Module 10/1

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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 to be carried out

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 unde

Part-21 Subpart J Production Organisation approval

The requirements for the issuance of ETSO authorizations are found in

Part -21 Section A Subpart O

If a certified aircraft has outstanding airworthiness directives that have not been complied with

It is not considered airworthy

An airworthiness directive contains at least the following information

an identification of the unsafe condition And the affected aircraft

Manuals required for the product's continued airworthiness include the following

aircraft maintenance and structure repair manual

Aircraft and engine manuals are most likely supplied to maintenance organisation on CD t

to reduce storage space requirements and to make updates and amendments easier

Elimination of damage by replacing parts or appliances without the necessity for design activity is considered

maintenance task requires no approval under Part-21

CAMO) is part of the EASA’s Implementing Rules EU 1321/ the abbreviation (CAMO) stand for.

Continuing airworthiness management organisation

Personnel required to be employed in a CAMO are

the accountable manager, the quality manager (to ensure all EASA requirements comply)

Findings in audits are categorised in levels: level 1 and Level 2.

Level 1 finding is a severe hazard to flight safety, and the approval to operate can be revoked until a satisfactory correction is taken

Airworthiness of light aircraft not used for commercial air transport must be managed under

Part-M Subpart C

The term “maintenance programme” includes

Scheduled maintenance tasks, associated procedures and standard maintenance practise

The maintenance programme details should be reviewed at least

annually

After any maintenance, the associated certificate of service release is entered in the aircraft continuing airworthiness records

As soon as practicable but in no event more than 30 days

the operator’s aircraft technical log is a system for

recording defects and malfunctions during the aircraft operation

Part-M applicable maintenance data is

procedure, standard or information issued by the competent authority and any applicable airworthiness directive

An independent inspection is an inspection first made by

an authorised person signing the maintenance release

the authorised certifying staff

can decide whether an aircraft defect hazards seriously the flight safety

Part-M Subpart E identifies

component standards for all EASA aircraft

Airworthiness review staff carry out a physical survey of the aircraft shall ensure that

all required markings and placards are correctly installed

Part-T relates to the definition of the continuing airworthiness requirements applicable to

third-country registered aircraft

A continuous airworthiness management organisation (CAMO-T) is an organisation approve

under Part-M Subpart G

A Part-CAO approved organisation is a ‘combined airworthiness organisation’ exercise the privileges

of both. Part-ML and Part-CAMO organisations and

PART CAO applies to

organisations for maintenance and maintenance management of non-complex and non-CAT aircraft

A)check detailed inspections performed

Every 500-800 flight hours

D) checks detailed inspections take up

2months to complete

A check, B check are considered

lighter checks

The training standard for personnel performing the pre-flight inspection should be described in

the operator’s continuing airworthiness management exposition

Emergency airworthiness directives (EAD), Published by responsible authorities such as

EASA or the FAA

A request for an Airworthiness directive alternative means of compliance (AMOC) should be made using an

EASA Form 42

communicate airworthiness information to owners/operators.

service information’ is used to encompass the various forms of notification that a manufacturer may use to

Alert service bulletins (ASB) (also known as emergency service bulletins) are issued

operator's urgent attention to items affecting safety

Vendor service bulletins (VSB) are issued by

equipment or component manufactures

An organisation wishing to design its modifications and repairs must be approved in accordance with

Part-21 aircraft certification

The unique aspect of the ATA 100-chapter numbers is its relevance for

all aircraft

the most used manuals in a line/hangar environment

The maintenance manual and illustrated parts catalogue

Illustrated parts catalogue (IPC) provides a means to

isolate and identify the correct components or aircraft parts and presents diagrams of structure and equipment breakdown

The engineer guidance regarding minor repair procedures to the aircraft’s structure stated in the

aircraft maintenance manual

The Structural repair SRM manual gives you details of

repair materials and procedures for structures subjected to repairs

Maintenance Manuals in cassette/CDs have the advantage of being easier to

Amend

Revision and amendments to manuals which is known as the revision cycle This usually happens

three or four times a year

The list of effective pages in each manual which lists every page and its issue date

so that the holder may check that a manual is complete and current

The role of the technical center “MAINTROL” is to

Minimize operational technical disruption and Ensure that day-to-day maintenance is performed

When aircraft stored for any reason, it becomes necessary to apply a preventative maintenance regime This is laid down in the

Aircraft maintenance manual (AMM)

The sole purpose of A functional check flight (FCF) is to

Check for specific aircraft systems for correct airborne function

Test flight is a mandatory requirement before

issuing a certificate of airworthiness

Extended Range Operations (ETOPS) is defined as flight conducted over a route that contains a point further than

approved threshold time at the approved one-engine out

ETOPS rules is defined in the

ETOPS manual

All-weather operations refer to instrument landing systems (ILS) requirements

Both airborne and ground-based equipment

To determine decision height CAT II and CAT III approaches are used

radio altimeter

Category II Autoland with a decision height of 100 ft has a visual line up approach limit of

350 meters.

The excess ILS deviation light is coloured

amber and flashing

Module5

Module5

Module 5 1

Module 5 1

Module 2

Module 2

Module2 /1

Module2 /1

Module9

Module9

Module 10

Module 10

Module 6

Module 6

Module 6/1

Module 6/1

Module 6/2

Module 6/2

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 to be carried out

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 unde

Part-21 Subpart J Production Organisation approval

The requirements for the issuance of ETSO authorizations are found in

Part -21 Section A Subpart O

If a certified aircraft has outstanding airworthiness directives that have not been complied with

It is not considered airworthy

An airworthiness directive contains at least the following information

an identification of the unsafe condition And the affected aircraft

Manuals required for the product's continued airworthiness include the following

aircraft maintenance and structure repair manual

Aircraft and engine manuals are most likely supplied to maintenance organisation on CD t

to reduce storage space requirements and to make updates and amendments easier

Elimination of damage by replacing parts or appliances without the necessity for design activity is considered

maintenance task requires no approval under Part-21

CAMO) is part of the EASA’s Implementing Rules EU 1321/ the abbreviation (CAMO) stand for.

Continuing airworthiness management organisation

Personnel required to be employed in a CAMO are

the accountable manager, the quality manager (to ensure all EASA requirements comply)

Findings in audits are categorised in levels: level 1 and Level 2.

Level 1 finding is a severe hazard to flight safety, and the approval to operate can be revoked until a satisfactory correction is taken

Airworthiness of light aircraft not used for commercial air transport must be managed under

Part-M Subpart C

The term “maintenance programme” includes

Scheduled maintenance tasks, associated procedures and standard maintenance practise

The maintenance programme details should be reviewed at least

annually

After any maintenance, the associated certificate of service release is entered in the aircraft continuing airworthiness records

As soon as practicable but in no event more than 30 days

the operator’s aircraft technical log is a system for

recording defects and malfunctions during the aircraft operation

Part-M applicable maintenance data is

procedure, standard or information issued by the competent authority and any applicable airworthiness directive

An independent inspection is an inspection first made by

an authorised person signing the maintenance release

the authorised certifying staff

can decide whether an aircraft defect hazards seriously the flight safety

Part-M Subpart E identifies

component standards for all EASA aircraft

Airworthiness review staff carry out a physical survey of the aircraft shall ensure that

all required markings and placards are correctly installed

Part-T relates to the definition of the continuing airworthiness requirements applicable to

third-country registered aircraft

A continuous airworthiness management organisation (CAMO-T) is an organisation approve

under Part-M Subpart G

A Part-CAO approved organisation is a ‘combined airworthiness organisation’ exercise the privileges

of both. Part-ML and Part-CAMO organisations and

PART CAO applies to

organisations for maintenance and maintenance management of non-complex and non-CAT aircraft

A)check detailed inspections performed

Every 500-800 flight hours

D) checks detailed inspections take up

2months to complete

A check, B check are considered

lighter checks

The training standard for personnel performing the pre-flight inspection should be described in

the operator’s continuing airworthiness management exposition

Emergency airworthiness directives (EAD), Published by responsible authorities such as

EASA or the FAA

A request for an Airworthiness directive alternative means of compliance (AMOC) should be made using an

EASA Form 42

communicate airworthiness information to owners/operators.

service information’ is used to encompass the various forms of notification that a manufacturer may use to

Alert service bulletins (ASB) (also known as emergency service bulletins) are issued

operator's urgent attention to items affecting safety

Vendor service bulletins (VSB) are issued by

equipment or component manufactures

An organisation wishing to design its modifications and repairs must be approved in accordance with

Part-21 aircraft certification

The unique aspect of the ATA 100-chapter numbers is its relevance for

all aircraft

the most used manuals in a line/hangar environment

The maintenance manual and illustrated parts catalogue

Illustrated parts catalogue (IPC) provides a means to

isolate and identify the correct components or aircraft parts and presents diagrams of structure and equipment breakdown

The engineer guidance regarding minor repair procedures to the aircraft’s structure stated in the

aircraft maintenance manual

The Structural repair SRM manual gives you details of

repair materials and procedures for structures subjected to repairs

Maintenance Manuals in cassette/CDs have the advantage of being easier to

Amend

Revision and amendments to manuals which is known as the revision cycle This usually happens

three or four times a year

The list of effective pages in each manual which lists every page and its issue date

so that the holder may check that a manual is complete and current

The role of the technical center “MAINTROL” is to

Minimize operational technical disruption and Ensure that day-to-day maintenance is performed

When aircraft stored for any reason, it becomes necessary to apply a preventative maintenance regime This is laid down in the

Aircraft maintenance manual (AMM)

The sole purpose of A functional check flight (FCF) is to

Check for specific aircraft systems for correct airborne function

Test flight is a mandatory requirement before

issuing a certificate of airworthiness

Extended Range Operations (ETOPS) is defined as flight conducted over a route that contains a point further than

approved threshold time at the approved one-engine out

ETOPS rules is defined in the

ETOPS manual

All-weather operations refer to instrument landing systems (ILS) requirements

Both airborne and ground-based equipment

To determine decision height CAT II and CAT III approaches are used

radio altimeter

Category II Autoland with a decision height of 100 ft has a visual line up approach limit of

350 meters.

The excess ILS deviation light is coloured

amber and flashing