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>6109 CASCADE AVIATION SERVICES INC. <strong>EASA</strong>.IM.A.S.02299 STC ST<strong>01</strong>181SE DORNIER 328-100<br />
Installation of increased security cockpit door A copy of this Certificate and Cascade Aviation<br />
19.<strong>01</strong>.2007<br />
DORNIER 328-300<br />
Services Master Drawing List (MDL)<br />
02CAS096-MDL, Revision D, dated July 14,<br />
2003 orlater approved revision must be<br />
maintained as part of the permanent records<br />
for the modified aircraft<br />
10027057 CASCADE AVIATION SERVICES INC. P-<br />
FAA STC ST<strong>01</strong>133SE DHC-8-102, -103, -106<br />
Installation of an increased security cockpit None 1) Prior to installation of this modification 02.09.2009<br />
<strong>EASA</strong>.IM.A.S.03259<br />
DHC-8-2<strong>01</strong><br />
doorFAA STC # ST<strong>01</strong>133SE<br />
the installer mustdetermine that the<br />
DHC-8-3<strong>01</strong>, -311, 314, 315<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product. 2) The inst<br />
10039180 CEAPR REV. 2 HR 200/100, HR200/100S<br />
HR200/120, HR200/120B<br />
HR200/160<br />
R2100, R2100A, R2112, R2120U<br />
R2160, R2160D, R2160I<br />
DET 1203<strong>01</strong> Rev. 0 - Oil pressure tranducer<br />
line R2000-HR2000 dated 7March 2<strong>01</strong>2<br />
10032548 CENTURY FLIGHT SYSTEMS, INC AK 847 STC SA 3389SW-D PA-31, PA-31-325, PA-31-350 AK 847 Validation / Century 41 Installation in<br />
Piper, Type CertificateNumber A20SO models<br />
PA-31, PA-31-325, PA-31-350<br />
Limitation to serial numbers 0<strong>01</strong> up to 378<br />
included.<br />
1. This STC is limited to aircraft Models PA-31,<br />
PA-31-325 and PA-31-350,2. Piper<br />
Model PA-31 is limited to S/N 712 and<br />
Up,3. Placard 13A990-1 stating<br />
"conduct trim check prior to first flight ofday<br />
(see POH)" is required<br />
Prior to installation of this modification it 26.<strong>04</strong>.2<strong>01</strong>2<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 />
The approval holder shall fulfill the 15.11.2<strong>01</strong>0<br />
obligations of Part 21, Pragraph21A.3<br />
The approval holder shall fulfill the<br />
obligations of Part 21, Paragraph21.A109<br />
Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between<br />
10<strong>01</strong>5954 CERTIFICATION DOCUMENTS AND <strong>EASA</strong>.IM.A.S.02097 FAA STC ST10674SC CESSNA 750 CITATION X Installation of an Aerodata AG Automatic Flight Limited to Aircraft Serial Number 262 only.<br />
Inspection System (AFIS).<br />
15.10.2007<br />
10<strong>01</strong>4339 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.<strong>01</strong>597 MITSUBISHI MU-2B-36A Avionics Upgrade in accordance with doc No<br />
CLS-05-MU-AC128, Revision 1.3., dated<br />
27/<strong>01</strong>/2006.<br />
Limited to S/N MU2B-36A-718SA. 08.02.2006<br />
10<strong>01</strong>4486 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.02548 LETECKE ZAVODY L 200 D Avionics upgrade in accordance with the<br />
document no;CLS-06-L200-AC 129, dated<br />
23/06/2006<br />
S/N 171206 28.07.2006<br />
10<strong>01</strong>4761 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.02951 CESSNA 421C Avionics Upgrade, Proj. No.: CLS-07-C421-<br />
AC147Replacement of existing obsolete<br />
transponder, altimeters, ELT and COM/NAV<br />
with new that meets the current technical and<br />
operating requirements.<br />
15.10.2007<br />
10<strong>01</strong>49<strong>01</strong> CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.03135 CESSNA 172S Installation of the DME KN 62A, ADF KR-87<br />
and XPDR KT-73<br />
10.10.2007<br />
10<strong>01</strong>4989 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.03284 LETECKE ZAVODY L-410-UVP- Installation of ACAS II system with XPDR This STC is valid only for L410-UVP-E13<br />
05.11.2007<br />
E13<br />
(MST-67A) and ELT defined in document CLS- aircraft type, registration OK-UDS, S/N 892321<br />
05-L410-AC125, revision 02 dated <strong>04</strong>.11.2005<br />
10<strong>01</strong>4990 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.03285 LETECKE ZAVODY L-410-UVP Installation of NAV/COM/GPS as defined in<br />
document CLS-06-6410-AC140, issue 0,<br />
revision 2 dated 13.09.2006<br />
1. This STC is valid only for L410-UVP aircraft<br />
type.<br />
10<strong>01</strong>4991 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.03286 LETECKE ZAVODY L 410 UVP-E Installation of- ACAS II (CAS-67) system with 1. This is valid only for L-410-UVP-E aircraft<br />
one XPDR (MST-67)- EGPWS Mk. VI system- type.<br />
KLN-94 GPS receiver, FA 2100 CVR, C 406-1<br />
ELT- KMA-24H-70, LUN1120 and SAE-5-35as<br />
defined in document CLS-06-L410-AC138,<br />
issue 0, revision 1 dated 14.<strong>04</strong>.2006<br />
10<strong>01</strong>5069 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.03395 LETECKE ZAVODY L 200 A<br />
LETECKE ZAVODY L 200 D<br />
10<strong>01</strong>5193 CESKA LETECKA SERVISNI A.S. <strong>EASA</strong>.A.S.03577 CESSNA 414<br />
CESSNA 414A<br />
10029112 CESKA LETECKA SERVISNI A.S. L-410 UVP-E-LW, L-410 UVP- Dual Mode-S Transponder upgrade for EHS<br />
E20,<br />
L-410 UVP-E9, L-410 UVP-LW,<br />
L-410M, L-410 UVP, L-410 UVP-E<br />
L-420<br />
capability<br />
05.11.2007<br />
05.11.2007<br />
Installation of new COM, NAV, GPS, XPDR +<br />
<strong>04</strong>.07.2008<br />
Encoder, DME, ADF and flight instruments to<br />
meet the current technical and operating<br />
requirements of IFR category.<br />
Avionics upgrade 16.12.2008<br />
None None 05.03.2<strong>01</strong>0<br />
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