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Ground risk mitigations RAE(F) evaluation

M1A Strategic mitigation - sheltering

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Note: Compliance with criterion 2 evaluation of penetration hazard should be assessed by a RAE(F) if you intend to use a UAS that weighs over 25kg and you select M1A.

Criterion Low robustness Medium robustness
1 Evaluation of people at risk CAA CAA
2 Evaluation of penetration hazard CAA if UAS ≤25kg
RAE(F) if UAS >25kg
CAA if UAS ≤25kg
RAE(F) if UAS >25kg

M1B Strategic mitigation using operational restrictions

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Criterion Low robustness Medium robustness High robustness
1 Evaluation of people at risk CAA CAA CAA
2 Impact on at risk population CAA CAA CAA

M1C Tactical mitigations – Ground observation

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Criterion Low robustness
1 Procedures CAA
2 Technical CAA

M2 Effects of UA impact dynamics are reduced

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Criterion Medium robustness High robustness
1 Technical design RAE(F) RAE(F)
2 Procedures RAE(F) RAE(F)
3 Training CAA CAA

Containment requirements

Untethered containment requirements

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Ref Criterion Low robustness Medium robustness High robustness
COR 1    Operational volume containment Operational volume containment CAA RAE(F) RAE(F)
COR 2    End of flight upon exit of the operational volume End of flight upon exit of the operational volume CAA RAE(F) RAE(F)
COR 3    Definition of the ground risk buffer Definition of the ground risk buffer CAA CAA CAA
COR 4    Ground risk buffer containment Ground risk buffer containment N/A RAE(F) RAE(F)

Tethered containment requirements

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Ref Criterion Low robustness Medium robustness High robustness
COT1 Technical requirements RAE(F) RAE(F) RAE(F)
COT2 Procedures RAE(F) RAE(F) RAE(F)

Operational Safety Objectives (OSOs)

This table summarizes the various OSOs at SAIL 3 to 6 where a RAE(F) should be used to demonstrate compliance.

We will evaluate all applicable OSOs at SAILs 1 and 2.

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Ref Requirement SAIL3 SAIL4 SAIL5 SAIL6
OSO 1 Ensure the UAS Operator is competent and/or proven CAA CAA CAA CAA
OSO 2 UAS manufactured by competent and/or proven entity RAE(F) RAE(F) RAE(F) RAE(F)
OSO 3 Criterion 1 UAS maintained by competent and/or proven entity RAE(F) RAE(F) RAE(F) RAE(F)
OSO 3 Criterion 2 UAS maintained by competent and/or proven entity CAA CAA CAA CAA
OSO 4 UAS components are designed to an Airworthiness Standard N/A RAE(F) RAE(F) RAE(F)
OSO 5 UAS is designed considering system safety and reliability RAE(F) RAE(F) RAE(F) RAE(F)
OSO 6 C3 link characteristics RAE(F) RAE(F) RAE(F) RAE(F)

OSO 7 Criterion 1

Conformity check of the UAS configuration RAE(F) RAE(F) RAE(F) RAE(F)

OSO 7 Criterion 2

Conformity check of the UAS configuration CAA CAA CAA CAA
OSO 8 Operational procedures are defined, validated and adhered to CAA CAA CAA CAA
OSO 9 Remote crew trained and current CAA CAA CAA CAA
OSO 13 External services supporting UAS operations are adequate for the operation CAA CAA CAA CAA

OSO 16

Criterion 1 and 2

Multi-crew coordination CAA CAA CAA CAA

OSO 16

Criterion 3

Multi-crew coordination RAE(F) RAE(F) RAE(F) RAE(F)
OSO 17 Remote crew is fit to operate CAA CAA CAA CAA
OSO 18 Automatic protection of the flight envelope from human errors RAE(F) RAE(F) RAE(F) RAE(F)
OSO 19 Safe recovery from human error RAE(F) RAE(F) RAE(F) RAE(F)
OSO 20 Human Factors evaluation RAE(F) RAE(F) RAE(F) RAE(F)
OSO 23 Environmental conditions RAE(F) RAE(F) RAE(F) RAE(F)
OSO 24 UAS designed and qualified for adverse environmental conditions RAE(F) RAE(F) RAE(F) RAE(F)