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
10016300 HOLLINGSEAD INTERNATIONAL EASA.IM.A.S.02597 FAA STC ST02147LA BOEING 777-200 SERIES Installation of B/E Aerospace air Chiller P/N Applicable only to A/C with C&D Zodiac pantry
18.06.2008
470-1
installation P/N C801001-101 and C801001-
103 covered by FAA STC ST02144LA and
EASA STC P-EASA.A.S.02421.
10016499 HOLLINGSEAD INTERNATIONAL EASA.IM.A.S.02861 FAA STC 01835LA BOEING 767-200
BOEING 767-300
10015343 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.00442 REV 3 FAA STC ST00705SE BOEING 747-400, 747-200 Installation of the Enhanced Ground Proximity
Warning System on a Boeing 747-200/-400
aircraft.
10015348 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.00498 FAA STC ST01124SE BOEING 747-400 SERIES Installation of the Flight Data Acquisition
Management System
10015371 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01014 REV 1 SEE STC LIST Installation of Honeywell TFE731-3D-1H or
TFE731-3DR-1H Turbofan Engines.
10015377 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01051 REV 1 FAA STC NO ST02005CH-D LEARJET 55 Installation of Honeywell N1 Digital Electronic
Engine Control (DEEC)Note: This revision
reflects the transfer of STC
EASA.IM.A.S.01051 from Garrett Aviation
Services to Honeywell International Inc.
10015462 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01209 FAA STC ST01298AT BOEING 767-200 SERIES
BOEING 767-300 SERIES
Installation of mounting provisions and electrical Prior to installation of this modification the
provisions for electronic flight bags.
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.
Installation of Flight Data Aquistion &
Management System (FDAMS) with Mark II
Aircraft Communication & Reporting System
1This 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.For Boeing B747-2001.
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
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. Pitch & Roll Attitude is sampled one per
second.2. Pneumatic power is sampled once
every 4 seconds.
10015491 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01253 FAA STC ST00961AT BOEING 757-200 SERIES
(ACARS)
Installation of Flight Data Acquisition and
Management System (FDAMS), FAA STC
ST00961AT.
10015547 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01438 FAA STC SA3122SO BOEING 747 Honeywell International Inc. of Redmond, 1. Refer to Approval Report IVW/LTB/TCP-
Washington, USA has applied for an STC to 05.5330542. This STC is approved only for
cover the installation of a CAS81 Traffic the product configuration as defined in the
Collision Avoidance System (TCAS) II with dual approved design data referred to in the
TRA-67 Mode S transponders on Boeing 747- paragraph "Description". Compatibility with
100/200/SP Series aircraft. The FAA has iss other aircraft/engine configurations sha
10015572 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01479 FAA STC SA00842WI-D BEECH 1900D Installation of the Honeywell Mark VI Enhanced AFMS 006-00875-0000 is required on-board
Grounfd Proximity Warning System
for operation with Beech 1900 D series
10015575 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01485 FAA STC SA2726SO DC-9-80 (MD-80) SERIES Installation of CAS-81 TCAS II SystemFAA
STC SA2726SO
10015685 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01670 FAA STC SA01116WI-D PILATUS PC-12/45 Single or Dual Altimeters (FAA STC
SA01116WI-D)
10015686 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01671 FAA STC SA01253WI-D PILATUS PC-12/45 RVSM (FAA STC SA01253WI-D issue dated PC-12/45: MSN 101 to 835 (except MSN
20/02/2007)
545)PC-12/47: MSN 684 to 835
10015745 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01776 FAA STC ST00491SE BOEING DC-9-81 (MD-81) FAA STC ST00491SE "Installation of the
BOEING DC-9-82 (MD-82)
BOEING DC-9-83 (MD-83)
BOEING DC-9-87 (MD-87)
BOEING MD-90-30
Enhanced Ground Proximity Warning System"
10015756 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01790 ST01619SE BOEING 747-400 Introduction of Honeywell International Inc.
Main/Nose Wheel pn. 2615901-1 and Carbon
Brake pn. 2615902-1 in accordance with
Honeywell Service Bulletin 2615901-32-
001_2615902-32-001 Revision New or later
FAA-approved revision as replacement for
Goodrich Br
10015805 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01870 FAA STC ST00705SE BOEING 747-100
Installation of Honeywell Enhanced Ground
BOEING 747-100F
BOEING 747-300
BOEING 747-SP
Proximity Warning System (EGPWS).
10015806 HONEYWELL INTERNATIONAL INC. EASA.IM.A.S.01871 FAA STC ST00140AT AIRBUS A310-200
Installation of MUA-45 Data Link System in
AIRBUS A310-300
Airbus A310-200 / -300 series aircraft.
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