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 />
10034119 ROEDER PRAEZISION GMBH PIPER PA-31-350 Provision for Camera Installation. None. This STC includes only the structural<br />
changes and the electrical powerbox. It<br />
does not include any installation of<br />
Equipment (e.g.Laserscanner, Computer,<br />
Cameras).Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship be<br />
08.03.2<strong>01</strong>1<br />
10039546 ROEDER PRAEZISION GMBH TU206F Installation of an additional Alternator with<br />
Battery for MissionPurposes<br />
10039554 ROEDER PRAEZISION GMBH 172S Installation of provision for the installation of a<br />
camera in the lowerfuselage as described in<br />
description document 14576DE 5300 10 00D.<br />
10<strong>01</strong>5845 ROSE UPHOLSTERY, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>945 SA1<strong>01</strong>88SC BAE JETSTREAM 32<strong>01</strong> Cabin Reconfiguration - 12 Passenger<br />
Executive Interior<br />
10<strong>01</strong>5376 ROSEMOUNT AEROSPACE, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong><strong>04</strong>9 FAA STC ST02175CH BOEING 747-400 Installation of Rosemount Aerospace 8400M<br />
Series Cockpit Door Surveillance System<br />
10<strong>01</strong>5857 ROSEMOUNT AEROSPACE, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>961 FAA STC ST00971SE-D BOEING 737-300<br />
BOEING 737-400<br />
BOEING 737-500<br />
10<strong>01</strong>5899 ROSEMOUNT AEROSPACE, Inc. <strong>EASA</strong>.IM.A.S.02020 FAA STC ST02368CH BOEING 737-300<br />
BOEING 737-400<br />
BOEING 737-500<br />
BOEING 737-600<br />
BOEING 737-700<br />
BOEING 737-800<br />
BOEING 737-900<br />
10<strong>01</strong>6410 ROSEMOUNT AEROSPACE, Inc. <strong>EASA</strong>.IM.A.S.02742 REV. 3 FAA STC ST02649CH A319-111/-112/-113/-114/-115<br />
A319-131/-132/-133<br />
A320-111/-211/-212/-214<br />
A320-231/-232/-233<br />
A321-111/-112/-131<br />
A321-211/-212/-213/-231/-232<br />
Installation of the Rosemount Aerospace<br />
Coockpit Door Surveillance system (CDSS).<br />
Installation of Rosemount Aerospace Cockpit<br />
Door Surveillance System (CDSS) in<br />
accordance with Rosemount Aerospace MDL,<br />
Doc No. D06400594, Revision B, dated<br />
December 29, 2006, or later <strong>EASA</strong> approved<br />
revision.<br />
Installation of Rosemount Aerospace 8700C2-<br />
4 Laptop Docking Station -Electronic Flight Bag<br />
(EFB) System Provisions.A319/ A320 / A321<br />
Series 8700C2-4 Laptop Docking Station<br />
(LDS) -Electronic Flight Bag (EFB) System<br />
Provisions. Revision of the <strong>EASA</strong> STC 10<strong>01</strong>6<br />
10<strong>01</strong>6424 ROSEMOUNT AEROSPACE, Inc. <strong>EASA</strong>.IM.A.S.02762 FAA STC ST02712CH BOEING 747-400 Installation of Rosemount Aerospace 8700C2-<br />
6 Series Laptop Docking Station (LDS) -<br />
Electronic Flight Bag (EFB) Systems<br />
Provisions in accordance with Rosemount<br />
Aerospace Master Data List, Doc. No.<br />
D06402649 Revision C, dated April 3, 2009 or<br />
10<strong>01</strong>6617 ROSEMOUNT AEROSPACE, Inc. <strong>EASA</strong>.IM.A.S.03<strong>04</strong>4 REV. 2 FAA STC ST02675CH A340-211, -212, -213<br />
A340-311, -312, -313<br />
A340-541, -642<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 />
10.05.2<strong>01</strong>2<br />
Installer must check availability of <strong>EASA</strong>-<br />
approval for one or morereferenced STC when<br />
airplane is modified per that / those<br />
STC(s).This STC is limited to S/N<br />
172S8186.This STC provides instructions only<br />
for the installation of theprovision for a camera.<br />
Fu<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
- Compatibility of this design change with other<br />
previously approved modifications must be<br />
determined by the installer.- In accordance with<br />
Flight Manual Supplement, Rosemount<br />
Aerospace Doc No D0640<strong>01</strong>84, Rev A, FAA<br />
approved January 4th, 2007, or later ap<br />
The installation of this modification by 10.05.2<strong>01</strong>2<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
disposal of the approvedappropriate<br />
documentation. Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
11.<strong>04</strong>.2006<br />
06.10.2005<br />
20.<strong>04</strong>.2006<br />
06.02.2007<br />
Not applicable 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 />
18.11.2<strong>01</strong>0<br />
1. FAA approved Airplane Flight Manual<br />
Supplement, Rosemount Aerospace Doc. No.<br />
D06402687, Revision A, approved April 2,<br />
2009 orlater FAA approved revision, is required<br />
on board of the modified aircraft.2. This<br />
installation approval does not include<br />
23.<strong>04</strong>.2009<br />
later FAA appro<br />
Installation of Rosemount Aerospace 8700C2- This installation approval does not cover the Prior to installation of this modification it 26.08.2<strong>01</strong>0<br />
3 Laptop Docking Station -Electronic Flight Bag Electronic Flight Bagcomputers, only the must be determined thatthe<br />
(EFB) System Provisions Revision of the <strong>EASA</strong> Electronic Flight Bag mounting and wiring. interrelationship between this modification<br />
STC 10<strong>01</strong>6617, Rev. 1 to remove EWIS Theoperational approval of the Electronic Flight and any other previouslyinstalled<br />
Limitation<br />
Bag computers shouldfollow the guidance in modification and/ or repair will introduce<br />
the Temporary Guidance Leaflet TGL no adverse effectupon the airworthiness<br />
of the product<br />
10<strong>01</strong>6655 ROSEMOUNT AEROSPACE, Inc. <strong>EASA</strong>.IM.A.S.031<strong>04</strong> BOEING MD 11F Installation of Rosemount Aerospace 8700C2- 1) Prior to installation of this modification the<br />
8 Series Laptop Docking Station (LDS) - installer must determine that the<br />
Electronic Flight Bag (EFB) System Provisions interrelationship between this modification<br />
inaccordance with Rosemount Aerospace andany other previously installed modification<br />
Master Data List, Doc. No. D06403165, will introduce no adverse effect upon the<br />
Revision D, dated April 3, 2009 or later FAA<br />
approv<br />
airworthiness of the product.2) FAA app<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 374/<strong>462</strong><br />
10.06.2009
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