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
10015847 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01947 FAA STC ST00417SE BOEING 767-200
Installation of Enhanced Ground Proximity Honeywell International Inc. Airplane Flight
07.04.2006
BOEING 767-300
Warning System (EGPWS)
Manual Supplements 060-4189-003 Revision
BOEING 767-300F
B, 060-4189-014 Revision A, 060-4189-008
Revision A, 060-4189-037 Initial Revision, 060-
4189-052 Revision A, 060-4189-013 Initial
Revision, 060-4189-068 Revision A, 060-4
10015893 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02013 FAA STC ST00446SE DC-9-80 (MD-80) SERIES Installation of the Honeywell Solid State Flight
Data Recorder
-- 11.09.2006
10015921 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02054 FAA STC ST00389SE BOEING 737-200
Installation of the Honeywell Enhanced Ground - Approval of this change in type design applies
28.02.2007
BOEING 737-300
proximity Warning System (EGPWS) and to the BOEING 737-200/ -300/ -400/ -500/ -
BOEING 737-400
Runway Awareness & Advisory System 700/ -800/-900 aircraft equipped with either a
BOEING 737-500
(RAAS).
flight management system (FMS) or a global
BOEING 737-700
positioning system (GPS) based navigation
BOEING 737-800
BOEING 737-900
system or an EGPWS equipped with
10015934 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02072 FAA STC ST00255DE-D BAE 146/AVRO 146 SERIES Installation of Allied Siganl VHF AFIS -- 26.09.2006
10015946 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02088 FAA STC ST01000SE BOEING 737-600
Installation of the Mark II Aircraft
1. Compatibility of this design change with
09.10.2006
BOEING 737-700
Communications Addressing and Reporting other previously approved modifications must
BOEING 737-800
System (ACARS) in the Boeing 737-600, -700, be determined by the installer.
BOEING 737-900
-800, -900Series Aircraft.
10015949 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02091 FAA STC ST01424CH-D HAWKER 125 -800 SERIES Installation of Honeywell N1 Digital Electronic
04.10.2006
HAWKER 125 -850XP SERIES Engine Control (DEEC)
10015962 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02110 FAA STC ST00844SE BAE 146/AVRO 146 SERIES Installation of the Flight Data Acquisition This change is not JAR-OPS-1.715
13.12.2006
Management System (FDAMS)
(EUROCAE ED55) compliant in the following
parameters:Parameter 6, Pitch Attitude is only
sampled once per second.Parameter 7, Roll
Attitude is only sampled once per
second.Parameter 23, Ground Spoiler position,
Brake Select
10016042 HONEYWELL INTERNATIONAL Inc. EASA.IM.A.S.02213 FAA STC ST01003CH-D 600A, 600B, 700A, 700B Installation of Honeywell N1 Digital Electronic 1. Compatibility of this modification with other
12.12.2006
DH. 125 SERIES 1A, 3A, 3A/RA, Engine Control (DEEC).
previously approved modifications must be
F3B, F3B/RA, 400A, 400B, 403B,
determined by the installer2. This STC is
approved only for the product configuration as
defined in the approved design data referred to
in the paragraph "Desc
10016089 HONEYWELL INTERNATIONAL Inc. EASA.IM.A.S.02276 FAA STC SA6086NM BOEING 767-300 Installation of Honeywell/Racal Aeronautical
SATCOM
10016115 HONEYWELL INTERNATIONAL Inc. EASA.IM.A.S.02306 FAA STC SA5473NM BOEING 747-100-400 Installation of Honeywell/Racal Aeronautical
Satelite Communication system
10016173 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02400 FAA STC ST00717WI BOEING 737-200 SERIES
BOEING 737-500
BOEING B737-300
BOEING B737-400
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.
Approval of this type design applies only to
Boeing 747 series aircraft when:1. Provisions
for this SATCOM installation have been
installed and approved in accordance with this
STC, or2. Provisions for this SATCOM
installation have been installed and
Installation of the Honeywell Mark II ACARS Compatibility of this design change with
previously approved modifications must be
determined by the installer.If the holder agrees
to permit another person to use this certificate
to alter the product, the holder shall give the
other person written eviden
10016195 HONEYWELL INTERNATIONAL Inc. EASA.IM.A.S.02433 FAA STC ST00361LA GULFSTREAM IV Installation of the Honeywell HUD-2020 Head Prior to installation of this modification the
up Display System on Gulfstream G-IV aircraft installer must determine that the
for Category II approach criteria.
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product.
10016402 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.02731 FAA STC ST00381SE BOEING 757 Installation of Enhanced Ground Proximity 1. Approval of this change in type design
Warning System in B-757 Series
applies to the above model aircraft equipped
Aircraft.Approval applies to aircraft equipped with either a flight management system (FMS),
with a flight management system, which meets which meets AC90-45A, or an EGPWS with a
AC90-45A, or an EGPWS with a GPS based global positioning system (GPS) based
navigation system or an EGPWS equipped
with an inter
navigation system or an EGPWS equipped wi
10028540 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.03210 BOEING 747-400
BOEING 747-400F
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21.12.2006
10.04.2007
21.05.2007
18.02.2009
11.04.2008
16.07.2009