BSI 24/30488471 DC:2024 Edition
$13.70
BS EN 4079-008 Aerospace series – Unmanned Aircraft Systems – Part 008: C5 Accessories kits
Published By | Publication Date | Number of Pages |
BSI | 2024 | 29 |
PDF Catalog
PDF Pages | PDF Title |
---|---|
7 | 1 Scope 2 Normative references |
8 | 3 Terms and definitions |
9 | 4 Product requirements and compliance for accessories kit transforming a C3-class UAS into a C5-class UAS 4.1 UA configuration 4.1.1 Requirements 4.1.2 Verification method |
10 | 4.1.3 Pass criteria 4.2 UAS software configuration 4.2.1 Requirements 4.2.2 Verification method 4.2.3 Pass criteria 4.3 UAS original C3 compliance 4.3.1 General 4.3.2 MTOM 4.3.2.1 Requirements 4.3.2.2 Verification method |
11 | 4.3.2.3 Pass criteria 4.3.3 Maximum characteristic dimension 4.3.3.1 Requirements 4.3.3.2 Verification method 4.3.3.3 Pass criteria 4.3.4 Safely controllable 4.3.4.1 Requirements 4.3.4.2 Verification method |
12 | 4.3.4.3 Pass criteria 4.3.5 Tethered UA 4.3.5.1 Requirements 4.3.5.2 Verification method 4.3.5.3 Pass criteria 4.3.6 Power 4.3.6.1 Requirements 4.3.6.2 Verification method 4.3.6.3 Pass criteria 4.3.7 Data link protection 4.3.7.1 Requirements 4.3.7.2 Verification method |
13 | 4.3.7.3 Pass criteria 4.3.8 Conspicuity lightning 4.3.8.1 Requirements 4.3.8.2 Verification method 4.3.8.3 Pass criteria 4.4 Accessories list 4.4.1 Requirements 4.4.2 Verification method 4.4.3 Pass criteria |
14 | 4.5 Accessories installation 4.5.1 Requirements 4.5.2 Verification methods 4.5.3 Pass criteria 4.6 Post-installation C5 compliance 4.6.1 Low speed mode 4.6.1.1 Requirements |
15 | 4.6.1.2 Verification method 4.6.1.3 Pass criteria 4.6.2 C2 link monitoring and alerting 4.6.2.1 Requirements |
16 | 4.6.2.2 Verification method 4.6.2.3 Pass criteria 4.6.3 Accessory kit link monitoring and alerting 4.6.3.1 Requirements |
17 | 4.6.3.2 Verification method 4.6.3.3 Pass criteria 4.6.4 Description of the means to terminate flight 4.6.4.1 Requirements 4.6.4.2 Verification method 4.6.4.3 Pass criteria 4.7 Kit instructions 4.7.1 Requirements 4.7.2 Verification methods |
18 | 4.7.3 Pass criteria |
19 | AnnexĀ A (informative)Example procedure for testing the functionalities of the accessories kit A.1 FTS functionality test A.2 Parachute system functionality test A.3 Other means to reduce the effects of impact dynamics functionality test |
20 | AnnexĀ B (informative)Functionalities added to perform conversion of C3 UA to C5 class B.1 FTS (refer to prENĀ 4709006:2023, AnnexĀ A) |
21 | B.2 Means to reduce the effect of impact dynamics (refer to prENĀ 4709006:2023, AnnexĀ D) |
22 | AnnexĀ C (informative)Accessories kits elements C.1 Accessories kit integration example |
23 | C.2 Details of the parts |
24 | AnnexĀ D (informative)Example of the structure of the accessory kit manual D.1 UA compatibility D.2 Kit components |
25 | D.3 Kit testing D.4 Kit installation D.5 Kit instructions |
26 | D.6 Operation recording |
28 | AnnexĀ ZA (informative)Relationship between this document and the essential requirements of Delegated regulation (EU) 2019/945 of 12th MarchĀ 2019 amended by (EU)Ā 2020/1058 on unmanned aircraft systems and on third-country operators of unmanned aircraft systems aimed to be covered |