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
10039248 ROSEN SUNVISOR SYSTEMS LLC FAA STC SA2367NM CL-600-1A11/-2A12/-2B16/-2B19 Cockpit Sunvisor Installation None Prior to installation of this modification it 20.04.2012
CL-600-2C10/-2D24
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.
10028673 ROSS FRESNO LLB EASA.IM.A.S.03153 CESSNA 441 SERIES 15.07.2009
10032879 ROTORCRAFT SUPPORT, Inc. FAA STC SR01456LA 407 Installation of Concorde RG407 Battery 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
06.12.2010
10017109 ROTORTECH LIMITED EASA.R.S.01085 EUROCOPTER FRANCE EC 155
B1
Compendium Modification. Compilation of 22
individual modifications associated with the
installation of equipment and systems enabling
the transfer of EC 155B1 S/N 6642 from FAA
register (N84AZ) to the UK register (G-NIVA).
10033185 ROW 44, Inc. REV. 1 FAA STC ST02829CH B737-700/-800/-900 Installation of Row 44 Broadband Antenna
System Provisions
10033186 ROW 44, Inc. REV. 2 FAA STC ST02836CH-D B737-700, -800, -900 Installation and activation of a Row 44
Broadband System
1. This STC is applicable to EC155B1 S/N
6642 only2. This STC is approved only for the
product configuration as defined in the
approved design data referred to in the
paragraph "Description". Compatibility with
22.09.2005
other aircraft/engine configurations shall be
The equipment for which these provisions are Prior to installation of this modification it 22.10.2012
intended has not beencertified. Additional must be determined thatthe
approval is required for the installation of interrelationship between this modification
thisequipment and must be evaluated to assure and any other previouslyinstalled
satisfactory compliance withthe applicable modification and/ or repair will introduce
airworthiness standards.
no adverse effectupon the airworthiness
of the product.
- The Row 44 Wireless Broadband System is
intended to provide internetconnection and
email services to the airplane's cabin using
portableelectronic devices (PEDs). Any other
use of this equipment will require a reexamination
of thecertification basis. -
10016327 ROYAL ATLANTIC AVIATION, INC. EASA.IM.A.S.02636 FAA STC SA02636AT CESSNA 441 SERIES Ground Recognition Strobe Light System 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.
10017127 RTE - STH EASA.R.S.01215 REV. 1 AS 355N New pilot/co-pilot manual quick release 1. Limited to the following AS 355 N aircrafts:pyrotechnic
sub-system, P/N JD3448AB00100- S/N 5649, F-GSTH equipped with DGAC-F
A0, for approved HEC devices ref: 01-STH- approved design changes ref. 01-STH-001 or
001 and 01-STH-002 and AAN 24527 01-STH-002-S/N 5543, F-GJAX equipped with
DGAC-F approved design change ref. 01-STH-
001-S/N 5566, G-LINE equipped with CAA-UK
a
10017135 RTE - STH EASA.R.S.01229 AS 332 C1 Installation for Human External Cargo (HEC)
applications
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 also applicable on AS355N when
equipped with EASA.R.S.01366.
10017165 RTE - STH EASA.R.S.01273 DGAC-F TC N° 168 AS 355 N Personnel transport aboard hooked baskets as
rotorcraft-load combinations for human external
cargo (HEC).
10017210 RTE - STH EASA.R.S.01366 DGAC FRANCE STC FAM
AS 355 N Helicopter equipped with ARRIUS 1A modified • Engine operating limitations as defined in
98STH0595
namedARRIUS 1E.DGAC-F approved design the “Installation Manual” reference X319 HS
change 98STH0595 relates toinstallation of two 0011.• Engine maintenance requirements
modified ARRIUS 1A engines on the AS355N defined in Manuel d’entretien Turbomoteur
helicopter. This installation allows increased
engine performance required to perform
GBF 124.
Prior to installation of this modification it 08.11.2012
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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