04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10016672 AVIDYNE CORPORATION EASA.IM.A.S.03174 FAA STC SA02013CH CIRRUS SR20
Installation of Avidyne Model 9900BX/ TAS 1) Prior to installation of this modification the
27.05.2009
CIRRUS SR22
600 Series Traffic Advisory System (TAS) installer must determine that the
interrelationship between this modification
andany other previously installed modification
will introduce no adverse effect upon the
airworthiness of the product.2) The ins
10030294 AVIDYNE CORPORATION REV. 1 FAA STC SA00269BO 1. SR20, SR22
2.SR22T
Installation of Avidyne 700-00033-() Tactical
Weather Detection System
10033140 AVIDYNE CORPORATION FAA STC SA00296BO SR20, SR22 Installation of Avidyne Model DFC90 Autopilot
P/N 700-00170-000 System
As indicated in FAA STC SA00269BO AML limited to Cirrus Design Corporation
SR20, SR22, SR22T only. Prior to
installation of this modification it must be
determined thatthe interrelationship
between this modification and any other
previouslyinstalled modification and/ or
repair will introdu
as indicated in FAA STC SA00296BOAvidyne
software P/N 530-00214-() Rev 02 or later
FAA approved revisionwith underspeed
protection functionality must be installed on
PFD P/N700-00006-()
10038669 AVIDYNE CORPORATION FAA STC SA00310BO PA46-350P, PA-46R-350T Autopilot Series / DFC 90 Autopilot P/N 700- Aircraft must be configured with an existing S-
00170-002 DFC100 AutopilotP/N 700-00170- TEC 55X (or 55SR)Autopilot and with an
003 as replacement for the S-Tec System 55X existing Avidyne Flight Display System as
Autopilot P/N1192-()-() in accordance with followsin order to accomplish this STC:For
Avidyne Corporation Master Document DFC90: Avidyne Primary Flight Display, p/n
ListAVDFC-077
700-00006-( ), loadedwith Release 8.0.4 so
10039607 AVIDYNE CORPORATION REV. 1 FAA STC SA0282BO PA-46R-350T Integrated Flight Display Enhanced Vision System (EVS) is not included
in the scope of thisapprovalCompatibility with
Mode 5 alerts must be shown when a TAWS
Class A isinstalled.
10041185 AVIDYNE CORPORATION FAA STC SA00282BO SR20, SR22 Installation of Avidyne Corporation 700-00083-
XXX Entegra IntegratedFlight Display System
on Cirrus SR20 and SR22 according Avidyne
Doc. NoAVIFD-006 in latest FAA approved
Revision
As indicated in FAA STC
SA00282BOEnhanced Vision System (EVS) is
not included in the scope of
thisapprovalCompatibility with Mode 5 alerts
must be shown when a TAWS Class A
isinstalled.
21.12.2010
Prior to installation of this modification it 20.12.2010
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the productIf the h
The approval holder shall fulfill the
obligations of Part 21,Paragraph
21.A109.Prior to installation of this
modification it must be determined
thatthe interrelationship between this
modification and any other
previouslyinstalled modification and/ or
06.03.2012
Prior to installation of this modification it 11.10.2012
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
Prior to installation of this modification it 28.08.2012
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product. If the
10042507 AVIDYNE CORPORATION FAA STC SA00323BO 182E, 182F, 182G, 182H, 182J, Installation of Avidyne Corporation Autopilot; Operation must be in accordance with Avidyne The installation of this modification by 05.12.2012
182K, 182L, 182M, 182N, 182P, model DFC90, p/n700-00170-022 (28-Volt Corporation AFMS documentNo. 600-00293- third persons is subject towritten
182R, 182S, 182T, R182. Electrical system) or p/n 700-00170-024 (14- 000, rev.00 dated 01-October-2012.The AFMS permission of the approval holder and
VoltElectrical system), loaded with Release 0 must be carried in the Aircraft during all disposal of the approvedappropriate
Software, as a replacement forthe S-Tec flights.Maintenance must be in accordance with documentation.Prior to installation of this
Autopilot.
ICA document AVDFC-125, rev.00dated 09- modification it must be determined
thatthe interrelationship b
10042851 AVION RESEARCH, Inc. REV. 1 FAA STC SA170CH 1. 172
Installation of a Control Yoke and Instrument None 1. A copy of this certificate or later FAA 21.12.2012
1. 172A/B/C/D/E/F/G/H/I/K/L/M Panel in accordance withFAA STC SA170CH
approved revision must bemaintained as
2. 175, 175A/B/C
part of the permanent records for the
modified aircraft.2. If the holder agrees to
permit another person to use this
certificateto alter the product, the holder
shall give th
10014692 AVIONES, PIEZAS Y ACCESORIOS, S.L. EASA.A.S.02857 PIPER PA-31 Installation Dual integrated NAV/COMM/GPS
GARMIN 480 and Transponder GARMIN GTX
33 (APA OT 5001 Rev.1).
05.02.2008
10014704 AVIONES, PIEZAS Y ACCESORIOS, S.L. EASA.A.S.02875 MITSUBISHI MU-2B-35 Installation of New Avionics Equipment to
comply with COM/NAV regulations for IFR and
B-RNAV Operation.
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10.12.2007