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>01</strong>4187 AERO ENGINEERING DESIGN Ltd <strong>EASA</strong>.A.S.<strong>01</strong>325 MD-80 Aero Engineering Design Modification 34-77-<br />
211. Introduction of Honeywell MK VII EGPWS<br />
25.07.2005<br />
10<strong>01</strong>4188 AERO ENGINEERING DESIGN Ltd <strong>EASA</strong>.A.S.<strong>01</strong>328 MD-80 Aero Engineering Design Modification 34-77-<br />
210.Introductiom of Honeywell RDR-4B<br />
Weather Radar<br />
10<strong>01</strong>6210 AERO MEDICAL PRODUCTS MFG INC. <strong>EASA</strong>.IM.A.S.02456 FAA STC SA1035GL PIPER PA-31<br />
PIPER PA-31-300<br />
PIPER PA-31-325<br />
PIPER PA-31-350<br />
FAA STC SA 1035GL "Aircraft Stretcher 1. Prior to the first flight of each modified<br />
System - Installation of Air Ambulance aircraft, and after each exchange to any of the<br />
Stretcher P/N 125 Kit P/N 800, Medical Communication, Navigational or MedPack<br />
Oxygen System Kit P/N 807 (FAA approved Equipment, a ground EMI test must be<br />
option), Inverter/ Pump Kit P/N 812 in conducted in accordance with EA form 173<br />
accordance with Drawing List Report 0<strong>01</strong> Rev. dated 15-11-1993. A copy of the EA form 17<br />
C or later appro<br />
10029339 AERO MEDICAL PRODUCTS MFG INC. FAA STC ST<strong>01</strong>188CH CESSNA 5<strong>01</strong>, 551 Installation of Air Ambulance Conversion iaw. As referred in limitations section of the AFM-S The installation of this modification by 19.03.2<strong>01</strong>0<br />
Aero Medical Products MfgInstallation Drawing Prior to the first flight of each modified aircraft, third persons is subject towritten<br />
List Report 006-1 or later FAA approved and after eachchange to any of the<br />
permission of the approval holder and<br />
revisions<br />
communication, Navigational, or Med Pack holding and disposal ofthe approved<br />
equipment,a ground EMI test must be appropriate documentation. Prior to<br />
conducted iaw. EA Form 173. A copy of EA Fo installation of this modification it must be<br />
determined thatthe interr<br />
10034128 AERO MEDICAL PRODUCTS MFG INC. FAA STC ST02863CH FALCON 50 Aircraft Medical stretcher for MF 50<br />
This STC does not constitute an approval for Prior to installation of this modification it 09.03.2<strong>01</strong>1<br />
aircraftFAA STC ST02863CH<br />
installation.Compliance with minimum following must be determined thatthe<br />
requirements below need to bedemonstrated interrelationship between this modification<br />
through a design approval for installation in and any other previouslyinstalled<br />
each aircraftmodel to be equipped with this modification and/ or repair will introduce<br />
medical stretcher assembly part:<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>7055 AERO PACIFIC <strong>EASA</strong>.IM.R.S.<strong>01</strong>486 REV. 1 FAA STC STC SR<strong>01</strong>521LA EUROCOPTER FRANCE AS 350<br />
B<br />
EUROCOPTER FRANCE AS 350<br />
B1<br />
EUROCOPTER FRANCE AS 350<br />
B2<br />
EUROCOPTER FRANCE AS 350<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
BA<br />
EUROCOPTER FRANCE AS 350<br />
10039781 AERO PACIFIC FAA STC SR<strong>01</strong>688LA<br />
D<br />
206, 206A, 206B, 206B-1, 206L<br />
206L-1, 206L-3, 206L-4, 407<br />
Installation of a Belly Utility Mount.Note: This<br />
STC supersedes <strong>EASA</strong>.IM.R.S.<strong>01</strong>486.<br />
Installation of Aero Pacific Belly Utility Mount<br />
AP206UM02(Validation of FAA STC<br />
SR<strong>01</strong>688LA)<br />
1. This STC provides approval for structural<br />
provisions for installation of other equipment.<br />
This other equipment for which these<br />
provisions are intended has not been certified.<br />
A separate <strong>EASA</strong> approval is required for the<br />
installation of this equipment<br />
- This Belly utility Mount Installation is approved<br />
for a maximum weightof not more than 150<br />
pounds and a frontal area of 2.5 square feet.-<br />
This STC only addresses structural,<br />
performance and handling<br />
qualitiesrequirements. No system or electrical<br />
requirem<br />
25.07.2005<br />
<strong>01</strong>.02.2008<br />
<strong>04</strong>.03.2009<br />
Prior to installation of this modification it 23.05.2<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 />
10<strong>01</strong>6841 AERO SEATS AND SYSTEMS, INC <strong>EASA</strong>.IM.R.S.<strong>01</strong>214 SR09455RC SIKORSKY S-76A Installation of External Liferaft Deployment Approval limited to Sikorsky S-76A registration<br />
11.05.2006<br />
System<br />
G-BVCX Serial number 76<strong>01</strong>83<br />
10<strong>01</strong>6842 AERO SEATS AND SYSTEMS, INC <strong>EASA</strong>.IM.R.S.<strong>01</strong>218 SR09355RC SIKORSKY S-76A<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
Installation of Passenger Seats None 10.05.2006<br />
10<strong>01</strong>6844 AERO SEATS AND SYSTEMS, INC <strong>EASA</strong>.IM.R.S.<strong>01</strong>220 FAA STC SR09<strong>01</strong>1RC SIKORSKY S-76A<br />
Installation of Emergency Exit Window in Configurations with forward facing seats only 27.07.2006<br />
SIKORSKY S-76B<br />
SIKORSKY S-76C<br />
Passenger Door<br />
10<strong>01</strong>6912 AERO SEATS AND SYSTEMS, INC <strong>EASA</strong>.IM.R.S.<strong>01</strong>293 FAA STC SR09211RC SIKORSKY S-76A<br />
Installation of External Mounted Life Raft Installation of external mounted life raft<br />
15.<strong>01</strong>.2007<br />
SIKORSKY S-76B<br />
Deployment System[Identified as “Basic STC” deployment system, with optional deployment<br />
SIKORSKY S-76C<br />
by the FAA and approved using the<br />
handles in passenger compartment, in<br />
FAA/JAA/<strong>EASA</strong> type validation principles accordance with Aero Seats and Systems Inc.<br />
(TVP)]<br />
Installation manual ASI-500-100-<strong>01</strong>/02, revision<br />
H, dated December 5, 2005 or later appro<br />
10<strong>01</strong>6924 AERO SEATS AND SYSTEMS, INC <strong>EASA</strong>.IM.R.S.<strong>01</strong>309 FAA STC SR09453RC BELL 412<br />
BELL 412 EP<br />
Installation of Cabin Seats 15.03.2007<br />
10<strong>01</strong>4192 AERO TECHNICS DESIGN LIMITED <strong>EASA</strong>.A.S.<strong>01</strong>334 1. BOEING 747-100<br />
Introduction of Horsebox Containers BAC1136-<br />
26.07.2005<br />
1. BOEING 747-200<br />
1. BOEING 747-400<br />
2. BOEING MD-11 SERIES<br />
3. DC-10 SERIES<br />
3<strong>01</strong> and BAC1136-4<strong>01</strong><br />
10<strong>01</strong>4600 AERO TECHNICS DESIGN LIMITED <strong>EASA</strong>.A.S.02722 REV 1 BOEING MD-83 Cabin Reconfiguration from 167Y to 52C/22Y<br />
Seating<br />
28.09.2006<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 13/<strong>462</strong>
Change language