ED Decision 2025/018/R
OPERATIONAL PROCEDURES WITH âMEDIUMâ AND âHIGHâ LEVEL OF ROBUSTNESS
1. Scope of this AMC
1.1 This AMC addresses the criteria for the âmediumâ and âhighâ level of robustness of the operational procedures that are required under the OSO #08: Operational procedures are defined, validated and adhered to.
These criteria may be used to also address the criteria for the âmediumâ and âhighâ level of robustness of the operational procedures required in other sections of the SORA (e.g the mitigations for the ground risk defined in Annex B to AMC1 Article 11 or for the air risk defined in Annex D to Article 11.
2. Criteria for the level of integrity
2.1. Criterion #1: Procedure definition
2.1.1. Annex E to AMC1 Article 11 provides the minimum elements that the operational procedures need to appropriately cover for the UAS operations.
2.1.2. Chapter A.3 of Annex A to AMC1 Article 11 provides an example of an operations manual structure and a table referencing each OM chapter with the OSOs the requirements refer to.
2.2. Criterion #2: Consideration of potential human error
Operational procedures should be developed to minimise human errors:
(a) each of the tasks and the complete sequence of the tasks of a procedure should be intuitive, unambiguous, and clearly defined;
(b) the tasks should be clearly assigned to the relevant roles and persons, ensuring a balanced workload; and
(c) the procedures should adequately address fatigue and stress, considering, among other aspects, the following: duty times, regular breaks, rest periods, the applicable health and safety requirements in the operational environment, handover/takeover procedures, responsibilities, and workload.
2.3 Criterion #3: Emergency response plan (ERP)
For more information regarding the ERP procedure, the UAS operator should refer to AMC3 UAS.SPEC.030(3)(e).
3. Criteria for the level of assurance
3.1. The purpose of the validation process described in this AMC is to confirm whether the proposed operational procedures are complete and adequate to ensure the safe conduct of the intended UAS operations.
3.2. The validation process should include the following:
(a) a review of the completeness of the procedures to ensure that:
(1) all elements that are indicated in points 2.1.1 and 2.1.2 have been addressed; and
(2) all relevant references have been considered, including but not limited to:
(i) the applicable regulations;
(ii) the requirements from the competent authority and/or other relevant authorities or entities;
(iii) the local requirements and conditions;
(iv) the available recommended practices for the intended type of UAS operations;
(v) the instructions from the UAS designer and of any other UAS equipment designer, if applicable;
(vi) the instructions and requirements from externally provided services that support the UAS operations, if applicable;
(vii) the results from previous experience, including tests and/or simulations as those indicated in point (c) and (d); and
(viii) consensus-based voluntary industry standards;
(b) an expert judgement to assess the adequacy of the procedures based on:
(1) the objective(s) of each procedure;
(2) relevant key performance parameters/indicators and/or benchmarking of options, if applicable;
(3) an assessment of the proceduresâ complexity in accordance with point 2.2; and
(4) an assessment of the effect of human factors on procedures in accordance with point 2.2;
(c) a proof of the adequacy of the procedures through tests or practical exercise for phases of the UAS operation other than the UA flight, which involve the UAS and/or any external system that supports the operation;
(d) a proof of the adequacy of the contingency and emergency procedures through:
(1) dedicated flight tests conducted in an area with reduced air and ground risk and/or representative subsystems tests; or
(2) simulation, provided it is proven valid for the intended purpose with positive results; or
(3) any other means acceptable to the competent authority that issues the authorisation;
(e) if the option in point (d)(3) is selected, a substantiation of the suitability of those means for proving the adequacy of the procedures;
(f) a record of proof of the adequacy of the procedures, including at least:
(1) the UAS operatorâs name and registration number;
(2) the date(s) and place(s) of tests or simulations;
(3) identification of the means used, e.g. for tests or simulations that use actual UASs: the type category, the name of the UAS designer, and the model and serial number of each UA used;
(4) a description of tests or simulations conducted, including their purpose, the expected results (including key performance parameters/indicators, where relevant), how they were conducted, the results obtained, and conclusions; and
(5) the signature of the person that is appointed by the UAS operator to conduct the tests or simulations;
(g) for UAS operations that require a âhighâ level of assurance, the procedures and the dedicated flight tests, simulations, or other means acceptable to the competent authority, which are indicated in point 3.2, validated by the competent authority that issues the authorisation or by an entity that is recognised by that competent authority.
3.3. The following conditions apply to the dedicated flight tests that are indicated in point 3.2(d)(1):
(a) the configuration of the UAS hardware and software should be identified;
(b) the UAS operator should conduct the dedicated flight tests;
(c) if no simulations as the ones indicated in point 3.2(d)(2) are conducted, the dedicated flight tests should cover all the relevant aspects of the contingency and emergency procedures;
(d) for UAS operations that require a âhighâ level of assurance, the dedicated flight tests that are performed to validate the procedures and checklists should cover the complete flight envelope or proven to be conservative;
(e) the UAS operator should conduct as many flight tests as agreed with the competent authority to prove the adequacy of the proposed procedures;
(f) the dedicated flight tests should be conducted in a safe environment (reducing the ground and air risks to the greatest extent possible), while ensuring the representativeness of the testsâ results for the intended UAS operations; and
(g) the UAS operator should record the flight tests as part of the information to be recorded as per point UAS.SPEC.050(1)(g), e.g. in a logbook, as indicated in AMC1Â UAS.SPEC.050(1)(g); such a record should include any potential issues identified.
3.4. The UAS operator should reduce the complexity of the procedures as much as possible.
3.4.1. The verification of the complexity of the procedures may include:
(a) an expert judgement, as indicated in point 3.3(b); and
(b) a proof of the adequacy of the procedures, as indicated in point 3.3(c) and (d).
3.4.2. The UAS operator may adopt a method for the evaluation of the complexity of the procedures applied by the relevant personnel, i.e. the remote pilot and/or other personnel in charge of duties essential to the UAS operation. That method should be adequate for the evaluation of the workload that is required by the task(s) of each procedure.
For example, a suitable method for evaluating the workload of the remote pilot and/or other personnel in charge of duties essential to the UAS operation may be the âBedford Workload Scaleâ, which was conceived as a qualitative and relatively simple methodology for rating the pilotsâ workload that is associated with the design of an aircraftâs humanâmachine interface (HMI). However, this methodology is deemed to be adequately generic to be also applicable to the tasks associated with the operational procedures to be conducted by remote pilots and/or other personnel in charge of duties essential to the UAS operation.
Figure 1 depicts the Bedford Workload Scale adapted to operational procedures for UAS operations: âpilotâ is replaced by âremote crew memberâ (i.e. the remote pilot or other personnel in charge of duties essential to the UAS operation), and âpilot decisionâ is replaced by âremote crew member performs a procedure taskâ. A procedure may include one or more tasks.
Figure 1 â Bedford Workload Scale adapted to operational procedures for UAS operations
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