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CALR > Module 5 And EASA > Flashcards

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

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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.

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3
Q

easa regulations part 21

A

airworthiness and environmental certification

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4
Q

easa part 66

A

maintenace certifying staff

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5
Q

easa part 145

A

maintenance organisation approval

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6
Q

easa part m

A

continuing airworthiness requirement

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7
Q

easa part 147

A

maintenance training organisation approvals

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8
Q

easa part 21 subpart j

A

design organisation approval

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9
Q

easa part 21 subpart g

A

production organisation

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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

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11
Q

easa subpart 21 a

A

general provision

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12
Q

easa subpart 21 b

A

type certificates

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13
Q

easa subpart 21 d

A

changes to type certificates

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14
Q

easa subpart 21e

A

supplemental type certificates

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15
Q

easa subpart 21 f

A

production without production organization approval

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16
Q

easa subpart 21 g

A

production organization approval

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17
Q

easa subpart 21 h

A

airworthiness certificates

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18
Q

easa subpart 21 i

A

noise certificates

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19
Q

easa subpart 21 j

A

design organization approval

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20
Q

easa subpart 21 k

A

parts and appliances

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21
Q

easa subpart 21 m

A

repairs

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22
Q

easa subpart 21 o

A

european technical standard order authorisations

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23
Q

easa subpart 21 p

A

permit to fly

24
Q

easa subpart 21 q

A

identification of products parts and appliances

25
Q

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

A

easa 21 subpart a

26
Q

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

A

easa subpart b

27
Q

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

A

easa 21 subpart d

28
Q

_____________ 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.

A

Minor Change

29
Q

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

A

easa 21 subpart e

30
Q

___________is a combined design & production
approval which _______________ within the EASA system.

A

FAA Parts Manufacturer Approval (PMA)
does not exist

31
Q

All design is done by
__________________ & All Production (assuming there is approved
design data) is done by____________________

A

EASA Part 21 Subpart J
EASA Part 21 G Organisation.

32
Q

___________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.

A

european part approval

33
Q

____________
should not be equated with _____________-
parts under the _________-system, as these are two different concepts.

A

EPA marked parts
PMA (Part Manufacturing Approval) marked
FAA

34
Q

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 ________________________________________

A

2004
not original
TC
ETSO
Maintenance Organisations
Accident or Incident investigators.

35
Q

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.

A

ETSO (European Technical Standard Order)
parts
appliances
minimum

36
Q

___________ 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

A

Letter of Agreement
CAA
21
one
g
G
CAA
JAA

37
Q

An __________is an organization which has
approval to manufacture aircraft parts and appliances in conformity with
approved data.

A

EASA Part 21 Subpart G organization

38
Q

This subpart gives the rules for showing compliance of products, parts, appliances with
applicable design data through an approval organization

A

EASA 21 SUBPART G

39
Q

Subpart where Production Organization Exposition (POE) is required

A

EASA 21 SUBPART G

40
Q

subpart where A link between a design organization and the production organization is necessary

A

EASA 21 SUBPART G

41
Q

No design privileges are associated with this subpart

A

EASA 21 SUBPART G

42
Q

(Authoriszed release certificate - components),

A

EASA Form 1

43
Q

EASA Form 52 (_____________) raised by organisation as appropriate -
________aircraft

A

Statement of Conformity
complete

44
Q

subpart _

For a new aircraft, a ___________ is issued upon presentation
relevant documentation (statement of conformity etc.) to the CAA

A

h
Certificate of Airworthiness

45
Q

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.

A

C of A
airworthiness review certificate
EU member state

46
Q

The ___issue a _________________________to an:
Aircraft which conforms to a restricted TC, or
Aircraft shown to comply with specifics CS ensuring adequate safety

A

CAA
restricted certificate of airworthiness

47
Q

For a new aircraft, a ____________- is issued upon presentation relevant
documentation (statement of conformity or similar if from outside the EU) to the CAA.

A

noise certificate

48
Q

For a used aircraft, a noise certificate is issued upon ______________________ and
_________________.

A

presentation noise information
relevant historical records

49
Q

The holder of an appropriate Design organization approval can submit compliance documents to the agency in
order to obtain a:
________________________________________________________________________________________________________________________________________________

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
Q

The holder of an appropriate DOA can submit compliance documents to the agency Which shall be accepted ____________ further verification, subject to _________

with or without

A

without
21.A.257b

51
Q

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

A

k
B
D
E
ETSO authorization
O

52
Q

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_.

A

ELA1
ELA2
release certificate certifying airworthiness
Q

53
Q

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.

A

standard part
design approval holder

54
Q

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.

A

standard part

55
Q

Major repairs can be approved by the _____ OF _________________ holder or by the Agency

A

TYPE CERTIFICATE OR SUPPLEMENTAL TYPE CERTIFICATE

56
Q

Repairs are classified as either _____ or ____

A

major
minor

57
Q

Classification can be made by either the _______ or by an appropriately _________

A

Agency
approved DOA

CALR (8 decks)

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