04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<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>04</strong>0513 ARMSTRONG AEROSPACE Inc. FAA STC ST03<strong>04</strong>7CH B747-400 Certification of Compatibility with Cellular and This STC may only be applied to an aircraft Prior to installation of this modification it 06.07.2<strong>01</strong>2<br />
Wireless DataTechnologies in accordance with when an airplane installedbase station using must be determined thatthe<br />
Armstrong Aerospace Master Data List,Doc. the cellular technologies is concurrently interrelationship between this modification<br />
No. DC1<strong>04</strong>-9026-00 Revision C, dated June installedin accordance <strong>EASA</strong> Form 96 Post-TC and any other previouslyinstalled<br />
28, 2<strong>01</strong>2 or later approvedrevision.Validation of Technical Visa <strong>Page</strong> 4/5 Issue 4,<strong>01</strong>/05/2<strong>01</strong>0 modification and/ or repair will introduce<br />
FAA STC ST03<strong>04</strong>7CH<br />
with a separate approval.This STC does no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>1316 ARMSTRONG AEROSPACE Inc. FAA STC ST03086CH B747-400 Installation and activation of a Panasonic None Modification of the aircraft in accordance 06.09.2<strong>01</strong>2<br />
Global Communication Suite(GCS) System in<br />
with this STC requires prioror concurrent<br />
accordance with Armstrong Aerospace Master<br />
modifications in accordance with FAA<br />
Data ListDoc. No. DC 1<strong>04</strong>-9034-00 Revision D,<br />
STC’s ST03<strong>04</strong>7CH andST03085CH. The<br />
dated May 14, 2<strong>01</strong>2 or later FAAapproved<br />
Panasonic eXPhone system equipment<br />
revisionValidation of FAA STC ST03086CH<br />
for which certain provisions inthis<br />
modification are intended has<br />
10<strong>04</strong>2211 ARMSTRONG AEROSPACE Inc. FAA STC ST02314CH A319-131, A319-133<br />
A320-232, A321-232<br />
10<strong>04</strong>2212 ARMSTRONG AEROSPACE Inc. FAA STC ST02314CH A319-111,-112,-113,-114,-115<br />
A319-131,-132,-133<br />
A320-111,-211,-212,-214,-231<br />
A320-232,-233<br />
A321-231,-232<br />
10<strong>01</strong>6057 AS&T AEROSPACE SYSTEM &<br />
TECHNOLOGIE<br />
10<strong>01</strong>6058 AS&T AEROSPACE SYSTEM &<br />
TECHNOLOGIE<br />
10<strong>01</strong>6257 AS&T AEROSPACE SYSTEM &<br />
TECHNOLOGIE<br />
<strong>EASA</strong>.IM.A.S.02234 FAA STC SA755GL CESSNA 206H<br />
CESSNA T206H<br />
CESSNA TU206G<br />
CESSNA U206F<br />
CESSNA U206G<br />
<strong>EASA</strong>.IM.A.S.02235 FAA STC SA<strong>01</strong>338WI CESSNA 182P<br />
CESSNA 182Q<br />
CESSNA 182R<br />
CESSNA 182S<br />
CESSNA 182T<br />
CESSNA R182<br />
CESSNA T182<br />
CESSNA TR182<br />
<strong>EASA</strong>.IM.A.S.02535 FAA STC SA<strong>01</strong>328WI PIPER PA-32-3<strong>01</strong>FT (PIPER 6X)<br />
PIPER PA-32-3<strong>01</strong>XTC (PIPER<br />
6XT)<br />
PIPER PA-32R-3<strong>01</strong><br />
PIPER PA-32R-3<strong>01</strong>T<br />
<strong>EASA</strong> validation of FAA STC ST02377CH<br />
"Installation of a Rockwell CollinsTailwind 560<br />
Satellite System and modification of a Thales<br />
Top Seriesi3000/i4000 In flight Entertainment<br />
(IFE) System"<br />
<strong>EASA</strong> validation of FAA STC ST02314CH<br />
"Installation of an Aft Cargo BayEquipment<br />
Rack"<br />
Installation of TKS Ice Protection Systems<br />
Components on a no-hazard / no credit basis.<br />
Installation of TKS Ice Protection Systems<br />
Components on a no-hazard / no credit basis<br />
Installation of TKS Ice Protection Systems<br />
Components on no-hazard / no credit basis.<br />
10031933 ASI INNOVATION T206H ASI-fam-0009-<strong>01</strong> Installation of FLIR MX10<br />
mechanical provision on T206Haircraft<br />
100329<strong>04</strong> ASI INNOVATION F406 ASI-FAM-0<strong>01</strong>5-02 Provision installation of<br />
console PMR/DMR and UHFantenna<br />
- The FAA STC ST02314CH validated through<br />
<strong>EASA</strong> STC Approval 10<strong>04</strong>2211 forAft Cargo<br />
Bay Equipment Rack Installation must be<br />
installed on aircraftprior or in conjunction with<br />
this STC design change.<br />
Prior to installation of this modification it 15.11.2<strong>01</strong>2<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 />
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>2<br />
1. This installation is not approved for flight into<br />
known icing conditions.2. A placard must be<br />
fitted on the upper control panel in front of the<br />
pilot, stating “FLIGHT INTO KNOWN ICING<br />
CONDITIONS IS PROHIBITED”. 3. This<br />
installation is approved on a no-h<br />
1. This installation is not approved for flight into<br />
known icing conditions.2. A placard must be<br />
fitted on the upper control panel in front of the<br />
pilot, stating "FLIGHTINTO KNOWN ICING<br />
CONDITIONS IS PROHIBITED".3. Applicable<br />
serial numbers: 182P: S/N 1826<br />
1. This installation is not approved for flight into<br />
known icing conditions.2. A placard must be<br />
fitted on the upper control panel in front of the<br />
pilot, stating “FLIGHT INTO KNOWN ICING<br />
CONDITIONS IS PROHIBITED”.3. This<br />
installation is approved on a no-ha<br />
Limitation to Cessna T206H serial number 445<br />
and 446<br />
Limited to: F406 S/N 006-<strong>01</strong>7-025-039-<strong>04</strong>2-<br />
070-074-075-077-086<br />
<strong>04</strong>.<strong>01</strong>.2007<br />
08.12.2006<br />
27.08.2007<br />
Prior to installation of this modification it 23.09.2<strong>01</strong>0<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 />
Prior to installation of this modification it 07.12.2<strong>01</strong>0<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>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 83/<strong>462</strong>
Change language