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21.A.307 The eligibility of parts and appliances for installation

Annex I · Regulation (EU) No 748/2012 · EAR revision 27 Nov 2025

IRImplementing rule

21.A.307The eligibility of parts and appliances for installation

(a)A part or appliance is eligible for installation in a type-certified product when it is in a condition for safe operation, marked in accordance with Subpart Q and accompanied by an authorised release certificate (EASA Form 1), certifying that the item was manufactured in conformity with approved design data.

(b)By way of derogation from point (a) and provided that the conditions in point (c) are met, the following parts or appliances do not require an EASA Form 1 in order to be eligible for installation in a type-certified product:

(1)a standard part;

(2)in the case of ELA1 or ELA2, a part or appliance that is:

(i)not life limited, nor part of the primary structure, nor part of the flight controls;

(ii)identified for installation in the specific aircraft;

(iii)to be installed in an aircraft whose owner has verified compliance with the applicable conditions in (i) and (ii), and has accepted responsibility for this compliance;

(3)a part or appliance for which the consequences of a non-conformity with its approved design data has a negligible safety effect on the product and which is identified as such by the holder of the design approval in the instructions for continued airworthiness. In order to determine the safety effects of a non-conforming part or appliance, the design approval holder may establish in the instructions for continued airworthiness specific verification activities to be conducted by the installer of the part or appliance on the product;

(4)in the case of the embodiment of a standard change in accordance with point 21.A.90B or a standard repair in accordance with point 21.A.431B, a part or appliance, for which the consequences of a non-conformity with its design data have a negligible safety effect on the product, and which is identified as such in the certification specifications for standard changes and standard repairs issued in accordance with point (a)(2) of point 21.A.90B and point (a)(2) of point 21.A.431B. In order to determine the safety effects of a non-conforming part or appliance, specific verification activities to be conducted by the person that installs the part or appliance on the product may be established in the certification specifications referred to above;

(5)a part or appliance that is exempted from an airworthiness approval in accordance with Commission Regulation (EU) No 965/2012 (); and

(6)a part or appliance that is an item of a higher assembly identified in points (b)(1) to (b)(5).

(7)a part or appliance manufactured by a person or organisation referred to in Article 9(4) of this Regulation;

(c)Parts and appliances listed in point (b) are eligible for installation in a type-certified product without being accompanied by an EASA Form 1, provided that the installer holds a document issued by the person or organisation that manufactured the part or appliance, which declares the name of the part or appliance, the part number, and the conformity of the part or appliance with its design data, and which contains the issuance date.

IR · 21.A.307 — Regulation (EU) No 748/2012 · Regulation (EU) 2022/1358 · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

AMCAcceptable means of compliance

AMC1 21.A.307(b)(3)and (b)(4) Verification activities to be conducted on the part or appliance or release documentation prior to installation

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To prevent a non-negligible safety effect on the product, due to the installation of a part or appliance referred to in point 21.A.307(b)(3) and (b)(4) that could potentially not conform to its design, the design approval holder (DAH) or EASA may identify in the ICA (in the case of 21.A.307(b)(3)) or in CS-STAN (in the case of 21.A.307(b)(4)) any specific verification activities to be conducted by the installer on the part or appliance before installing it on the product in accordance with Regulation (EU) No 1321/2014. When assessing the safety effect of a part or appliance identified in point 21.A.307(b)(3) and (b)(4), the DAH or EASA should assume that the installer would conduct, in accordance with Regulation (EU) No 1321/2014, any specific verification activities on the part or appliance or release documentation, as identified in the ICA or in CS-STAN. Example: Information from the DAH contained in the ICA: ‘Part XXX-YY must comply with flammability requirement JJJ-KKK’.

AMC · AMC1 21.A.307(b)(3) — Regulation (EU) No 748/2012 · ED Decision 2021/007/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

GMGuidance material

GM1 21.A.307(b)(3)and (b)(4) Meaning of ‘negligible safety effect’

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For the purpose of 21.A.307(b)(3) and (b)(4), when ‘a part or appliance for which the consequences of non-conformity to its design has a negligible safety effect when installed on the product’ is mentioned, it means that any non-conformity of the part or appliance not identified by the installer that conducted the specific verification activities mentioned in 21.A.307(c):

(a)for ELA1 and ELA2 aircraft, at worst:

(1)slightly reduces the operational or functional certified capabilities of the aircraft or its safety margins;

(2)causes some physical discomfort to its occupants; and

(3)slightly increases the workload of the flight crew; and

(b)for any other aircraft:

(1)has no effect on the operational or functional certified capabilities of the aircraft, or on its safety margins;

(2)causes no physical discomfort to the occupants; and

(3)has no effect on the flight crew.

GM · GM1 21.A.307(b)(3) — Regulation (EU) No 748/2012 · ED Decision 2021/007/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

GMGuidance material

GM1 21.A.307(b)(4)Certification specifications referred to in point 21.A.307(b)(4)

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The corresponding certification specifications issued by EASA and mentioned in point 21.A.307(b)(4) are the Certification Specifications for Standard Changes and Standard Repairs (CS-STAN).

GM · GM1 21.A.307(b)(4) — Regulation (EU) No 748/2012 · ED Decision 2021/007/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

GMGuidance material

GM1 21.A.307(b)(5)Equipment exempted from an airworthiness approval in accordance with Commission Regulation (EU) No 965/2012

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The equipment exempted from an airworthiness approval in accordance with Commission Regulation (EU) No 965/2012 that can be installed during maintenance as new equipment on an aircraft under point 21.A.307(b)(5) is the equipment identified in the following points: CAT.IDE.A.100(a), CAT.IDE.H.100(a), NCC.IDE.A.100(b) and (c), NCC.IDE.H.100(b) and (c), NCO.IDE.A.100(b) and (c), NCO.IDE.H.100(b) and (c), NCO.IDE.S.100(b) and (c), NCO.IDE.B.100(b) and (c), SPO.IDE.A.100(b) and (c), SPO.IDE.H.100(b) and (c), SPO.IDE.S.100(b) and (c), and SPO.IDE.B.100(b) and (c) of Commission Regulation (EU) No 965/2012.

GM · GM1 21.A.307(b)(5) — Regulation (EU) No 748/2012 · ED Decision 2021/007/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

GMGuidance material

GM1 21.A.307(b)(6)Part or appliance that is part of a higher-level assembly

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An EASA Form 1 is not required for a part or appliance when that part or appliance is an element of a higher-level assembly for which an EASA Form 1 is not required.

GM · GM1 21.A.307(b)(6) — Regulation (EU) No 748/2012 · ED Decision 2021/007/R · Initial Airworthiness Easy Access Rules · EAR revision 27 Nov 2025

All rules in SECTION A — TECHNICAL REQUIREMENTS

Consolidated from the EASA Easy Access Rules (revision 27 Nov 2025, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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