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 />
10038498 ALPINE AVIATION, L.L.C. FAA STC SA0<strong>04</strong>69NY 1- G36<br />
Installation of Main Landing Gear Auxiliary None. Prior to installation of this modification it 21.02.2<strong>01</strong>2<br />
2- 33, 35, 36<br />
Landing Lights in accordancewith FAA STC<br />
must be determined thatthe<br />
SA0<strong>04</strong>69NYInstallation of Main landing Fear<br />
interrelationship between this modification<br />
Auxiliary Landing Lights in accordancewith<br />
and any other previouslyinstalled<br />
Alpine Aviation, Inc. Installation Manual, Report<br />
modification and/ or repair will introduce<br />
No. <strong>01</strong>4, datedJune 14, 1996.<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>6940 ALTAIR AVIONICS CORPORATION <strong>EASA</strong>.IM.R.S.<strong>01</strong>332 FAA STC SR0<strong>01</strong>70BO AGUSTA AB-412<br />
BELL 212<br />
BELL 222<br />
BELL 222B<br />
BELL 222U<br />
BELL 412<br />
BELL 412 EP<br />
EUROCOPTER DEUTSCHLAND<br />
BK117 A<br />
EUROCOPTER DEUTSCHLAND<br />
BK117 B<br />
EUROCOPTER DEUTSCHLAND<br />
BK117 C<br />
10038718 ALTITUDE AEROSPACE Inc. TCCA STC SA11-43 DHC-8-2<strong>01</strong>/-202 Installation of an Oven and a Coffee Brewer in<br />
the GalleyTCCA STC SA11-43, Issue 1<br />
Monitoring System "Altair Avionics SmartCycle" This STC supersedes <strong>EASA</strong> STC 20<strong>04</strong>-1554<br />
by adding model Bell 412 EP to the<br />
applicability list.<br />
10032055 ALTITUDE AEROSPACE INTERIORS Ltd. REV. 1 B747-400 Installation of Honeywell / Racal MSC6000<br />
SatCom System per AltitudeAerospace<br />
Interiors Master Data List MDL 220<strong>01</strong>052 Rev.<br />
B<br />
10032069 ALTITUDE AEROSPACE INTERIORS Ltd. B747-400 Refurbishment of the B747-400 Upper and<br />
Main deck interior installationand seating<br />
configuration in accordance with Altitude<br />
AerospaceInteriors Master Data List MDL<br />
220<strong>01</strong>038 Rev. A or later EAWSA<br />
approvedrevision.<br />
10028359 AMAC AEROSPACE SWITZERLAND AG P-<strong>EASA</strong>.A.S.03791 REV. 1 A320 Humidification and Zonal Dryer System<br />
Installation(see project description document<br />
PD-AA32<strong>01</strong>-2100)<br />
10028365 AMAC AEROSPACE SWITZERLAND AG P-<strong>EASA</strong>.A.S.03792 REV. 1 A320-232 Interior Outfitting(see project description<br />
document PD-AA<strong>01</strong>-2500-1) The limitation for<br />
use of Supplemental Water Tanks has been<br />
removed atRev. 1 of <strong>EASA</strong> STC 10028365.<br />
10032<strong>04</strong>3 AMAC AEROSPACE SWITZERLAND AG A319-133CJ MSN4114 Interior Outfitting.The change<br />
consists in a complete cabin interior outfitting<br />
with a 28passenger VIP interior including two<br />
medical stretcher units.<br />
18.05.2007<br />
Galley PN H82530009 only 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 />
09.03.2<strong>01</strong>2<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 />
15.11.2<strong>01</strong>0<br />
This STC is applicable to A/C Serial Numbers Prior to installation of this modification it 06.10.2<strong>01</strong>0<br />
24855, 24896, 24957, 25605,26910, 27602 must be determined thatthe<br />
and 29375. Several parts installed with this interrelationship between this modification<br />
STC deviate from Part 21A.8<strong>04</strong>regarding EPA and any other previouslyinstalled<br />
marking. The responsible NAA grant a 14.4 modification and/ or repair will introduce<br />
exemptions toaccept the aircraft on its r no adverse effectupon the airworthiness<br />
of the product.<br />
According to doc. No ICA-A32<strong>01</strong>-2100 as Prior to installation of this modification it <strong>04</strong>.03.2<strong>01</strong>0<br />
listed under associated technicaldocumentation 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 />
Restricted to MSN 3379 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 />
08.<strong>01</strong>.2<strong>01</strong>0<br />
MSN 4114 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 />
05.10.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 71/<strong>462</strong>
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