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 />
10026871 CHIPPEWA AEROSPACE, Inc. P-<br />
FAA STC ST03280AT BAE 125-700<br />
Installation of a Honeywell Flitelink Engine None. 1. Prior to installation of this modification 19.08.2009<br />
<strong>EASA</strong>.IM.A.S.03213<br />
BAE 125-800<br />
Condition Trend Monitoring- Data Downloader<br />
the installer mustdetermine that the<br />
BAE 125-800A<br />
(ECTM-DD)<br />
interrelationship between this modification<br />
BAE 125-800B<br />
and anyother previously installed<br />
HAWKER 750<br />
modification will introduce no adverse<br />
HAWKER 800<br />
effectupon the airworthiness of the<br />
HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
product.2. The insta<br />
10026882 CHIPPEWA AEROSPACE, Inc. P-<br />
FAA STC ST03573AT CL-600-2B19, CL-600-2C10, Installation of a Goodrich Class 2 Electronic Restricted to Configuration 2 as defined in 1) Prior to installation of this modification 19.08.2009<br />
<strong>EASA</strong>.IM.A.S.03218<br />
CL-600-2D15, CL-600-2D24 Flight Bag<br />
Chippewa AerospaceCertification Plan No 6<strong>01</strong>- the installer mustdetermine that the<br />
<strong>462</strong>0-CP Rev D, dated 24 March 2009. The interrelationship between this modification<br />
applicant must submit the final EWIS ICA, if and anyother previously installed<br />
applicable, to theAgency by7 June 2<strong>01</strong>0 modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product. 2) The inst<br />
10031668 CHIPPEWA AEROSPACE, Inc. REV. 1 FAA STC SA03859AT LIBERTY XL-2 Garmin GTX 330 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 />
05.11.2<strong>01</strong>0<br />
10032241 CHIPPEWA AEROSPACE, Inc. FAA STC SA03860AT LIBERTY XL-2 Honeywell KN-62A DME 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 />
05.11.2<strong>01</strong>0<br />
10<strong>04</strong>21<strong>01</strong> CHIPPEWA AEROSPACE, Inc. FAA STC ST026<strong>04</strong>AT DHC-8-102,-103,-106<br />
DHC-8-2<strong>01</strong>,-202<br />
DHC-8-3<strong>01</strong>,-311,-314,-315<br />
10<strong>04</strong>2660 CHIPPEWA AEROSPACE, Inc. FAA STC ST02<strong>04</strong>6AT DHC-8-102, DHC-8-103,<br />
DHC-8-106, DHC-8-2<strong>01</strong>,<br />
DHC-8-202, DHC-8-3<strong>01</strong>,<br />
DHC-8-311, DHC-8-314,<br />
DHC-8-315.<br />
Installation of a Honeywell MK VIII Enhanced<br />
Ground Proximity WarningSystem (EGPWS).<br />
Installation of a ground service busFAA STC<br />
ST02<strong>04</strong>6AT<br />
The aircraft must be equipped with the factory<br />
installed HoneywellGround Proximity Warning<br />
System (GPWS).<br />
Prior to installation of this modification it 08.11.2<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 />
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 />
12.12.2<strong>01</strong>2<br />
10<strong>01</strong>4984 CHRISTEN-AIRTECH AG <strong>EASA</strong>.A.S.03276 CESSNA P210N Avionics RetrofitOut: King KMA-24; Sigtronics<br />
SPA-400; Dual King KY-196; Dual King KN-53;<br />
King KI-525A; trimble TNL-2000; King KT-76A;<br />
ARGUS-5000; BF Goodrich WX-1000In:<br />
Garmin GMA-347; Dual Garmin GNS-430;<br />
Garmin GTX-330; Garmin GMX-200; L-3 WX-<br />
500; Sande<br />
Reg: HB-CZK S/N: P21-00860 24.<strong>01</strong>.2008<br />
10<strong>01</strong>4987 CHRISTEN-AIRTECH AG <strong>EASA</strong>.A.S.03280 CESSNA P210N Avionics Upgradeby removing:1. GPS-155 1. Reg.: HB-CHJ S/N: P210-0522. Valid for<br />
06.11.2007<br />
GPS2. KX-165 COM/NAV 13. KX-155 this S/N Only.2. Prior to installation of this<br />
COM/NAV 24. WX-8 Stormscope5. KMA- modification the installer must determine that<br />
24 Audio Paneland installing:1. GNS-530 the interrelationship between this modification<br />
COM/NAV/GPS 12. GNS-430<br />
and any other previously installed modification<br />
COM/NAV/GPS 23. WX-500 Stormscope4. will introduce n<br />
GMA-347 Audio Panel<br />
10<strong>01</strong>5066 CHRISTEN-AIRTECH AG <strong>EASA</strong>.A.S.03392 BEECH C90KING AIR GNS 530A, GNS 430A, GAD 42<br />
installation:Removed equipment:- 2 KTR 905<br />
COM 1 & COM 2- 2 KNR 630 NAV 1 & NAV 2-<br />
1 KLN 90B GPS with AK-950 GPS<br />
Annunciator- 1 KDM 705A DME with KDI 570<br />
DME IndicatorNew installed equipment:- 1<br />
GNS 530AW COM/NAV/GPS 1 with GAD 4<br />
F-GBLU, SN: LJ-822. 10.09.2008<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 155/<strong>462</strong>
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