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Airworthiness of light aircraft not used for commercial air transport must be managed under
Part-M Subpart C
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The certificate of design states that the aircraft
Meets current stated design requirements specified in the certification specifications
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communicate airworthiness information to owners/operators.
service information’ is used to encompass the various forms of notification that a manufacturer may use to
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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
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All-weather operations refer to instrument landing systems (ILS) requirements
Both airborne and ground-based equipment
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The sole purpose of A functional check flight (FCF) is to
Check for specific aircraft systems for correct airborne function
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Alert service bulletins (ASB) (also known as emergency service bulletins) are issued
operator's urgent attention to items affecting safety
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you can find the airworthiness code applies to small rotorcraft with a maximum weight of 3,175 kg in
Certification specifications (CS 27
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The role of the technical center “MAINTROL” is to
Minimize operational technical disruption and Ensure that day-to-day maintenance is performed
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Changes must be classified as minor or major and approved by
An approved design organisation within the scope of its privileges
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the operator’s aircraft technical log is a system for
recording defects and malfunctions during the aircraft operation
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Manuals required for the product's continued airworthiness include the following
aircraft maintenance and structure repair manual
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The training standard for personnel performing the pre-flight inspection should be described in
the operator’s continuing airworthiness management exposition
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Part-M Subpart E identifies
component standards for all EASA aircraft
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Maintenance Manuals in cassette/CDs have the advantage of being easier to
Amend
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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
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Minor changes in type design means
Changes that have no appreciable effect on the mass, balance and structural strength
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The requirements for the issuance of ETSO authorizations are found in
Part -21 Section A Subpart O
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Category II Autoland with a decision height of 100 ft has a visual line up approach limit of
350 meters.
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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
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Emergency airworthiness directives (EAD), Published by responsible authorities such as
EASA or the FAA
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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
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the most used manuals in a line/hangar environment
The maintenance manual and illustrated parts catalogue
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Aircraft design and manufacture standards are prescribed in the
certification specifications (airworthiness codes)
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A request for an Airworthiness directive alternative means of compliance (AMOC) should be made using an
EASA Form 42
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The annex for Regulation (EU) No 748/2012 is
Part 21
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the authorised certifying staff
can decide whether an aircraft defect hazards seriously the flight safety
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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
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Elimination of damage by replacing parts or appliances without the necessity for design activity is considered
maintenance task requires no approval under Part-21
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CAMO) is part of the EASA’s Implementing Rules EU 1321/ the abbreviation (CAMO) stand for.
Continuing airworthiness management organisation
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The Structural repair SRM manual gives you details of
repair materials and procedures for structures subjected to repairs
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An organisation wishing to design its modifications and repairs must be approved in accordance with
Part-21 aircraft certification
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Certification specifications (CS) are sometimes referred to as
European Aviation Certification Standards (EACS) and airworthiness codes
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Personnel required to be employed in a CAMO are
the accountable manager, the quality manager (to ensure all EASA requirements comply)
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The maintenance programme details should be reviewed at least
annually
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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)
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The CS 22 certificate specifications refer to
Sailplanes and powered sailplanes
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A Part-CAO approved organisation is a ‘combined airworthiness organisation’ exercise the privileges
of both. Part-ML and Part-CAMO organisations and
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The principle of operational suitability data (OSD)
specific data necessary for the safe operation of the aircraft type
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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
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Revision and amendments to manuals which is known as the revision cycle This usually happens
three or four times a year
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Test flight is a mandatory requirement before
issuing a certificate of airworthiness
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ETOPS rules is defined in the
ETOPS manual
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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
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The term “maintenance programme” includes
Scheduled maintenance tasks, associated procedures and standard maintenance practise
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Certification specifications Subpart B deals with
Flight tests to be carried out
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A continuous airworthiness management organisation (CAMO-T) is an organisation approve
under Part-M Subpart G
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An aircraft or engine manufacturer will typically have both
Design organisation approval (DOA) and production organization approval (POA) approvals
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PART CAO applies to
organisations for maintenance and maintenance management of non-complex and non-CAT aircraft
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Subpart K in Part 21 includes
Parts and Appliances
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Part-T relates to the definition of the continuing airworthiness requirements applicable to
third-country registered aircraft
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A check, B check are considered
lighter checks
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A)check detailed inspections performed
Every 500-800 flight hours
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To determine decision height CAT II and CAT III approaches are used
radio altimeter
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Part-M applicable maintenance data is
procedure, standard or information issued by the competent authority and any applicable airworthiness directive
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The unique aspect of the ATA 100-chapter numbers is its relevance for
all aircraft
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Airworthiness review staff carry out a physical survey of the aircraft shall ensure that
all required markings and placards are correctly installed
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The type-certificate and restricted type certificate are both considered to include
The type design and the operating limitations
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D) checks detailed inspections take up
2months to complete
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The engineer guidance regarding minor repair procedures to the aircraft’s structure stated in the
aircraft maintenance manual
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An airworthiness directive contains at least the following information
an identification of the unsafe condition And the affected aircraft
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The holder of the type-certificate or restricted type-certificate shall provide at least
one full set of instructions for continued airworthiness
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The Technical requirements for the design and construction of aircraft engines are found in
EASA Part-21 subpart CS E
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the type certificate holder keep the type certificate valid
through Continuously following airworthiness directives, issuing service bulletins
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The responsible for keeping the data current regarding the type certificate data sheet (TCDS) is
The manufacturer
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The term ‘changes to the type certificate’ is consistently used in
Part 21 Subpart D and E
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Supplemental type certificate is issued following a modification The STC defines
the product design change, states how the modification affects the existing type design
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An independent inspection is an inspection first made by
an authorised person signing the maintenance release
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Vendor service bulletins (VSB) are issued by
equipment or component manufactures
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The letter of agreement is issued for a limited duration
not exceeding one year
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If a certified aircraft has outstanding airworthiness directives that have not been complied with
It is not considered airworthy
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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
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The excess ILS deviation light is coloured
amber and flashing
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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