513
harmonized process an independent assessment
body must check the suitability of the chosen
methods as well as the results of the risk
managementprocess.
Consequently,thesignificanceofachangeisnot
decisive whether a risk management process has to
be appliedornotbutdetermines if an independent
assessment
isrequiredornot.Inthiscontext,thefour
qualitative criteria innovation, complexity,
monitoringand reversibilityconsider ifthereisany
experience with the change itself and its
implementation or not. Therefore, it is more likely
that a change is significant, if there is only little
experience with the proposed
change within the
companywherethechangetakesplace.Againstthis
background, the implementation of new technology
likethe first‐timeuse ofLEDtechnology withinthe
signalingsystemforrailwaysrepresentsanexample
fora significantchange.Ontheotherhand,addinga
new function to an electronic interlocking is
a
complex task and the interlocking is also highly
safety relevant. However, the company which
implements this type of change usually has the
experience to do so and uses well‐known practices.
Therefore, in this case the change is not significant
and the company has to apply its own safety
procedure without the participation of an
independentassessmentbody.
3 APPROACHTOEVALUATECHANGESIN
AVIATION
In the area of European aviation the European
AviationSafetyAgency(EASA)isresponsibleforthe
safety management and the certification of aviation
productswithintheEuropeanUnion(EU).Onemain
elementofthe safety
management withintheEUis
the Commission Regulation No 748/2012 (2012),
which lays down implementing rules for the
airworthiness as well as for the certification of
aircraftandrelatedproductsandthe certificationof
designandproductionorganizations.
Article 2 of this regulation constitutes that
products, parts and appliances shall
be issued
certificates,whicharespecifiedinAnnex1(Part21)
of the Commission Regulation. Also design and
production organizations which are responsible for
thedesignrespectivelythemanufactureofproducts,
parts and appliances have to demonstrate their
capability. Moreover, Section B of this Annex
addresses the type certification and the
relevant
proceduresforissuingthesetype‐certificates.Basisof
thetypecertificationaretheapplicableairworthiness
code and any relevant special condition. These
special conditions refer to aspects of the product
whichmaybeunusualregardingthedesignfeatures
orpracticesaswellasto unconventional use of the
product
or unsafe conditions which may appear
during operation. Additionally, the type‐certificate
hastocontainthedemonstrationofcompliancewith
theenvironmentalrequirementswhichrefertonoise
and emission requirements and it has to be shown
that “no feature or characteristic makes it unsafe”.
Furthermore, any aircraft type‐certificate requires a
type‐certificate for the engine or the propeller
installedinthegivenaircraft.
The given Commission Regulation distinguishes
between repairs and changes. Speaking of changes,
point 21.A.19 of Subpart B describes a “change in
design,power,thrustormass[which]issoextensive
that a substantially complete investigation of
compliance
with the applicable type‐certification is
required”. In this case, the changed product can
generally be regarded as a new product which
requires a reinvestigation of compliance with the
airworthiness requirements. An example for a
substantial change in this area is the change in the
numberorthelocationofengines
ofanaircraft.
Beside these substantial changes, Subpart D
addresses further changes to type design and type‐
certificatesanddescribestheprocedureswhichhave
to be done by the proposer. For this purpose,
proposed changes to a type design are subdivided
into three categories: standard changes, minor and
majorchanges
whereassubstantialchangesdescribed
above are also major changes. According to point
21.A.90B,standardchangesrefertoaircraftsof5.700
kgMaximumTake‐OffMass(MTOM)orlessaswell
as to rotorcrafts, sailplanes, balloons or European
Light Aircrafts. For standard changes acceptable
methods, techniques and practices issued by the
EASA
for the identification and implementation of
standard changes have to be applied. If these
conditions are met, a change is regarded as a
standard change and is not subject to an approval
process.
Changes in type design which are no standard
changesareclassifiedintominorandmajorchanges.
In
thisrespect,point21.A.91ofSubpartDdescribes
thatachangeisregardedasaminorchange,ifithas
no “appreciable effect on the mass, balance,
structural strength, reliability operational
characteristics,noise,fuelventing,exhaustemission,
orothercharacteristicsaffectingtheairworthinessof
the product”. All other changes are regarded
as
major changes. This classification determines the
further proceeding for the implementation of the
change. Minor and major changes to a type design
havetoappliedinformandmannerdeterminedby
theEASA.Accordingtopoint21.A.93theapplication
has to include a description of the change which
identifies
all parts of the type design and the
approved manuals affected by the change. In
addition, the application has to outline “the
certification specifications and environmental
protection requirements with which the change has
beendesignedtocomply”.
Minorchangeshavetobeapprovedeitherbythe
EASA or by an appropriately
approved design
organization. Furthermore, minor changes require a
record‐keepingforeachchange.Moreover,variations
ininstructionsforcontinuedairworthinessduetothe
changeshallbemadeavailabletoallknownowners
of affected products. Nevertheless, this type of
approvalisonlypossible,iftheapplicantshowsthat
the change
meets the applicable certification
specifications of point 21.A.101 regarding the
compliance with the airworthiness code and the
environmental protection requirements. In this
context,thesingleinstallationofaGPS‐basedFlight