Part 145.A.42 Acceptance of Components

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Part 145.A.42(a)

• 145.A.42(a). Are all components classified and appropriately segregated into the following categories?

  Satis

  Level 1

  Level 2

  N/A

  N/R

• 1. Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Subpart Q of Annex I (Part 21) to Regulation (EU) No 748/2012.

• 2. Unserviceable components which shall be maintained in accordance with this section.

• 3. Unsalvageable components which are classified in accordance with point 145.A.42 (d).

• 4. Standard parts used on an aircraft, engine, propeller or other aircraft component when specified in the manufacturers illustrated parts catalogue and/or the maintenance data.

• 5. 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. All material must be accompanied by documentation clearly relating to the particular material and containing a conformity to specification statement plus both the manufacturing and supplier source.

• 6. Components referred to in point 21.A.307 (c) of Annex I (Part 21) to Regulation (EU) No 748/2012.

Part 145.A.42(b)

• 145.A.42(b). Prior to installation of a component does the organisation ensure that the particular component is eligble to be fitted when different modifications and/or airworthiness directive standards may be applicable?

  Satis

  Level 1

  Level 2

  N/A

  N/R

Part 145.A.42(c)

• 145.A.42(c). Does the organisation only fabricate a restricted range of parts to be used in the course of undergoing work within its own facilities and in accordance with procedures in the Exposition?

  Satis

  Level 1

  Level 2

  N/A

  N/R

Part 145.A.42(d)

• 145.A.42(d). Are components which have reached their certified life limit or contain a non-repairable defect classified as unsalvageable and prevented from re-entering the component supply system unless certified life limits have been extended or a repair solution has been approved according to Part-21?

  Yes

  No

  N/A

Part 145.A.42(e)

• 145.A.42(e). Are components referred to in point 21.A.307(c) of the Annex (Part-21) to Regulation (EC) No 1702/2003 only installed if considered eligible for installation by the aircraft owner in its own aircraft?

  Satis

  Level 1

  Level 2

  N/A

  N/R

Procedures Reviewed During Audit

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