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 />
10035488 KUERZI AVIONICS AG DHC-6-300 Installation of two Aspen Electronic Flight None Prior to installation of this modification it 27.06.2<strong>01</strong>1<br />
Display (EFD1000 Pro, oneGarmin GNS530W<br />
must be determined thatthe<br />
(GPS, COM, NAV), one Garmin GNS430W<br />
interrelationship between this modification<br />
(GPS, COM, NAV), oneGarmin GTX330<br />
and any other previouslyinstalled<br />
(XPDR) and one Garmin GTS800 (TAS)<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product<br />
10036481 KUERZI AVIONICS AG MF50 P-RNAV and RNP10 certificationCertification <strong>EASA</strong> STC 10034392 is a required pre-<br />
of P-RNAV and RNP10 for a Falcon 50 based requisite.<br />
on existing <strong>EASA</strong>STC 10034392.<br />
10036940 KUERZI AVIONICS AG EC 130 B4 G500H Avionic RetrofitOut: Original OEM S/N: all; minimum one G500H compatible<br />
installed Horizon and Directional Gyro system( GPS/WAAS navigator is aprerequisite.<br />
option1 and 2) Original OEM installed Airspeed<br />
Indicator (only option 1) andAltimeter (only<br />
option 1),In: Garmin G500H system including<br />
PFD/MFD GDU 620, Attitude Heading<br />
10039239 KUERZI AVIONICS AG MF900 SATCOM Upgrade to WiFiActivation of the<br />
WLAN option of the existing AVIATOR 300<br />
SATCOM systemon MF900 S/N 118<br />
10<strong>04</strong><strong>01</strong>76 KUERZI AVIONICS AG B737-300 GSM mail tracker installation:a small GSM<br />
device integrated into the aircraft and able to<br />
report itscurrent position by means of GSM cell<br />
information.<br />
Prior to installation of this modification it 12.09.2<strong>01</strong>1<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. 03.11.2<strong>01</strong>1<br />
Limited to MF 900 S/N 118 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.<strong>04</strong>.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 />
18.06.2<strong>01</strong>2<br />
10<strong>04</strong>1972 KUERZI AVIONICS AG R 90-230RG Avionic upgrade Removed: - Original flight None. The approval holder shall fulfill the<br />
instrument including KCS55 pictorial<br />
obligations of Part 21 §21.A118. Prior to<br />
navigationsystem, attitude indication (with flight<br />
installation of this modification it must be<br />
director), electrical attitudeindication, encoding<br />
determined thatthe interrelationship<br />
Altimeter 2x, mechanical AS, VS and turn and<br />
between this modification and any other<br />
bank.- Original vacuum system<br />
previouslyinstalled modification and/ or<br />
repair will i<br />
10<strong>04</strong>2467 KUERZI AVIONICS AG PC-12/45 Replacement of obsolete systemsReplacement<br />
of: - Bendix/King EFIS40/50 Systems with<br />
Universal EFI890R 3-Display.Configuration<br />
(PFD/ND/CPFD) incl. required controls.-<br />
Universal UNS-1K FMS with UNS-1Lw FMS<br />
incl. LPV Monitor as primary NAVSource.<br />
Installation<br />
10<strong>01</strong>7171 KUERZI AVIONICS DEUTSCHLAND<br />
GMBH<br />
10028707 KUERZI AVIONICS DEUTSCHLAND<br />
GMBH<br />
<strong>EASA</strong>.R.S.<strong>01</strong>282 REV. 2 EUROCOPTER FRANCE SA<br />
330J<br />
S/N: 134 ; HB-FOG The approval holder shall fulfill the<br />
obligations of Part 21 §21.A118.Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will in<br />
Avionics UpgradeGPS, Monitor, Cabin Prior to installation of this modification the<br />
Intercom, EMS, SAT111 Tracking System, HF installer must determine that the<br />
Radio, WX Radar, Power Connector, FM interrelationship between this modification and<br />
Radio<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
P-<strong>EASA</strong>.A.S.03752 REV.2 PC-6-B2-H4 Transfer of STC 10028707 Garmin G950<br />
Installation.Integration of a new Garmin G950<br />
Integrated Flight Deck and legacysystems on<br />
the Pilatus PC-6/B2-H4 model.The G950<br />
system (a derivate of the G1000 system)<br />
combines primary flightinstrumentation, aircraft<br />
s<br />
Required pre-modifications:- Pilatus PC-6 pitch<br />
trim warning system according SB-180-<br />
Electrical stall warning system, type Safe Flight<br />
1-02-0005 No. 164(Transmitter) and C-73113<br />
(Buzzer)- Electrical power distribution system<br />
(MCA 06/24/130)- Electrical fl<br />
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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 302/<strong>462</strong><br />
29.10.2<strong>01</strong>2<br />
03.12.2<strong>01</strong>2<br />
06.<strong>01</strong>.2009<br />
30.03.2<strong>01</strong>1
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