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
10016392 DUNCAN AVIATION, INC. EASA.IM.A.S.02721 FAA STC ST00914WI-D LOCKHEED 1011-385-1 Installation of Dual IS&S Air Data/ Altimeter approval may be extended to aircraft models
26.05.2008
System along with two inch standby pneumatic Lockheed 1329-23, previously modified iaw
altimeter (FAA STC ST00914WI-D).
FAA STC SA2326SW, when this STC has
been EASAvalidated.Lockheed 1329-25 Group
Approval for RVSM requirements can be
shown in conjunction with FAA STC
ST01082SE (AeroMech
10016393 DUNCAN AVIATION, Inc. EASA.IM.A.S.02722 FAA STC ST01059WI LOCKHEED 1011-385-1 Installation of Honeywell MK VII Enhanced This Design Approval may be extended to
Ground Proximity Warning System (EGPWS). Airplanes Model Lockheed 13-29-23,
FAA STC ST01059WI.
previously modified iaw FAA STC SA2326SW,
when validatedby EASA.Prior to installation of
this modification the installer must determine
that the interrelationship between this modif
10026867 DUNCAN AVIATION, INC. P-
EASA.IM.A.S.03211
10028927 DUNCAN AVIATION, INC. P-
EASA.IM.A.S.03046
FAA STC ST00703WI CESSNA 650 Installation of an AlliedSignal Enhanced Ground According to associated technical
Proximity Warning System(EGPWS) documentation, FAA STC, AFMS and ICA
FAA STC ST01409WI-D MYSTERE FALCON MF900 EASA Validation of FAA STC ST01409WI- Validation limited to Basic Mystere Falcon
DInstallation of an L3 Communications, GH-
3100 Electronic StandbyInstrument System
(ESIS) in accordance with Duncan Aviation Inc
MasterDocument List No 06062208, Revision
C, dated February 19th, 2008or later revisions
a
MF900 aircraft model
10040935 DUNCAN AVIATION, INC. FAA STC ST00600CH-D MF 900 & F900EX EASA validation of FAA STC ST00600CH-D As per FAA STC ST00600CH-D issue dated
issue dated 12 Sept 2008Installation of
Honeywell Enhanced Ground Proximity
Warning System withWindshear Detection and
optional Terrain Display (S/W level -218-
218)and optional Runway Advisory Awareness
System (RAAS)
12 Sept 2008
10028837 DUNLOP AIRCRAFT TYRES LIMITED P-EASA.A.S.03864 REV. 1 EMBRAER ERJ 190-100 ECJ
EMBRAER ERJ 190-100IGW
EMBRAER ERJ 190-100LR
EMBRAER ERJ 190-100STD
EMBRAER ERJ 190-200IGW
EMBRAER ERJ 190-200LR
EMBRAER ERJ 190-200STD
10038094 DUNLOP AIRCRAFT TYRES LIMITED 0010014209-001 TCCA STC SA02-29 CL-600-2B19 Installation, Dunlop Aircraft Tyres Ltd P/N
DR27921T Main and DR15112TNose Gear
Tyres This STC is issued in order to reflect the
transfer of ownership fromACS-NAI Ltd to
Dunlop Aircraft Tyres Ltd. This STC has
previously been validated in the following Eur
10039387 DUNLOP AIRCRAFT TYRES LIMITED ATR 42-200/-300/-320/-400/-500 Installation of Dunlop Aircraft Tyres on ATR 42
seriesThe STC installs Dunlop Aircraft Tyres
Ltd P/N DZ33012T (Main LandingGear) and
P/N DR15520T (Nose Landing Gear).
10041486 DUNLOP AIRCRAFT TYRES LIMITED ERJ 170-100 LR,
ERJ 170-100 STD,
ERJ 170-200 LR,
ERJ 170-200 STD.
Dunlop Aircraft Tyres Limited P/N DZ32816T
Radial Nose Landing Gearinstallation on ERJ
170.
Different nose landing gear part number tires
may not be intermixed onthe same axle.
13.10.2008
Prior to installation of this modification it 18.08.2009
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 19.02.2010
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 product.
Prior to installation of this modification it 06.08.2012
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.
29.06.2009
Prior to installation of this modification it 18.01.2012
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.
None Prior to installation of this modification it
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.
02.05.2012
It is not allowable to mix different tyre types
(radial and bias) in thenose landing gear leg.
Prior to installation of this modification it 20.09.2012
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.
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