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>04</strong>0254 H4 AEROSPACE (UK) Ltd. B757-200 Passenger cabin reconfiguration on Openskies None<br />
B757<br />
None 20.06.2<strong>01</strong>2<br />
10<strong>04</strong>0531 H4 AEROSPACE (UK) Ltd. 767-200, -300 Introduction of an AD Aerospace Cockpit Door none Prior to installation of this modification it 09.07.2<strong>01</strong>2<br />
and Cabin SurveillanceSystem on Boeing B767-<br />
must be determined thatthe<br />
200/300.<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>04</strong>1036 H4 AEROSPACE (UK) Ltd. B757-200 Cabin Re-configuration and Airvod IFE System<br />
Installation<br />
10<strong>01</strong>5668 HARTZELL PROPELLER INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>644 FAA STC SA<strong>01</strong>850CH DIAMOND DA-40 Installation of Hartzell Two blade propeller HC-<br />
C2YR-1BF/F7495S with STC SA<strong>01</strong>850CH in<br />
the Diamond DA40 aeroplane<br />
1003<strong>01</strong>56 HARTZELL PROPELLER INC. P-<br />
<strong>EASA</strong>.IM.A.S.03250<br />
FAA STC SA02677CH-D PA-46-350P, PA-46R-350T <strong>EASA</strong> validation of FAA STC SA02677CH-<br />
DInstallation of Hartzell Propellers HCI3YR-<br />
1N/N7605(K)+2,HCI3Y1R-1N/N7605(K)+2<br />
10034394 HARTZELL PROPELLER INC. FAA STC SA10551SC 58, 58A, G58 Installation of Hartzell PHC-J3YF-<br />
2UF/FFC7391D(B, K) propellers<br />
10038909 HARTZELL PROPELLER INC. FAA STC SA02130SE KING AIR B200GT AND B200CGT Installation of BLR Hartzell Composite<br />
Propeller HC-E4N-3A/NC9208K.<br />
10039256 HARTZELL PROPELLER INC. FAA STC SA0<strong>04</strong>70AT A188, A188A, A188B Installation of either a Hartzell model PHC-<br />
C3YF-1RF/F8468A()-6Rpropeller and<br />
associated spinner assembly C-3535-1(P) in<br />
accordance withFAA STC SA0<strong>04</strong>70AT<br />
10<strong>01</strong>5394 HARTZELL SERVICE CENTER <strong>EASA</strong>.IM.A.S.<strong>01</strong>095 SA1105CH PIPER PA-32-260 Installation of Hartzell HC-C3YR-1RF/F7693F<br />
three bladed propeller on the Piper-PA32-260<br />
per FAA STC SA1105CH<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 />
17.08.2<strong>01</strong>2<br />
Diamond Modifications as detailed in the<br />
Installation instructions<br />
For further limitations see applicable<br />
associated technicaldocumentation<br />
30.09.2005<br />
1. Prior to installation of this modification 31.05.2<strong>01</strong>0<br />
the installer mustdetermine that the<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 />
Only aircraft equipped with a Teledyne Prior to installation of this modification it 31.03.2<strong>01</strong>1<br />
Continental IO-550-C engine areeligible for this must be determined thatthe<br />
STC.<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 />
Requires the installation of a BLR Aerospace Eligible Serial Numbers are listed in FAA 22.03.2<strong>01</strong>2<br />
Ultimate PerformancePackage (UPP) ref FAA Approved MDL BLR-KA250CP-<br />
STC SA02131SE and <strong>EASA</strong> STC 10038758. 002,Revision B dated May 3, 2<strong>01</strong>1. Prior<br />
to installation of this modification it must<br />
be determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modi<br />
None If the holder agrees to permit another<br />
person to use this certificate toalter the<br />
product, the holder shall give the other<br />
person writtenevidence of that<br />
permission.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
1. <strong>EASA</strong> does not consider this modification to<br />
increase the noise level and it was not<br />
considered an acoustical change from the HC-<br />
C2YK-1F/F8477-2 Propeller.2. If the holder<br />
agrees to permit another person to use this<br />
certificate to alter the product, the<br />
10<strong>01</strong>5485 HARTZELL SERVICE CENTER <strong>EASA</strong>.IM.A.S.<strong>01</strong>245 FAA STC SA02181AK CESSNA 208, CESSNA 208B Installation of a Hartzell HC-B3TN-<br />
3AF(Y)/T10890CN(K)-2 three bladed propeller<br />
and D-4897(P) assembly on the type Cessna<br />
208, 208A and 208B in accordance with the<br />
application dated 22 April 2005.FAA STC:<br />
SA02181AK<br />
-- 07.08.2006<br />
10<strong>01</strong>5907 HARTZELL SERVICE CENTER <strong>EASA</strong>.IM.A.S.02033 SA02092AK CESSNA 208<br />
Installation of Hartzell HC-D4N-3R/D9511F(K) This approval is limited to Model 208<br />
13.<strong>04</strong>.2007<br />
CESSNA 208A<br />
CESSNA 208B<br />
Four Bladed Propeller and D-630-3(P) Spinner landplanes only.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 260/<strong>462</strong><br />
20.<strong>04</strong>.2<strong>01</strong>2<br />
30.05.2005
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