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
10014640 BOURNEMOUTH AVIATION
EASA.A.S.02789 AEROSPATIALE ATR 42 Indraero Siren Cargo Container System This STC is applicable on the following
29.01.2008
(CONSULTANTS)
AEROSPATIALE ATR 72 installation on ATR42-320 and ATR72-202 aircraft:Those ATR42-320 previously converted
aircraft previously converted to Class E Cargo to Class E Cargo Compartment Freighter by
Compartment Freighter.
the embodiment of the following ATR GIE
Service Bulletins: • ATR42-25-0070
Reinforce all floor panels, and• ATR42-25-
0063
10014697 BOURNEMOUTH AVIATION
EASA.A.S.02864 BOEING 757-200 Installation of B/C LOPA with standing bar
08.03.2007
(CONSULTANTS)
tables
10014863 BOURNEMOUTH AVIATION
EASA.A.S.03087 REV. 4 B747-100, -200B/C/F, -300, STC EASA.A.S.03087: This modification None. Airplane Flight Manual Supplement, FMS- 21.05.2012
(CONSULTANTS)
B747-400, -400F
introduces a Universal CockpitDisplay System
468-38 Rev. 5 or later approvedrevision,
(Electronic Flight Bag) into the aircraft
is required on board the aircraft Prior to
consisting of 2Flight Deck Displays, an
installation of this modification it must be
Application Server Unit, an Accessible
determined thatthe interrelationship
DataUnit, an external video camera and
between this modification and any other
associated wi
previouslyi
10014928 BOURNEMOUTH AVIATION
(CONSULTANTS)
EASA.A.S.03181 BAE 146-200 SSR Mode S Enhanced Surveillance 16.08.2007
10014999 BOURNEMOUTH AVIATION
EASA.A.S.03299 AIRBUS 1-11 TAWS Installation. Prior to installation of this modification the
30.09.2008
(CONSULTANTS)
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. The install
10015001 BOURNEMOUTH AVIATION
(CONSULTANTS)
10015020 BOURNEMOUTH AVIATION
(CONSULTANTS)
10015023 BOURNEMOUTH AVIATION
(CONSULTANTS)
10015048 BOURNEMOUTH AVIATION
(CONSULTANTS)
10015117 BOURNEMOUTH AVIATION
(CONSULTANTS)
10015122 BOURNEMOUTH AVIATION
(CONSULTANTS)
10015290 BOURNEMOUTH AVIATION
(CONSULTANTS)
10017101 BOURNEMOUTH AVIATION
(CONSULTANTS)
EASA.A.S.03301 BAE 146 Installation of VIP LOPA (Inc. Club 4 Layout). 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. The install
EASA.A.S.03326 BOEING 737-500 Layout of Passenger Accommodation. 19.05.2008
EASA.A.S.03329 BOEING 767-300 Layout Passenger Accomodation 17.04.2008
EASA.A.S.03364 BOEING 757 - 200 Installation of revised Passenger
Accommodation
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.The installa
EASA.A.S.03466 BOMBARDIER CL-600-2B16 (604) Installation of Electronic Flight Bag Restricted to ASN 5383 06.06.2008
EASA.A.S.03471 REV. 1 BOEING 737-300 Installation of B1/B2 Power Connector (Engine
Thrust Change).
Prior to embodying this modification the aircraft
must be modified inaccordance with the
applicable Boeing Service Bulletins for the
22000lbs thrust setting with two CFM-56-3B-2
engines installed as listed inBAC/737/091.
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.
EASA.A.S.03825 REV. 1 A320 Installation of 148 PAX Layout of Passenger none Prior to installation of this modification it 12.11.2012
Accommodation (LOPA)This STC is revised in
must be determined thatthe
order to remove the EWIS Limitation
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
EASA.R.S.01071 MD900 Upgrading of existing Single Cargo Hook to
Dual Hook System
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.
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