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 />
10036542 B/E AEROSPACE, Inc. FAA STC ST02876CH B777-200, B777-200LR<br />
Installation of B/E Aerospace, Inc., Vacuum None Prior to installation of this modification it 19.09.2<strong>01</strong>1<br />
B777-300, B777-300ER<br />
Toilet Assembly Retrofit Kit<br />
must be determined thatthe<br />
B777F<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 />
10036558 B/E AEROSPACE, Inc. FAA STC ST02876CH B737-600/700/800/900 Installation of Vacuum Toilet Assembly Retrofit<br />
Kit P/N 4100390-003.<br />
10036659 B/E AEROSPACE, Inc. FAA STC ST02876CH B747-400<br />
B747-400F<br />
Installation of Vacuum Toilet Assembly Retrofit<br />
Kit P/N 4100390-003Validation FAA STC<br />
ST02876CH. ,,<br />
10<strong>04</strong>0968 B/E AEROSPACE, Inc. FAA STC ST02876CH B767-200/-300/-300F/-400ER Installation of BE Aerospace Inc. Vacuum<br />
Toilet Assembly Retrofit Kit<br />
10<strong>01</strong>6917 BAE SYSTEMS AEROSPACE &<br />
DEFENSE<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>302 REV. 1 FAA STC SR<strong>01</strong>906LA BK117 C-2 Installation of the Folding Utility Seat in Multiple-<br />
Place SeatArrangements. The Utility Seating<br />
System, as installed in the MBB BK117 C-2<br />
helicopteris multiple-place utility seating system<br />
consiting of energy-absorbingUtility Installation<br />
of the Folding U<br />
10<strong>01</strong>5952 BARBARA AND ROBERT WILLIAMS <strong>EASA</strong>.IM.A.S.02094 SA572CE CESSNA 150<br />
CESSNA 150A<br />
CESSNA 150B<br />
CESSNA 150C<br />
CESSNA 150D<br />
CESSNA 150E<br />
CESSNA 150F<br />
CESSNA 150G<br />
CESSNA 150H<br />
CESSNA 150J<br />
CESSNA 150K<br />
CESSNA 150L<br />
CESSNA 150M<br />
CESSNA A150K<br />
CESSNA A150L<br />
Replacement of Continental O-200A with<br />
Lycoming 150 or 160hp Model O-320 engines<br />
10<strong>01</strong>6380 BASIC AIRCRAFT PRODUCTS, INC. <strong>EASA</strong>.IM.A.S.027<strong>04</strong> FAA STC ST00702AT CESSNA 210 Installation of Basic Type mBAE-14/28 Model<br />
2025 Deployable Air Driven Alternator System<br />
10<strong>01</strong>6497 BASIC AIRCRAFT PRODUCTS, INC. <strong>EASA</strong>.IM.A.S.02859 FAA STC SA02747AT CESSNA 182 Stand-by Alternator – Installation of Basic Type<br />
BAE-14/28 Deployable Air Driven Alternator<br />
System.<br />
10<strong>01</strong>4838 BAYO S.A.S. <strong>EASA</strong>.A.S.03055 MOONEY M20K Modification of radio electric installation for B-<br />
RNAV capacity with AP/FD coupling.<br />
10<strong>01</strong>4903 BAYO S.A.S. <strong>EASA</strong>.A.S.03138 CESSNA P210N 53/2006 - IFR B-RNAV certification extension<br />
of the GNS530 already installed.<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 />
19.09.2<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 />
27.09.2<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 />
09.08.2<strong>01</strong>2<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 />
14.12.2009<br />
As defined in FAA STC SA572CEModified<br />
engine mounting structure and relocated<br />
battery installation must be inspected every<br />
500 flight hours or annually, whichever occurs<br />
earlier for any cracking or corrosion and if<br />
found rectified with an <strong>EASA</strong> approved re<br />
This approval should not be extended to other<br />
aircraft of this moel on which other previously<br />
approved modifcations will produce noadverse<br />
effect upon the airworthiness of that aircrat.<br />
<strong>EASA</strong> approved Supplemental Airplane Flight<br />
Manual or <strong>EASA</strong> approved Air<br />
20.09.2006<br />
18.<strong>01</strong>.2008<br />
As per FAA STC SA02747AT limitations. 29.08.2008<br />
Modification limited to serial number<br />
250508AFMS must be on board for any flight.<br />
STC Bayo 36/2006 must be already<br />
installed.The aricraft must be equipped with<br />
HSI KI525A and S-TEC 55X autopilot.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 109/<strong>462</strong><br />
31.05.2007<br />
21.<strong>01</strong>.2008
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