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
10015850 STAR AVIATION Inc. EASA.IM.A.S.01950 ST02989AT CESSNA 500
The modification will consist of a composite
12.05.2006
CESSNA 501
structure with a metal faceplate wich will be
CESSNA 550
fitted over the center of the existing
CESSNA 551
Glareshield. An area of the existing glareshield
CESSNA S550
will be removed to allow for wires to be routed
to the annunciators and switc
10036456 STAR AVIATION Inc. P-
EASA.IM.A.S.00285
REV. 1 FAA STC ST02861AT B747-400 Installation of Connexion by Boeing Next
Generation Antenna and SateliteData System
in accordance with Star Aviation Inc. Master
Data ListR44-0163, Revision CP, Dated May
12, 2011 or later approved revision
10041648 STAR AVIATION Inc. EASA.IM.A.S.00286 REV. 1 FAA STC ST02942AT 747-400 Installation of Cabin Wireless Local Area
Network (CWLAN) in accordancewith Star
Aviation Inc. Master Data List R44-0175,
Revision G, datedOctober 13, 2004, or later
FAA approved revisions and
Provisionalinstallation of a Panasonic Avionics
Corporation eXP
10016830 STARFLEX L.L.C. EASA.IM.R.S.01201 FAA STC SH7962SW-D EUROCOPTER FRANCE AS
355F2
Installation of two Allison 250-C20R engines
and enhanced anti-torque system in
accordance with AHC drawing list 355A82-
1755 Revision D dated November 5, 1990 or
later FAA approved revision
10016832 STARFLEX L.L.C. EASA.IM.R.S.01203 SH7961SW-D Installation of two Allison 250-C20R engines in
accordance with AHC drawing list 355A82-
1753 Revision H dated November 5, 1990 or
later FAA approved revision
10035635 STARFLEX L.L.C. AS 355 F1, AS 355 F2 Compliance of C20R installation with BCAR
10035081 STC ACQUISITION, LLC FAA STC ST01567LA G-1159 (GULFSTREAM II)
G-1159A (GULFSTREAM III)
G-1159B (GULFSTREAM IIB)
Section G and confirmation ofability of C20R to
fly one engine inoperative profiles.
Installation of a pylon mounted ejector system
with new design thrustreversers, to show
compliance with ICAO Annex 16, Volume 1,
Amendment 9,Chapter 3 noise requirements.
None Aircraft Flight Manual Supplement R44-
0300 Rev. IR dated October 16,2004 is a
required part of this STC.Instruction for
Continued Airworthiness Star Aviation
Document No #R44-0273, Rev. D, dated
June 20, 2011 must be made available to
theoperator at the ti
None AFM Supplement R44-0293, Revision A,
dated October 18, 2004 shall be onboard
the modified aircraftInstructions for
Continued Airworthiness Document #
R44-0182 Rev. IRdate June 16, 2004,
Document # R44-290, Rev. IR dated July
15, 2004 andDocument # R44-0427
1. The present STC is the validation of the FAA
STC SH7962SW-D, last amended on 01
February 2006.2. Compatibility of this
modification with previously approved
modifications of the aircraft must be
determined by the installer.
1. The present STC is the validation of the FAA
STC SH7961SW-D, last amended on 01
February 2006.2. Compatibility of this
modification with previously approved
modifications of the aircraft must be
determined by the installer.
none When fitted with STC
EASA.IM.R.S.01203, the AS355F1 is
certificated asGroup A under BCAR
Section G ("Equivalent to Category A" in
accordancewith JAR OPS 3, ACJ OPS
3.480 (a)(1)&(a)(2)) when the
followingconditions are met (as listed in
Model G-1159, (Gulfstream II)1),,Aircraft
without Aircraft Service Change (ASC) 81,
“62,500 PoundIncreased Gross Weight
Modifications, or those with a Maximum
(ramp)weight less than 62,500 lb are not
eligible for this modification.2),,Aircraft with
ASC 200
09.09.2011
23.10.2012
16.01.2007
16.01.2007
06.07.2011
the TCDS EASA.R.146)
Prior to installation of this modification it 24.05.2011
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.
10014128 STC TWENTY ONE LIMITED EASA.A.S.01238 REV 1 DC-9-80 (MD-80) SERIES Introduction of FlightVu Cabin Surveillance
System
21.06.2006
10014129 STC TWENTY ONE LIMITED EASA.A.S.01239 BOEING 757-200 Introduction of SSR Mode S Enhanced
Surveillance
30.05.2005
10014131 STC TWENTY ONE LIMITED EASA.A.S.01241 BAE ATP Rework to Landing Gear Emergency Up-Lock
Release Mechanism
15.11.2005
10014185 STC TWENTY ONE LIMITED EASA.A.S.01323 REV 1 FOKKER F.27 MARK 500
FOKKER F.27 MARK 600
Use of TRA-45A Display Indicator 30.01.2006
10014209 STC TWENTY ONE LIMITED EASA.A.S.01361 REV 1 BAE ATP Introduction of Class E Compartment for LFD
Modified Aircraft.
1. Flight Manual Supplement S21.FMS-0008; 09.04.2008
10014210 STC TWENTY ONE LIMITED EASA.A.S.01362 REV 1 BAE ATP Introduction of Freight Loading & Restraint This major change is limited to embodied into a
09.04.2008
System for LFD Modified Aircraft.
Bae aircraft previously modified for the
installation of a large cargo door at the rear of
the fuselage in accordance with Bae Service
Bulletin ATP-52-036 and with the installation of
a main cabin Class 'E' c
10014211 STC TWENTY ONE LIMITED EASA.A.S.01363 BAE ATP Installation of AAR Freight Loading System This STC may only be embodied into BAe ATP
aircraft previously modified for the installation
of a large cargo door at the rear of the
fuselage, in accordance with British Aerospace
Service Bulletin SBATP-52-036 (Modification
M60138A), with a barrier net in
30.01.2006
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