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
10035929 LIBERTY AEROSPACE INC. FAA STC SA03488AT XL-2 S-TEC system 30 autopilot installation on Option 1: Chippewa Aerospace Inc Document Prior to installation of this modification it 28.07.2011
Liberty XL-2 series inaccordance with the XL2-2210-01-0002 Rev IR, datedJune 18, must be determined thatthe
following:Option 1 (for use with S-Tec Model 2007, or later FAA approved revision - interrelationship between this modification
ST-901 GPS Steering Converter
Instructions forContinued Airworthiness and any other previouslyinstalled
Unit):Chippewa Aerospace Master Data List (ICA).Option 2: Liberty Aerospace Document modification and/or repair will introduce
(MDL) n° XL2-2210-01-0001, revision4, dated 135A-970-110, rev D. dated July 19,2010, or no adverse effectupon the airworthiness
November 20
lat
of the product.Option 2
10015453 LIFEPORT, Inc. EASA.IM.A.S.01198 FAA STC SA01093SE CESSNA 525
CESSNA 525A
Installation and inspection of emergency
medical stretcher and base, oxygen system in
accordance with FAA STC SA01093SE or
later EASA approved revision.
10015454 LIFEPORT, Inc. EASA.IM.A.S.01199 FAA STC ST00909SE LEARJET 45 Installation of emergency medical stretchers
and bases, oxygen and electrical systems and
associated Lifeport Inc. Report No. EGR-644-
12 Revision IR dated November 6 2000 &
Master Drawing List EGR-644-00 revision R
dated 25 April 2001 or later approved rev
10015551 LIFEPORT, Inc. EASA.IM.A.S.01445 FAA STC SA00273WI BEECH 100
BEECH 200
BEECH 300
BEECH 65-90
BEECH 65-A90
BEECH B90
BEECH C90
BEECH C90 A
BEECH E90
BEECH F90
Installation of a Patient Loading and Utility
System (PLUS)
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.
Modification must be used with AFMS 35 for
Lifeport PLUS
10015614 LIFEPORT, Inc. EASA.IM.A.S.01553 REV. 1 FAA STC ST01780LA CESSNA 560 XL Installation of a Patient Loading and Utility Ref. AFM Supplement EGR-777-11, Revision
System (PLUS) inaccordance with FAA STC A, dated June 24, 2005, or later FAA approved
ST01780LA or later EASA approved revision
Note: Revision 1 issued to correct a type in the
Original STC number.
revision
10015646 LIFEPORT, INC. EASA.IM.A.S.01619 FAA STC SA00635SE 208 208A 208B Installation of a Patient Loading and Utility
System (PLUS) in accordance with FAA STC
SA00635SE or later EASA approved revision.
1. Airplane Flight Manual supplement EGR-571-
11, Revision A, dated January 11, 2002, or
later FAA approved revision.
10016288 LIFEPORT, Inc. EASA.IM.A.S.02583 FAA STC SA02060LA BEECH 1900D Emergency Medical System The installer of this STC must ensure that, if
the life vests have been removed with the
seats, a life vest for the occupant of thelitter
system is installed and available to the
occupant.
10016483 LIFEPORT, Inc. EASA.IM.A.S.02837 FAA STC ST02119LA CESSNA 750 CITATION X Emergency Medical 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. The install
10016489 LIFEPORT, Inc. EASA.IM.A.S.02845 FAA STC SA00096LA BAE 125 SERIES 1000A
BAE 125 SERIES 1000B
BAE 125 SERIES 800A
BAE 125 SERIES 800B
HAWKER 1000
HAWKER 800
HAWKER 800 XP
HAWKER HS 125-700A
10016492 LIFEPORT, Inc. EASA.IM.A.S.02854 FAA STC ST00154SE CESSNA 500
CESSNA 550
CESSNA 560
CESSNA S550
10016578 LIFEPORT, Inc. EASA.IM.A.S.02977 REV. 1 FAA STC SA00528SE PA-31, PA-31-300, PA-31-350,
PA-31P, PA-31T, PA-31T1,
PA-31T2, PA-31T3, PA-31P-350,
PA-42, PA-42-1000
Installation of a Patient Loading and Utility
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. The install
Emergency Medical 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. The install
Emergency Medical System (The Emergency
Medical System attaches only to the existing
aircraft seat tracks. The system will be a free
standing unit that can be rapidly installed and
removed from the cabin).
13.02.2007
21.06.2005
19.09.2005
24.07.2009
16.02.2006
04.10.2007
30.07.2008
30.07.2008
27.08.2008
None. None. 30.04.2010
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