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>04</strong><strong>01</strong>83 INTERNATIONAL ENGINEERING<br />
F177RG IEA/STC/ERHC/<strong>01</strong>/2<strong>01</strong>0 revision 00 - Electric Limitation to F177RG serial number 0<strong>01</strong>6. Prior to installation of this modification it 15.06.2<strong>01</strong>2<br />
ASSISTANC<br />
Rudder Hand Control.<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 />
10027431 ISEI P-<strong>EASA</strong>.R.S.<strong>01</strong>543 AS350 B3, EC130 B4 -Installation of Safetyplane Equipment-<br />
Installation of a system for tracking a set of<br />
flight and systemparameters during operation<br />
of the rotorcraft. The modification is basedon<br />
ISEI change N-EC130 AS350B3 as defined in<br />
Dossier de Définition de laModificat<br />
10027889 ISEI REV. 1 EC 120 B Installation of HELICOM V1 or HELICOMV2<br />
data recording system.Revision 1 of STC<br />
10027889 introducing change in system<br />
name(Safetyplane becomes HELICOM<br />
V1), new V2 version and<br />
Associateddocumentation.<br />
10028200 ISEI R44, R44 II Title: Installation of Safetyplane<br />
EquipmentDescription: Installation of a system<br />
for tracking a set of flight andsystem<br />
parameters during operation of the rotorcraft.<br />
The modificationis based on ISEI change N-<br />
R44 as defined in the Master Document ListN1-<br />
R<br />
10028789 ISEI AS350 B, BA, BB, B1, B2 Installation of Safetyplane<br />
EquipmentInstallation of a system for tracking a<br />
set of flight and systemparameters during<br />
operation of the rotorcraft as defined in the<br />
ApprovalChange Document N2-AS350 B BA<br />
BB B1 B2 E-A-02.<br />
10033288 ISEI P-<strong>EASA</strong>.R.S.<strong>01</strong>542 REV. 1 AS 355 NP Installation of HELICOMV2 NUMInstallation of<br />
a system for tracking a set of flight and<br />
systemparameters during operation of the<br />
rotorcraft. The modification is basedon ISEI<br />
change N-AS355_NP as defined in N1-AS355<br />
NP-HV2 NUM-APPROVALCHANGE FILE-E-<br />
A.<br />
10033974 ISEI REV. 1 A109E Installation of HELICOM V1 or HELICOM V2<br />
data monitoring system.Revision 1 of STC<br />
10033974 introducing change in system<br />
name(Safetyplane becomes HELICOM V1),<br />
new V2 version and associateddocumentation.<br />
10034914 ISEI EC135 P1(CPDS),<br />
EC135 P2(CPDS),<br />
EC135 P2+,<br />
EC135 T1(CPDS),<br />
EC135 T2(CPDS),<br />
EC135 T2+<br />
Installation of HELICOMV2 NUMInstallation of<br />
a system for tracking a set of flight and<br />
systemparameters during operation of the<br />
rotorcraft. The modification is basedon ISEI<br />
change "Installation of HELICOMV2 NUM" as<br />
defined in ApprovalChange File N1- EC135<br />
10035287 ISEI REV. 2 AS350B2, AS350B3, EC130B4 Installation of HELICOM V2 NUMRevision 1<br />
introducing alternate positions for<br />
antennas.Revision 2 correcting minor<br />
discrepancies in associated documentation.<br />
None The approval holder shall fulfil the<br />
obligations of Part 21,<br />
Paragraph21.A109. Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repai<br />
30.09.2009<br />
None. None. 03.06.2<strong>01</strong>1<br />
None The approval holder shall fulfil the<br />
08.12.2009<br />
obligations of Part 21, Paragraph21.A109<br />
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<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 />
09.02.2<strong>01</strong>0<br />
None The system does not replace standard<br />
maintenance records and<br />
pilotreporting.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repair w<br />
None The approval holder shall fulfil the<br />
obligations of Part 21,<br />
Paragraph21A.118A. Prior to installation<br />
of this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
31.<strong>01</strong>.2<strong>01</strong>1<br />
05.05.2<strong>01</strong>1<br />
None.<br />
repa<br />
The system does not replace standard<br />
maintenance records and<br />
pilotreporting.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repair w<br />
16.05.2<strong>01</strong>1<br />
For AS350B2 model this STC is applicable The system does not replace standard 27.11.2<strong>01</strong>2<br />
only to aircraft equipped withVEMD system maintenance records and pilotreporting.<br />
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<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 281/<strong>462</strong>
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