04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>5688 GULFSTREAM AEROSPACE SERVICES <strong>EASA</strong>.IM.A.S.<strong>01</strong>673 FAA STC ST02229CH-D GULFSTREAM GIV-X Installation of Corporate Aircraft Completion 1. Aircraft Serial Number 4027 only2. This STC<br />
13.03.2006<br />
STC<br />
is approved only for the product configuration<br />
as defined in the approved design data<br />
referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by<br />
10<strong>01</strong>5848 GULFSTREAM AEROSPACE SERVICES <strong>EASA</strong>.IM.A.S.<strong>01</strong>948 ST10308SC-D GULFSTREAM 100<br />
GULFSTREAM 1125 WESATRD<br />
ASTRA<br />
10<strong>01</strong>5856 GULFSTREAM AEROSPACE SERVICES <strong>EASA</strong>.IM.A.S.<strong>01</strong>960 FAA STC NO ST02237CH-D<br />
GULFSTREAM ASTRA/SPX<br />
GULFSTREAM 100<br />
GULFSTREAM ASTRA/SPX<br />
Installation of Dual Universal Avioniks UNS-<br />
1C+ Flight Management Systems. FAA STC<br />
<strong>01</strong>0308SC-D<br />
10<strong>01</strong>4830 H4 AEROSPACE (UK) Ltd. <strong>EASA</strong>.A.S.03<strong>04</strong>5 BOEING B737-800 Installation of a Satcom Antenna for a GSM<br />
system on B737-800<br />
This STC is only applicable to A/C with<br />
previous installed dual Universal Avionik UNS-<br />
1C FMS.<br />
13.07.2006<br />
Installation of a Corporate Aircraft Completion Limited to S/N 158 11.08.2006<br />
in accordance with Gulfstream Master Drawing<br />
List GA122<strong>04</strong>6000, Rev B dated July 19,2006<br />
or later approved revision<br />
As in Instrucions for Continued Airworthiness<br />
H4ADR259 Issue 1 or later <strong>EASA</strong> approved<br />
revision.<br />
10<strong>01</strong>4843 H4 AEROSPACE (UK) Ltd. <strong>EASA</strong>.A.S.03060 Interior Changes for the B/E Aerospace First 1. Instructions for Continued Airworthiness,<br />
Class Seat Integration in the Forward Ref. No. H4ADR238.2. This approval is<br />
Passenger Cabin.This modification removes limited to only the installation made in the<br />
the existing 16 off Weber Business class seats Boeing Model B767-306, Serial Number 30393<br />
and installs 12 B/E Aerospace First Class aircraft.3. Prior to installation of this<br />
Passenger Seats with Ottomans and Sideledg modification the installer must de<br />
10<strong>01</strong>4867 H4 AEROSPACE (UK) Ltd. <strong>EASA</strong>.A.S.03091 BOEING B737-800 Installation of GSM Phone / SATCOM system<br />
on B737-800 aircraft.<br />
1. Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.2.<br />
10<strong>01</strong>4876 H4 AEROSPACE (UK) Ltd. <strong>EASA</strong>.A.S.03103 BOEING 767-300 The cabin reconfiguration of B767-300 Aircraft Continued Airworthiness Manual, Ref. No.<br />
with Brice B1000S seats for TUI<br />
ML3263, Rev. A.This approval is limited to only<br />
ARKEFLY/This modification removes the the installation made in the Boeing Models<br />
existing 260 economy class seats and installs B767-300, S/N 24477, S/N 24847, S/N 24848<br />
260 new Brice B1000s economy class seats in aircraft.<br />
an identical passenger layout.<br />
10<strong>01</strong>4883 H4 AEROSPACE (UK) Ltd. <strong>EASA</strong>.A.S.03111 BOEING 737-500 Implementation of Interior Changes associated<br />
with the cabinreconfiguration from 124YC to<br />
126YC.<br />
Prior to installation of this modification the<br />
installer must determine that<br />
theinterrelationship between this modification<br />
and any other previously installedmodification<br />
will introduce no adverse effect upon the<br />
airworthiness of theproduct.The installatio<br />
10<strong>01</strong>5300 H4 AEROSPACE (UK) Ltd. <strong>EASA</strong>.A.S.03859 AIRBUS A320-232 GUEST/STAFF SEATING AREA<br />
Approval valid only for MSN 2403.The use of<br />
<strong>04</strong>.05.2009<br />
RECONFIGURATION & MISC CABIN ITEMS the aircraft is limited to non-commercial<br />
FOR A320-232 AIRCRAFT as defined in operation only. For other Limitations refer to<br />
H4ACP057.Model: Airbus A320-232 MSN<br />
2403, A6-DLM<br />
Flight Manual Supplement H4AFMS<strong>01</strong>9.<br />
10026811 H4 AEROSPACE (UK) Ltd. P-<strong>EASA</strong>.A.S.03841 BOEING 767-300 Installation of Lifeport Stretcher. None. Prior to installation of this modification the 12.08.2009<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.The installatio<br />
10027495 H4 AEROSPACE (UK) Ltd. REV. 1 B737-800 Introduction of Recaro Economy Passenger None The STC is based upon cabin<br />
09.03.2<strong>01</strong>1<br />
Seats on Boeing 737-800, inaccordance with<br />
installations as approved under<br />
project H4A1239(Revision of STC 10027495<br />
STC<strong>EASA</strong>.A.S.03836. Applicable<br />
to remove EWIS Limitation)<br />
documents must be considered.Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previo<br />
10029103 H4 AEROSPACE (UK) Ltd. REV. 2 A319, A320, A321 Installation of Runway Turnoff and Logo Lights. Restricted to the aircraft listed in doc. N° Prior to installation of this modification it 20.10.2<strong>01</strong>0<br />
Minor Change to <strong>EASA</strong> STC10029103, Rev.1 H4ADR530 - MasterEffectivity List for must be determined thatthe<br />
issue date 31.03.2<strong>01</strong>0 granted to H4<br />
Goodrich RTO and Logo Light Installation. interrelationship between this modification<br />
Aerospace (UK) Ltd.Minor change approval is<br />
and any other previouslyinstalled<br />
sought to reflect the up issue wording of<br />
modification and/ or repair will introduce<br />
theinstructions of continued airworthiness inc<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
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16.<strong>01</strong>.2008<br />
19.06.2007<br />
12.12.2008<br />
14.06.2007<br />
10.06.2008
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