M10C5

39問 • 1年前

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通報

問題一覧

The annex for Regulation (EU) No 748/2012 is

Part 21

Subpart K in Part 21 includes

Parts and Appliances.

Certification specifications (CS) are sometimes referred to as

European Aviation Certification Standards (EACS) and airworthiness codes.

Aircraft design and manufacture standards are prescribed in the

certification specifications (airworthiness codes)

The CS 22 certificate specifications refer to

Sailplanes and powered sailplanes.

you can find the airworthiness code applies to small rotorcraft with a maximum weight of 3,175 kg in

Certification specifications (CS 27)

The Technical requirements for the design and construction of aircraft engines are found in

EASA Part-21 subpart CS E.

Certification specifications Subpart B deals with

Flight tests.

An aircraft or engine manufacturer will typically have both

Design organisation approval (DOA) and production organization approval (POA) approvals.

The letter of agreement is issued for a limited duration,

not exceeding one year.

Supplemental type certificate is issued following a modification The STC defines

the product design change, states how the modification affects the existing type design

the type certificate holder keep the type certificate valid

through Continuously following airworthiness directives, issuing service bulletins.

The certificate of design states that the aircraft

Meets current stated design requirements specified in the certification specifications.

The main reason for the Issuing of a restricted type-certificate is

For an aircraft that does not meet the provisions of Part 21 entirely.

The type-certificate and restricted type certificate are both considered to include

The type design and the operating limitations.

The holder of the type-certificate or restricted type-certificate shall provide at least

one full set of instructions for continued airworthiness

The principle of operational suitability data (OSD)

specific data necessary for the safe operation of the aircraft type.

The responsible for keeping the data current regarding the type certificate data sheet (TCDS) is

The manufacturer.

Minor changes in type design means

Changes that have no appreciable effect on the mass, balance and structural strength.

The term ‘changes to the type certificate’ is consistently used in

Part 21 Subpart D and E.

Changes must be classified as minor or major and approved by

An approved design organisation within the scope of its privileges.

The scope of a Supplemental type certification STC can be extremely narrow or broad

It could include minor modifications to passenger cabin items And Substantial modifications may involve engine replacement.

To convert the aircraft and fit with all equipment necessary for operations in emergency medical services (EMS) approved under

Part-21 Subpart J Production Organisation approval.

The requirements for the issuance of ETSO authorizations are found in

Part 21 Section A Subpart O.

Each aircraft must have its own aircraft registration based on

rules and regulation of the respective country of registration

Annex 7 to the Convention on International Civil Aviation describes

The definitions, location, and measurement of nationality and registration marks.

The competent authority of the EASA member state must not enter an aircraft on their national register if it appears that

the aircraft is registered outside the member state and an unqualified person holds any legal or beneficial interest by way of ownership

Every aircraft shall have a fireproof registration plate bearing

The aircraft’s nationality and registration mark and The manufacturer’s designation and serial number .

The aircraft owner name plate must be

fixed Near the front door.

Airworthiness certificates are classified as follows

Certificates of airworthiness, Restricted certificates of airworthiness and permit to fly

Radio license and installation approval are Essential documents required for the issue of a

Certificate of airworthiness.

An airworthiness review certificate (ARC) issued

Per Part-M.

An airworthiness check flight is required using a pilot agreed by

The competent authority.

Permits to fly are issued per

Part-21 Subpart P.

Each application for a permit to fly shall include

The purpose(s) of the flight(s) and The flight conditions

A noise certificate may be amended or modified only by the

Competent authority of the member state of registry.

Mass and centre of gravity (CG) of the aircraft shall comply with

limitations specified in the aircraft flight manual and operations manual.

An operator shall establish mass and balance documentation before each flight specifying

The load and its distribution.

All transmitting radio equipment (VHF, HF, ELT, radar) installed on an aircraft should be covered in

The radio license.

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