Title Page
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Conducted on
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Prepared by
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Location
Audit Planning
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The audit is conducted in accordance with the Part-145 requirements applicable at the time of the audit. The regulatory requirements applicable at the time have been checked at www.EASA.europa.eu/regulations on:
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The latest published applicable regulation is recorded as:
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This audit checklist has been confirmed as being reflective of the published regulation (As quoted above) by the auditor named in the report
Audit pre-amble/context
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Audit pre-amble:
Review of previous findings
Review a sample of the findings from the previously accomplished product sample audit. Record the action taken and sample available evidence attesting to the effectivity of the preventative action taken, or otherwise.
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1) Record: Finding reference/preventative action taken/effective yes/no. Attach evidence where applicable.
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2) Record: Finding reference/preventative action taken/effective yes/no. Attach evidence where applicable.
Part-145 compliance with 'components' requirements listed below
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(a) Classification of components. All components shall be classified into the following categories:
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(i) Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Subpart Q of the Annex I (Part-21) to Regulation (EU) No 748/2012, unless otherwise specified in Annex I (Part-21) to Regulation (EU) No 748/2012 or in this Annex II (Part-145)
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(ii) Unserviceable components which shall be maintained in accordance with this Regulation
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u/s components
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(iii) Components categorised as unsalvageable because they have reached their certified life limit or contain a non-repairable defect
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Unsalvageable components
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(iv) Standard parts used on an aircraft, engine, propeller or other aircraft component when specified in the maintenance data and accompanied by evidence of conformity traceable to the applicable standard
Standard parts
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(v) Material, both raw and consumable, used in the course of maintenance when the organisation is satisfied that the material meets the required specification and has appropriate traceability
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All material shall be accompanied by documentation clearly relating to the particular material and containing a conformity to specification statement as well as the manufacturing and supplier source
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Raw materials and consumables
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(b) Components, standard parts and materials for installation
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(i) The organisation shall establish procedures for the acceptance of components, standard parts and materials for installation to ensure that components, standard parts and materials are in satisfactory condition and meet the applicable requirements of point (a)
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Do you have a procedure to verify if the components, standard parts and materials are in satisfactory condition?
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(ii) The organisation shall establish procedures to ensure that components, standard parts and materials shall only be installed on an aircraft or a component when they are in satisfactory condition, meet the applicable requirements of point (a) and the applicable maintenance data specifies the particular component, standard part or material
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(iii) The organisation may fabricate a restricted range of parts to be used in the course of undergoing work within its own facilities, provided procedures are identified in the exposition
Fabrication requirements:
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Review fabrication application p/n
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Workshop tracker: review for usage and correct completion
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(iv) Components referred to in point 21.A.307(c) of the Annex I (Part-21) to Regulation (EU) No 748/2012 shall only be installed if considered eligible for installation by the aircraft owner on its own aircraft
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NA BAMC
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(c) Segregation of components
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(i) Unserviceable and unsalvageable components shall be segregated from serviceable components, standards parts and materials
SEGREGATION OF U/S AND UNSALVAGABLE COMPONENTS
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(ii) Unsalvageable components shall not be permitted to re-enter the component supply system, unless certified life limits have been extended or a repair solution has been approved in accordance with Regulation (EU) No 748/2012