Module 5 And EASA Flashcards
1
Q
Agency with REGULATORY and
EXECUTIVE tasks in the field of civilian
aviation safety.
A
european union aviation agency
2
Q
EASA responsibilities:
A
Conduct analysis and research of safety
· Authorizing foreign operators
· Giving advice for the drafting of EU Legislation
· Implementing and monitoring safety rules
· Release Type Certification of aircraft and components as well as the
approval of organizations involved in the design, manufacture and
maintenance of aeronautical products.
3
Q
easa regulations part 21
A
airworthiness and environmental certification
4
Q
easa part 66
A
maintenace certifying staff
5
Q
easa part 145
A
maintenance organisation approval
6
Q
easa part m
A
continuing airworthiness requirement
7
Q
easa part 147
A
maintenance training organisation approvals
8
Q
easa part 21 subpart j
A
design organisation approval
9
Q
easa part 21 subpart g
A
production organisation
10
Q
Regulates the approval of aircraft design and production
organisations and the certification of aircraft Products,
Parts, and Appliances.
A
EASA PART 21 - Airworthiness and Environmental
Certification
11
Q
easa subpart 21 a
A
general provision
12
Q
easa subpart 21 b
A
type certificates
13
Q
easa subpart 21 d
A
changes to type certificates
14
Q
easa subpart 21e
A
supplemental type certificates
15
Q
easa subpart 21 f
A
production without production organization approval
16
Q
easa subpart 21 g
A
production organization approval
17
Q
easa subpart 21 h
A
airworthiness certificates
18
Q
easa subpart 21 i
A
noise certificates
19
Q
easa subpart 21 j
A
design organization approval
20
Q
easa subpart 21 k
A
parts and appliances
21
Q
easa subpart 21 m
A
repairs
22
Q
easa subpart 21 o
A
european technical standard order authorisations
23
Q
easa subpart 21 p
A
permit to fly
24
Q
easa subpart 21 q
A
identification of products parts and appliances
25
Establishes general rights and obligations of applicant/holder
Requirement for dealing with failures, malfunctions and defects
Covers airworthiness directives
Defines co-operation required between design and production
easa 21 subpart a
26
Obtaining a TC for an aircraft, engine or propeller
Issue of a restricted TC for an aircraft
Application for a TC only acceptable from the holder of an appropriate Design
Organisational Approvals (DOA) - Subpart J
Alternative procedures to subpart J in certain cases agreed by the Agency
Rights and Obligations of TC holders
The Agency evaluates to relevant technical codes (CS-25, CS-29) : CS - Certification
Specifications
easa subpart b
27
Major Changes to the TC can be applied for by the TC holder only under this subpart
Any person may apply to the agency for the approval of a minor change to the TC
easa 21 subpart d
28
_____________ has no appreciable effort on the mass, balance, structural strength,
reliability, operational characteristics, noise, fuel venting, exhaust emission, or
other characteristics affecting the airworthiness of the product. All other changes
are major.
Minor Change
29
Major Changes to a TC by other than a TC holder
How to obtain an STC
Only accepted from a DOA holder except in circumstances agreed by the Agency
Rights and obligations of an STC holder
EPA marking (European Part Approval)
Also relevant to repairs and minor changes
easa 21 subpart e
30
___________is a combined design & production
approval which _______________ within the EASA system.
FAA Parts Manufacturer Approval (PMA)
does not exist
31
All design is done by
__________________ & All Production (assuming there is approved
design data) is done by____________________
EASA Part 21 Subpart J
EASA Part 21 G Organisation.
32
___________refers to parts that are produced in accordance
with approved design data which is not property of the type certificate holder,
except for European Technical Standard Order (ETSO) parts.
european part approval
33
____________
should not be equated with _____________-
parts under the _________-system, as these are two different concepts.
EPA marked parts
PMA (Part Manufacturing Approval) marked
FAA
34
So to consider that EPA serves a different purpose. In fact, The EPA marking was
introduced in ____________- essentially to clearly identify any "___________" Part.
This means any Part or Appliance not designed by the __or ____ Approval
Holder - This also serves as relevant continuing airworthiness information for
both __________ and ________________________________________
2004
not original
TC
ETSO
Maintenance Organisations
Accident or Incident investigators.
35
The __________________authorization represents one
way (and not the only way) to have _____ and _____ approved. This is an optional step which ensures that a part or appliance complies with a ____________
performance standard.
ETSO (European Technical Standard Order)
parts
appliances
minimum
36
___________ for use of subpart F is issued by the __________ after the applicant:
Establishes a satisfactory production inspection system
Provides an acceptable manual
Demonstrates it complies with relevant part ______requirements
Letter of agreement issued for a max duration of _____year
Applicant shall demonstrate that either:
Subpart _ is not appropriate or
Release of product, part or appliance is needed prior to issuance of subpart_
approval
Approval of design data and coordination with design organization same as subpart G
Not previously used by the ______under the _______ system
remains an option for specific cases
Letter of Agreement
CAA
21
one
g
G
CAA
JAA
37
An __________is an organization which has
approval to manufacture aircraft parts and appliances in conformity with
approved data.
EASA Part 21 Subpart G organization
38
This subpart gives the rules for showing compliance of products, parts, appliances with
applicable design data through an approval organization
EASA 21 SUBPART G
39
Subpart where Production Organization Exposition (POE) is required
EASA 21 SUBPART G
40
subpart where A link between a design organization and the production organization is necessary
EASA 21 SUBPART G
41
No design privileges are associated with this subpart
EASA 21 SUBPART G
42
(Authoriszed release certificate - components),
EASA Form 1
43
EASA Form 52 (_____________) raised by organisation as appropriate -
________aircraft
Statement of Conformity
complete
44
subpart _
For a new aircraft, a ___________ is issued upon presentation
relevant documentation (statement of conformity etc.) to the CAA
h
Certificate of Airworthiness
45
For a used aircraft__________ is issued upon presentation of either:
An _________________ for an aircraft from an ________________, or
As above plus additional info (see 21.A.174b3) for an aircraft from outside the
EU.
C of A
airworthiness review certificate
EU member state
46
The ___issue a _________________________to an:
Aircraft which conforms to a restricted TC, or
Aircraft shown to comply with specifics CS ensuring adequate safety
CAA
restricted certificate of airworthiness
47
For a new aircraft, a ____________- is issued upon presentation relevant
documentation (statement of conformity or similar if from outside the EU) to the CAA.
noise certificate
48
For a used aircraft, a noise certificate is issued upon ______________________ and
_________________.
presentation noise information
relevant historical records
49
The holder of an appropriate Design organization approval can submit compliance documents to the agency in
order to obtain a:
________________________________________________________________________________________________________________________________________________
Type certificate or approval of a major change to a type certificate
Supplemental type certificate
European Technical Standard Order
(ETSO) authorization for auxiliary power
unit (APU)
Major Repair Design Approval
50
The holder of an appropriate DOA can submit compliance documents to the agency Which shall be accepted ____________ further verification, subject to _________
with or without
without
21.A.257b
51
Subpart _
Showing compliance of the part or appliance with applicable requirements shall be
made:
As part of the type certification process, subpart___, ____, or __, or
Under ______________, subpart __, or
In the case of standard parts,
in accordance with officially recognized standards
k
B
D
E
ETSO authorization
O
52
With the exception of standard parts and non-critical parts _______ or _______ aircraft , no
part or appliance is eligible for installation in type-certificated product unless it is:
Accompanied by an authorized release certificate certifying airworthiness, and
Marked in accordance with subpart_.
ELA1
ELA2
release certificate certifying airworthiness
Q
53
A part is considered as a "_____________" where it is designated, as such by the ______________________ responsible for the product, or appliance, in which the part is intended
to be used.
standard part
design approval holder
54
In order to be considered a "____________________", all design manufacturing, inspection
data, and marking requirements necessary to demonstrate the conformity of that part
should be in the public domain and published or established as part of officially
recognized standards.
standard part
55
Major repairs can be approved by the _____ OF _________________ holder or by the Agency
TYPE CERTIFICATE OR SUPPLEMENTAL TYPE CERTIFICATE
56
Repairs are classified as either _____ or ____
major
minor
57
Classification can be made by either the _______ or by an appropriately _________
Agency
approved DOA
