
installed.<br />
10<strong>01</strong>6610 FLIGHT STRUCTURES, Inc. <strong>EASA</strong>.IM.A.S.03030 REV. 2 FAA STC ST020<strong>04</strong>SE B777-200 Remove EWIS limitation for <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>. IM.A.S.03030 - Door 3Overhead<br />
Attendant Rest Installation<br />
10029094 FLIGHT STRUCTURES, Inc. P-<br />
<strong>EASA</strong>.IM.A.S.02978<br />
10029964 FLIGHT STRUCTURES, Inc. P-<br />
<strong>EASA</strong>.IM.A.S.03<strong>04</strong>5<br />
10031815 FLIGHT STRUCTURES, Inc. P-<br />
<strong>EASA</strong>.IM.A.S.03215<br />
REV. 1 FAA STC ST02051SE B777-200 Remove EWIS limitation for <strong>EASA</strong> STC No.<br />
10029094 - First Class SeatInstallation<br />
REV. 1 FAA STC ST02060SE B747-400 Amendment of STC 10029964 in order to<br />
remove EWIS Limitations and updatethe MDL<br />
reference<br />
FAA STC ST02038SE A330-300 Installation of an Interior Reconfiguration in<br />
A330-300 Series aircraft<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 will introduce<br />
no adverse effectupon the airworthiness<br />
of the product<br />
07.10.2<strong>01</strong>0<br />
18.09.2008<br />
The Main deck seating arrangement must be Prior to installation of this modification it 07.10.2<strong>01</strong>0<br />
installed in accordance withBritish Airways must be determined thatthe<br />
drawing 3-302-342 revision 10 dated 12 interrelationship between this modification<br />
February 2009FSI STC 10<strong>01</strong>6319 rev. 2 (FAA and any other previouslyinstalled<br />
STC number ST<strong>01</strong>950SE) for the FSI Door modification and/ or repair will introduce<br />
1Overhead Flight Crew Rest Installation no adverse effectupon the airworthiness<br />
(OFCR) mus<br />
of the product<br />
Concurrent installation of <strong>EASA</strong> STC No.<br />
10029095 (<strong>EASA</strong> Project No.P-<br />
<strong>EASA</strong>.IM.A.S.03<strong>04</strong>3) is requiredConcurrent<br />
installation of <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>797 is required<br />
Concurrent Installation of <strong>EASA</strong> STC No.<br />
10029975 is requiredConcurrent installation of<br />
FAA STC ST00720LA (<strong>EASA</strong> approved<br />
undergrandfather rights by CAA Airworthiness<br />
Approval Note No. 26656 dated 8March 1999)<br />
is required<br />
Prior to installation of this modification it <strong>04</strong>.10.2<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 it <strong>04</strong>.10.2<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 />
Not applicable Concurrent installation of Delta<br />
Engineering Supplemental<br />
TypeCertificate <strong>EASA</strong> STC 10031836 is<br />
required Concurrent installation of<br />
AmSafe, Inc. Supplemental Type<br />
Certificate<strong>EASA</strong> STC 10031808 is<br />
required Prior to installation of this<br />
modification it must be<br />
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