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
10038053 FOKKER SERVICES B.V. F28 MARK 0070 Activation of WLAN functionality of an already -Installation of EASA STC 10027637 is a Prior to installation of this modification it 16.01.2012
installed andcertificated router (ref EASA STC prerequisite for this STC-Limitation of Wireless must be determined thatthe
10027637)The Fokker 70 aircraft contains a Local Area Network as documented in AFM interrelationship between this modification
router that has been certificatedunder STAC changeAFMJET2011-007
and any other previouslyinstalled
10027637. Fokker Services will activate and
modification and/ or repair will introduce
certificate theWLAN functionali
no adverse effectupon the airworthiness
of the product.
10042160 FOKKER SERVICES B.V. B737-600/-700/-800/-900/-900ER Introduction of LED light assembles in the
Boeing B737 NG aircraft
10015713 FOKKER50FREIGHTER STC CORP. EASA.IM.A.S.01710 REV 1 FAA STC ST01916LA FOKKER F.27 MARK 050 Installation of Large Cargo door.Installation of
Large Cargo door.
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.
12.11.2012
1. To allow the carriage of cargo STC
IM.A.S.01711 shall be incorporated;2. The
maximum number of occupants in the aircraft
including crew members is 3;3. This STC is
approved only for the product configuration as
defined in the approved design da
10015714 FOKKER50FREIGHTER STC CORP. EASA.IM.A.S.01710 REV 1 FAA STC STO1916LA - EASA.IM.A. FOKKER F.27 MARK 050 21.05.2008
10015715 FOKKER50FREIGHTER STC CORP. EASA.IM.A.S.01711 REV 1 FAA STC ST00260DE FOKKER F.27 MARK 050 Installation of Class E Cargo Interior,
1. Cargo Loading Manual WB-2052 Rev. C or
02.11.2007
configuration 24B301-211 in accordance with later approved revisions shall be used when
Branson Aircraft Corporation Drawing List loading the aircraft.2. This STC is approved
24A300, revision B dated November 5, 1996, only for the product configuration as defined in
FAA approved November 7, 1996 or later the approved design data referred to in the
revision approved in accordance with ED
Decision
paragraphs "Description" and “As
10028703 FORCED AEROMOTIVE
FAA STC SE10926SC IO-550-N Installation of BAR Air, LLC supercharger The supercharged IO-550-N engine is limited Prior to installation of this modification it 03.02.2010
TECHNOLOGIES
system on Teledyne ContinentalMotors IO-550- to 29.6 in Hg (204 kPa) MAPand 2700 RPM or must be determined thatthe
N Engines in accordance with Master Drawing 310 HP (231 kW).
interrelationship between this modification
ListMDL-SR22-1-E, Revision A, dated April 4,
and any other previouslyinstalled
2008 or later FAA approvedrevision - EASA
modification and/ or repair will introduce
Validation of FAA STC SE10926SC.
no adverse effectupon the airworthiness
of the product If the
10029290 FORCED AEROMOTIVE
TECHNOLOGIES
10029878 FORCED AEROMOTIVE
TECHNOLOGIES
10030005 FORCED AEROMOTIVE
TECHNOLOGIES
FAA STC SA10925SC SR22 Installation of BAR Air, LLC modified Teledyne As referred in limitations section of the AFM-S
Continental MotorsIO-550-N iaw. MDL-SR22-1- 22006Engine must be modified acc. EASA
A, Rev. E or later FAA approved
revisions.Installation requires EASA STC
10028703 to be installed.
STC 10028703
FAA STC SE10233SC O-470-L, -R, -S, -U Installation of a Belt-Driven Vortech V-1S
supercharger assembly on theTeledyne
Continental Motors (TCM) O-470-L, O-470-R,
O-470-S, and O-470-Uengines in accordance
with Type Inspection Data contained in
MasterDrawing List No. MDL-182-1-E, Rev. D,
dated Ja
FAA-STC SE10233SC 182E, 182F, 182G, 182H, 182J,
182K, 182L, 182M, 182N, 182P,
182Q, 182R
The supercharged O-470-L, -R, -S, and -U
engines are limited to 28 inHg(193 kPa) MAP
and 2600 RPM or 230 HP (171.5 kW) with
minimum fuel gradeAvgas 100LL.
Installation of Rod Sage Supercharged This Supplemental Type Certificate requires
Teledyne Continental Motors (TCM)O-470-L, O- installation of EASA STC10029878 (see also
470-R, O-470-S and O-470-U Engines in acc. FAA-STC SE10233SC)
with FAA STCSA10232SC
10033805 FR AVIATION LIMITED B300 Observer Training Platform Mod.-B300. The approval is limited to the Aircraft Serial
Numbers: FL-597,FL-618, FL-629 and
FL-633.
21.05.2008
Prior to installation of this modification the 17.03.2010
installer must determinethat the
interrelationship between this modification
and any otherpreviously installed
modification will introduce no adverse
effect uponthe airworthiness of the
product.The installatio
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 productIf the h
28.04.2010
Prior to installation of this modification it 10.05.2010
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
Prior to installation of this modification the 09.02.2011
installer must determinethat the
,,interrelationship between this
modification and any otherpreviously
installed ,,modification will introduce no
adverse effectupon the airworthiness of
the product. The instal
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