What should be checked before installing a component, standard part, or material according to GM1 145.A.42(b)(ii)?

The part number, modification status, limitations, etc., of the component, standard part or material should be checked to ensure they are the ones specified in the applicable maintenance data of the particular aircraft or component where it is going to be installed.

Which regulation is referenced in GM1 145.A.42(b)(ii) as the source for specifying components, standard parts, and materials in maintenance data?

145.A.45(b) is referenced as the regulation that specifies the applicable maintenance data.

GM1 145.A.42(b)(ii) Components

Q: What is the purpose of the check described in GM1 145.A.42(b)(ii) before installing a component?

The check ensures that the part number, modification status, limitations, etc., of the component, standard part or material are the ones specified in the applicable maintenance data of the particular aircraft or component where it is going to be installed.

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GM1 145.A.42(b)(ii) Components

ED Decision 2021/009/R

INSTALLATION OF COMPONENTS

Components, standard parts and materials should only be installed when they are specified in the applicable maintenance data as specified in 145.A.45(b). So, the installation of a component, standard part or material can only be done after checking the applicable maintenance data.

This check should ensure that the part number, modification status, limitations, etc., of the component, standard part or material are the ones specified in the applicable maintenance data of the particular aircraft or component where the component, standard part or material is going to be installed. The organisation should establish procedures to ensure that this check is performed before installation.

Details

Source-Title: GM1 145.A.42(b)(ii) Components View latest amendments

Erulesid: ERULES-1963177438-11593 Compare versions

Domain: Continuing airworthiness

Aircraftcategory: Complex motor-powered aircraft (CMPA), Non-complex motor-powered aircraft (non-CMPA)

Applicabilitydate: 18 May, 2022

Entryintoforcedate: 16 June, 2021

Regulatorysource: ED Decision 2021/009/R Navigate

Regulatorysubject: Part-145

Typeofcontent: GM to IR (Guidance material to implementing rule)

Parentir: 145.A.42 Components

Origin: EASA

Category: EAR