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>7241 AEROLITE GmbH <strong>EASA</strong>.R.S.<strong>01</strong>429 REV. 2 AB139, AW139 EMS Kit Light Lateral Stretcher P/N139127- None The approval holder shall fulfill the 30.08.2<strong>01</strong>1<br />
5<strong>01</strong> Note: this STC is issued for the purpose of<br />
obligations of Part 21,<br />
transferring STC No.10<strong>01</strong>7241 Rev. 1 and<br />
Paragraph21A.118A. Prior to installation<br />
AFM approval 10029997 of Aerolite AG to the<br />
of this modification it must be determined<br />
aboveidentified new holder.<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
rep<br />
10<strong>01</strong>7280 AEROLITE GmbH <strong>EASA</strong>.R.S.<strong>01</strong>528 REV. 4 MBB-BK 117 C-2 Stylence Package (VIP Kit) Aerolite P/N When the Cargo Separation Wall is installed Prior to installation of this modification it 02.03.2<strong>01</strong>2<br />
145305-5<strong>01</strong>/-502 (Revision<br />
the original BK117 C-2 smokedetector kit must must be determined thatthe<br />
to<strong>EASA</strong>.R.S.<strong>01</strong>528)Passenger Seat<br />
be installed in the cargo compartment.When interrelationship between this modification<br />
Modification P/N 021376-502, Curtain Inst. P/N operating the rotorcraft with the doors open or and any other previouslyinstalled<br />
145319-502and Finishing P/N 145302-506/- removed, thelimitations given in Flight Manual modification and/ or repair will introduce<br />
507<br />
Supplement No. FMS 9.1-2 mus<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10033323 AEROLITE GmbH REV. 1 429 EMS Equipment P/N 429020-5<strong>01</strong>/-502This<br />
STC revision introduces the new EMS<br />
Equipment P/N 429020-502.In addition the<br />
following modifications to the existing EMS<br />
EquipmentP/N 429020-5<strong>01</strong> are covered by this<br />
change:- Introduction of Cargo Platform P/N<br />
429022-50<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product<br />
24.05.2<strong>01</strong>1<br />
10036324 AEROLITE GmbH AB 139, AW 139 EMS Equipment P/N 139250-5<strong>01</strong> none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
31.08.2<strong>01</strong>1<br />
10037576 AEROLITE GmbH REV. 1 AW109SP EMS Equipment with Floor Modification, EMS<br />
Gas, PAX/Med Seats,Stretcher, and Cabinet<br />
Installations in accordance with<br />
AeroliteConfiguration Matrix Drawing No. 109-<br />
0002060<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
22.05.2<strong>01</strong>2<br />
10039929 AEROLITE GmbH AW109SP EMS Equipment P/N 109-0008662-5<strong>01</strong> None. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>01</strong>.06.2<strong>01</strong>2<br />
10<strong>04</strong>2079 AEROLITE GmbH AW139 "EMS Equipment P/N 139-00<strong>04</strong>728-5<strong>01</strong>". None. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
06.11.2<strong>01</strong>2<br />
10<strong>01</strong>4816 AEROLITE MAX BUCHER AG <strong>EASA</strong>.A.S.03024 BOMBARDIER CL-600-2B16 (6<strong>04</strong>) 3rd Stretcher and Cargo Platform. P/N 6<strong>04</strong>489- S/N: 5529/5530/5540<br />
5<strong>01</strong><br />
20.06.2007<br />
10<strong>01</strong>4983 AEROLITE MAX BUCHER AG <strong>EASA</strong>.A.S.03275 MD-11 Modification of two SICMA Mono F/C Seat It is the responsibility of the installer to make<br />
16.11.2007<br />
Type 17<strong>01</strong>1(X)1-(XX) as detailed in Lufthansa sure that this installation is certified for the use<br />
Supplemental Type Definition Document STDD in effective aircraft.Compliance with the<br />
25-05/32 R02 and in accordance with Aerolite following Cabin Safety requirements is not<br />
Bucher Master Document List MDL-06-<strong>01</strong>5 covered by this approval:1. FAR/JAR 25.791<br />
Rev. B for installation in MD-11 MSN48533. Passenger information<br />
10<strong>01</strong>5764 AEROLITE MAX BUCHER AG <strong>EASA</strong>.IM.A.S.<strong>01</strong>800 REV. 2 L35A EMS Equipment InstallationIntroduction of Limited to: S/N: 628, 663 The approval holder shall fulfil the<br />
stretcher configuration P/N Aerolite 250071-<br />
obligations of Part 21,<br />
506 andpower box installation P/N Aerolite<br />
Paragraph21.A109. Prior to installation of<br />
250080-503 into existing EMSconfiguration P/N<br />
this modification it must be determined<br />
Aerolite 250070-5<strong>01</strong><br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repai<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 25/<strong>462</strong><br />
06.<strong>01</strong>.2<strong>01</strong>0
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