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Annex to Delegated Regulation (EU) 2019/945 · Unmanned Aircraft Systems · Regulations (EU) 2019/947 and 2019/945
PART 1 — Requirements for a class C0 Unmanned aircraft system
A class C0 UAS bears the following class identification label on the UA:
PART 2 — Requirements for a class C1 Unmanned aircraft system
A class C1 UAS bears the following class identification label on the UA:
PART 3 — Requirements for a class C2 Unmanned aircraft system
A class C2 UAS bears the following class identification label on the UA:
PART 4 — Requirements for a class C3 Unmanned aircraft system
A class C3 UAS bears the following class identification label on the UA:
PART 5 — Requirements for a class C4 Unmanned aircraft system
A class C4 UAS bears the following label on the UA in a visible manner:
PART 6 — Requirements for a direct remote identification add-on
A direct remote identification add-on shall comply with the following:
PART 7 — Conformity assessment Module A — Internal production control
Internal production control is the conformity assessment procedure whereby the manufacturer fulfils the obligations set out in points 2, 3 and 4 of this…
PART 8 — Conformity assessment Modules B and C — EU-type examination and conformity to type based on internal production control
When reference is made to this Part, the conformity assessment procedure shall follow Modules B (EU-type examination) and C (Conformity to type based on…
PART 9 — Conformity assessment Module H — Conformity based on full quality assurance
Conformity based on full quality assurance is the conformity assessment procedure whereby manufacturers fulfil the obligations set out in paragraphs 2…
PART 10 — Contents of the technical documentation
The manufacturer shall establish the technical documentation.
PART 11 — EU declaration of conformity
The product (type, batch and serial number). Name and address of the manufacturer or his authorised representative.
PART 12 — Simplified EU declaration of conformity
The simplified EU declaration of conformity referred to in Article 14(3) shall be provided as follows:
PART 13 — Noise test code
This Part lays down the methods of measurement of airborne noise that shall be used for the determination of the measured A-weighted sound power levels…
PART 14 — Indication of the guaranteed sound power level
The indication of the guaranteed sound power level must consist of the single number of the guaranteed sound power in dB, the sign LWA and a pictogram…
PART 15 — Maximum sound power level per class of UA (including transition periods)
UA class MTOM m in gram Maximum sound power level LWA in dB as from entry into force as from 2 years after entry into force as from 4 years after entry…
PART 16 — Requirements for a class C5 unmanned aircraft system and C5 accessories
A class C5 UAS bears the following class identification label on the UA:
PART 17 — Requirements for a class C6 unmanned aircraft system
A class C6 UAS bears the following class identification label on the UA:
Consolidated from the EASA Easy Access Rules (revision 29 Jun 2026, 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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