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
10027121 AIRCRAFT PERFORMANCE
P-
REV. 1 FAA STC SA01935LA 401, 401A, 401B, 402, 402A, Installation of external aft body strakes None 1) Prior to installation of this modification 22.02.2010
MODIFICATIONS,
EASA.IM.A.S.03144
402B, 402C, 411, 411A, 414,
the installer mustdetermine that the
414A, 421, 421A, 421B, 421C,
interrelationship between this modification
425, 441
and anyother previously installed
modification will introduce no adverse
effectupon the airworthiness of the
product.2) The insta
10015803 AIRCRAFT SAFETY EQUIPMENT EASA.IM.A.S.01868 SA3278SO BOEING DC-10
BOEING MD 11 SERIES
10040586 AIRCRAFT STRUCTURES
INTERNATIONAL
10041470 AIRCRAFT STRUCTURES
INTERNATIONAL
10015313 AIRCRAFT SYSTEMS AND
MANUFACTURING,
10015341 AIRCRAFT SYSTEMS AND
MANUFACTURING,
10015342 AIRCRAFT SYSTEMS AND
MANUFACTURING,
10015350 AIRCRAFT SYSTEMS AND
MANUFACTURING,
10015772 AIRCRAFT SYSTEMS AND
MANUFACTURING,
10015950 AIRCRAFT SYSTEMS AND
MANUFACTURING,
10015964 AIRCRAFT SYSTEMS AND
MANUFACTURING,
10016137 AIRCRAFT SYSTEMS AND
MANUFACTURING,
Smoke Barrier Cargo Copmartment McDonnell- 1. The Aircraft Flight Manual should be
Douglas (Boeing) MD-11F, aircraft serial no. amended in order to make sure that before
48445.Installation of a modified berrier in the each flight:(a) the integrity of the smoke barrier
Class "E" cargo compartment in accordance is checked:(1) the smoke barrier should be
with FAA STC SA3278SO, reissued on without any tears(2) the OEM crown area
September 24, 2004
smoke barrier should be without any tear
FAA STC SA10840SC CESSNA 208, CESSNA 208B Installation of Jack Pads on Cessna 208 Series None Prior to installation of this modification it 11.07.2012
aircraft in accordancewith FAA STC
must be determined thatthe
SA10840SC
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
FAA STC NO. SA011054SC 208, 208B Installation of an internal Cargo Pod lighting
system.
EASA.IM.A.S.00166 FAA STC ST09887 SC BOEING 727 Installation of RVSM compliant equipment
(dual DADS).FAA STC N° ST09887 SC
EASA.IM.A.S.00415 FAA STC ST09988SC DC-9-81 (MD-81)
DC-9-81 (MD-82)
DC-9-81 (MD-83)
DC-9-81 (MD-87)
EASA.IM.A.S.00416 ST09989SC DC-9-81 (MD-81)
DC-9-81 (MD-82)
DC-9-81 (MD-83)
DC-9-81 (MD-87)
EASA.IM.A.S.00522 FAA STC ST09586SC REV 1 DC-9-81 (MD-81)
DC-9-81 (MD-82)
DC-9-81 (MD-83)
DC-9-81 (MD-87)
EASA.IM.A.S.01811 FAA STC ST09580SC BOEING 767-200
BOEING 767-300
EASA.IM.A.S.02092 ST10084SC BOEING 737-100
BOEING 737-200
BOEING 737-300
Installation of Universal Avionics Terrain
Awareness & Warning System.
Installation of Universal Avionics Multi Function
Display Model 640.
If the holder agrees to permit another person to
use this certificate toalter the product, the
holder shall give the other person
writtenevidence of that permission.
1. This STC is approved only for the
installation of an RVSM compliant Air Data
System and does not constitute an approval of
RVSM operation.2. This STC is approved
only for the product configuration as defined in
the approved design data referred to
1. This STC is approved only for the product
configuration as defined in the approved design
data referred to in the paragraph "Description".
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
1. This STC is approved only for the product
configuration as defined in the approved design
data referred to in the paragraph "Description".
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
Installation of Universal UNS Flight
1. This STC is approved only for the product
Management System with UL-601 Unilink Data configuration as defined in the approved design
Link System
data referred to in the paragraph "Description".
Compatibility with other aircraft/engine
configurations shall be determined by the
installer.
Installation of Digital Flight Data Recorder
(RFDR) Expanded ParameterUpgrade for
Teledyne ARINC 717 DFDAU.
Installation of an Innovative Solutions &
Support (IS&S) digital air data system
consisting of an electric altimeter, Digital Air
Data Computer (DADC), Air Data Display Unit
(ADDU), and an altitude alerter in accordance
with ASM Master Data List 5572-0001-
The installation of this modification by
third persons is subject towritten
permission of the approval holder and
disposal of the approvedappropriate
documentation. Prior to installation of this
modification it must be determined
thatthe interrelationship
EASA.IM.A.S.02113 ST09744SC BAE 146/AVRO 146 SERIES Installation of a Digital Flight Data Recorder
(DFDR) Expanded Parameter Sensor Upgrade
on a British Aerospace Avro 146-RJ85A
Aircraft
None 19.07.2006
EASA.IM.A.S.02333 FAA STC NO. ST10606SC BOEING 767-200
Installation of Mode S Upgrade, Elementary
07.03.2008
BOEING 767-300
BOEING 767-400
and Enhanced Surveillance Parameters
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14.11.2006
19.09.2012
07.10.2004
14.12.2004
14.12.2004
19.01.2005
20.03.2006
15.03.2007