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>6599 RAISBECK ENGINEERING <strong>EASA</strong>.IM.A.S.03<strong>01</strong>2 REV. 1 FAA STC ST3591NM 200, 200C, 200T, 200CT, A200, Installation of lower aft fuselage strakes. None Prior to installation of this modification the <strong>01</strong>.07.2<strong>01</strong>1<br />
A200C, A200CT, B200, B200C,<br />
installer must determinethat the<br />
B200GT, B200CGT<br />
interrelationship between this modification<br />
B200T, B200T, B200CT,<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product. The installati<br />
10<strong>01</strong>6620 RAISBECK ENGINEERING <strong>EASA</strong>.IM.A.S.03051 FAA STC ST00752SE BEECH 200<br />
This change applies only to the above listed Requires the prior incorporation of Raisbeck<br />
15.12.2008<br />
SEE ATTACHED <strong>EASA</strong><br />
model aircraft in accordance with Raisbeck STC’s ref:-SA4175NM (when equipped with<br />
APPROVED TYP<br />
Engineering Master Drawing List 99-1500, High Floatation<br />
Revision D, dated May 13, 2008 or later gear)SA3366NMSA3831NMSA3519NMIt is<br />
approved revisions.<br />
the installers responsibility to ensure all these<br />
referenced STC’s are <strong>EASA</strong> approved.<br />
1003<strong>01</strong>24 RAISBECK ENGINEERING <strong>EASA</strong>.IM.A.S.02986 REV. 3 FAA STC SA4175NM 200, 200C, 200T, 200CT, A200<br />
A200C, A200CT, B200, B200C<br />
B200T, B200CT, B200GT,<br />
B200CGT<br />
B300, B300C<br />
Installation of fully enclosed main landing gear<br />
door system forhigh-flotation gear equipped<br />
aircraft.<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 />
10.08.2<strong>01</strong>1<br />
10031275 RAISBECK ENGINEERING <strong>EASA</strong>.IM.A.S.00765 REV. 1 FAA STC SA2698NM-S BEECH 200, A200, B200 Installation of Hartzell/Raisbeck Quiet Turbofan Data is suitable for reproduction and installation Prior to installation of this modification it 09.08.2<strong>01</strong>0<br />
Propeller. Thisinstallation consists of Hartzell 4- on all Beech SuperKing Model 200 series must be determined thatthe<br />
bladed propellers and aluminum hubswith aircraft. Approval of this change in type interrelationship between this modification<br />
spinners, and a propeller de-icing system designapplies to the above model aircraft only and any other previouslyinstalled<br />
This approval should not be extended to other modification and/ or repair will introduce<br />
aircraft on which otherpreviou<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10031307 RAISBECK ENGINEERING FAA STC ST<strong>01</strong>182LA A320-232 A320 bin extension systemInstallation of a bin<br />
extension system in accordance with<br />
FAASupplemental Type Certificate<br />
ST<strong>01</strong>182LA issued 10 July 20<strong>01</strong>.<br />
10027805 RAM AIRCRAFT, LIMITED<br />
PARTNERSHIP<br />
10031425 RAM AIRCRAFT, LIMITED<br />
PARTNERSHIP<br />
10031513 RAM AIRCRAFT, LIMITED<br />
PARTNERSHIP<br />
10032348 RAM AIRCRAFT, LIMITED<br />
PARTNERSHIP<br />
- Refer to paragraph "Limitations & Conditions"<br />
listed in the FAA STCST<strong>01</strong>182LA;The<br />
Maintenance Instructions for Continued<br />
Airworthiness are containedin the RCAG<br />
Component Maintenance Manual 200A-2560.<br />
These maintenanceinstructions must be<br />
included in the o<br />
Prior to installation of this modification it 09.08.2<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 />
FAA STC SE10746SC-D IO-520-B -, -BB, -C, -CB Conversion of Teledyne Continental Motors The RAM model IO-550-B-RA engine is This approval should not be extended to 17.11.2009<br />
(TCM) models IO-520-B, -BB toRAM model IO- identical to and has the sameratings,<br />
other engines of these models onwhich<br />
550-B-RA engine, or conversion of TCM limitations, and installation interfaces as TCM other previously approved modifications<br />
models IO-520-C, -CBto RAM model IO-550-C- model IO-550-Bengine. The RAM model IO- are incorporated unless itis determined by<br />
RA engine in accordance with RAM Master 550-C-RA is identical to and has the<br />
the installer that the interrelationship<br />
DrawingList 2691, Revision I.R. dated sameratings, limitations, and installation between thischange and any other<br />
November 7, 20<br />
interfaces as T<br />
previously approved m<br />
REV. 2 FAA STC SA8125SW-D CESSNA 414A Installation of vortex generators in acc. with None See under "Description" Prior to 12.11.2<strong>01</strong>0<br />
FAA STC SA8125SW-D, lastissue, dated May<br />
installation of this modification it must be<br />
12, 2008:Option 1: Modification in acc. with<br />
determined thatthe interrelationship<br />
RAM Master Drawing No. 1507,Revision C,<br />
between this modification and any other<br />
dated 11/03/1992.Option 2: Modification in acc.<br />
previouslyinstalled modification and/ or<br />
with RAM Master Drawing No. 1507,Re<br />
repair will introduce no adverse<br />
effectupon the airworthines<br />
REV. 1 FAA STC SA09105SC-D CESSNA 414A Modification in acc. with FAA STC SA09105SC-This<br />
approval is limited to Hartzell PHC-C3YF- Prior to installation of this modification it 12.11.2<strong>01</strong>0<br />
D: Aircraft modified inaccordance with RAM 2UF/FC7663D(B)-2Q or PHC-C3YF- must be determined thatthe<br />
Master Drawing No. 1765, Revision B, 2UF/FC7693DF(B) propellers.<br />
interrelationship between this modification<br />
dated20/09/1995 and Installation of modified<br />
and any other previouslyinstalled<br />
TCM engine model TSIO-520-NB:Option 1:<br />
modification and/ or repair will introduce<br />
Cessna 414A modified by FAA STC<br />
no adverse effectupon the airworthiness<br />
SE091<strong>04</strong>SC-D or S<br />
of the product.<br />
REV. 1 FAA STC SA09971SC-D 1. CESSNA 340, 340A<br />
2. CESSNA 414, 414A, 402C<br />
Installation of Hartzell propeller PHC-C3YF-<br />
2UF/FC7693DF(B) inaccordance with FAA<br />
STC SA09971SC-D<br />
1. Hartzell Modell PHC-C3YF-2UF/FC7693DF Prior to installation of this modification it<br />
or PHC-C3YF-2UF/FC7693DFBpropellers are must be determined thatthe<br />
02.11.2<strong>01</strong>0<br />
limited to aircraft that are previously FAA interrelationship between this modification<br />
approved toinstall 78-inch (198 cm) diameter and any other previouslyinstalled<br />
propellers and have TCM model TSIO- modification and/ or repair will introduce<br />
520series engines with maximum rated power no adverse effectupon the airworthiness<br />
from 285<br />
of the product<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 365/<strong>462</strong>
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