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
10014006 AERODISA S.L. EASA.A.S.01043 EMBRAER EMB-120 Installation TCAS IIHoneywell TCAS II TPU Subject th the conditions, limitations and
31.07.2006
67A Processor and Configuration Module with procedures contained in Doc No.
lower and upper ANT 67A Antennas, dual IVA- AED2004_01M_D03_OP1 "Flight Manual
81D TA/RA/VSI System Displays, one Supplement for 1 transponder installation", Rev
MST67A Mode S Transponder (OPTION 1) or 0 or AED2004_01M_D03_OP2 " Flight Manual
two MST67A Mode S Transponder (OPTION Suppplement for 2 transponders installation",
2) with lower
Rev. 0
10014051 AERODISA S.L. EASA.A.S.01133 FAIRCHILD SWEARINGEN SA TCAS II installation on Fairchild SA
Subjected to the conditions, limitations and
04.09.2006
227 SE
227Honeywell TCAS II TPU 67A Processor pocedures contained in Doc N°
FAIRCHILD SWEARINGEN SA and Configuration Module with lower and upper AED2004_02M_D03 "Flight Manual
227-BC
ANT 67A Antennas, dual IVA-81D TA/RA/VSI Supplement", Rev 0
System Displays, two MST67A Mode S
Transponders with lower and uppar KA60
Omnidirectional Ant
10014286 AERODISA S.L. EASA.A.S.01523 DC-8-62 SERIES Revision to the cargo modification on DC-8-62. Limited to DC-8-62 series airplanes which have
18.04.2007
Compliance with FAA AD 2001-26-04 & AD been converted from a passenger to a cargo-
2001-26-01.
carrying ("freighter") configuration by FAA STC
No. SA1802SO, but with a deviation in the
main deck cargo 9g crash barrier that was
installed following FAA STC No. SA
10014368 AERODISA S.L. EASA.A.S.01638 EMBRAER EMB-120 Structural Permanent element for a Winch
installation.
10014475 AERODISA S.L. EASA.A.S.02537 FALCON 20 AED2006-01M: TCAS II Installation for Falcon
20.
10014608 AERODISA S.L. EASA.A.S.02734 EMBRAER EMB-120 AED2006-03M: TAWS Installation on
EMBRAER 120.
10014609 AERODISA S.L. EASA.A.S.02735 FAIRCHILD SWEARINGEN SA
226 SE
FAIRCHILD SWEARINGEN SA
227 SE
AED2006-04M: TAWS installation on Fairchild
SA 226/227
1. Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The i
1. See FM Supplement AED2006-01M_D03
Section I: LIMITATIONS.2. Certification basis
CS 25 Orig issue.3. TGL 8 Rev.2 "ACAS II"
complied with.4. TGL 13 Rev.1 "Elementary
Surveillance" complied with.5. Prior to
installation of this modification
1. See FM Supplement AED2006-
01M_MDL_D03 Section II: LIMITATIONS.2.
Certification basis per ANAC TCDS EA-8505:
RBHA 25 corresponding to FAR 25 Amdt 54.3.
TGL 12 complied with.4. SANDEL
mandatory SB 3400-09 to be incorporated.5.
Prior to ins
See FM Supplement AED2006-04M_D03
Section II: Limitations.Certification basis per
FAA TCDS A8SW: FAR 23 Amdt 6.TGL 12
10014735 AERODISA S.L. EASA.A.S.02918 MYSTERE FALCON 20 AED2006-14M: TAWS installation for Falcon
complied with.
See FM Supplement AED2006-14M_D03
26.07.2007
20.
Section II "Limitations".Certification basis:
CS25 initial issue.TGL 12 complied
with.SANDEL mandatory SB 3400-09 to be
incorporated.
10014748 AERODISA S.L. EASA.A.S.02933 MD80 SERIES LOPA for MD80 Series 168 Pax/ Layout The installation should not be incorporated in
31.05.2007
passenger arrangement to allow 168
any other aircraft unless it is determined that
passengers capacity.
the interrelationship between this installation
and any previously approved configuration will
not introduce any adverse effect upon the
airworthiness of the air
10014776 AERODISA S.L. EASA.A.S.02974 PIPER PA-23-250 Upgrade of NAV/COM Equipment for IFR
navigation.
S/N: 27-7754134. 18.07.2007
10015273 AERODISA S.L. EASA.A.S.03756 FALCON 900 Upgrade of dual Mode S SSR Transponder 1. Prior to installation of this modification the
27.03.2009
installation to provide both Elementary Mode S installer must determine that the
Surveillance Flight ID and Enhanced Mode S interrelationship between this modification and
Surveillance capability (EHS Capable). any other previously installed modification
will introduce no adverse effect upon the
airworthiness of the product.2.
10028207 AERODISA S.L. P-EASA.A.S.03152 REV. 1 FALCON 2000 Pocket Door Installation for Falcon 2000In Design Change limited to Falcon 2000 aircraft Prior to installation of this modification it 21.12.2009
accordance with Aerodisa Master Data List serial number 55
must be determined thatthe
AED2007-09M_MDL Revision 3,dated 04th
interrelationship between this modification
December 2009 or later revisions approved by
and any other previouslyinstalled
EASA
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
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