AMC6 NCC.GEN.131(b)(2) Use of electronic flight bags (EFBs)

• ED Decision 2019/008/R found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Feb 2025)

AMC6 NCC.GEN.131(b)(2) Use of electronic flight bags (EFBs) ED Decision 2019/008/R USE OF COMMERCIAL OFF-THE-SHELF (COTS) POSITION SOURCE COTS position sources may be used for AMMD EFB applications and for EFB applications displaying the own-ship position in-flight when the following considerations are complied with: (a) Characterisation of the receiver: The position should originate from an airworthiness approved GNSS receiver, or from a COTS GNSS receiver fully characterised in terms of technical specifications and featuring an adequate number of channels (12 or more). The EFB application should, in addition to position and velocity data, receive a sufficient number of parameters related to the fix quality and integrity to allow compliance with the accuracy requirements (e.g. the number of satellites and constellation geometry parameters such as dilution of position (DOP), 2D/3D fix). (b) Installation aspects: COTS position sources are C-PEDs and their installation and use should follow the requirements of [NCC.GEN.130](#_DxCrossRefBm927679627). If the external COTS position source transmits wirelessly, cybersecurity aspects have to be considered. (c) Practical evaluation: As variables can be introduced by the placement of the antennas in the aircraft and the characteristics of the aircraft itself (e.g. heated and/or shielded windshield effects), the tests have to take place on the type of aircraft in which the EFB will be operated, with the antenna positioned at the location to be used in service. (1) COTS used as a position source for AMMD The test installation should record the data provided by the COTS position source to the AMMD application. The analysis should use the recorded parameters to demonstrate that the AMMD requirements are satisfactorily complied with in terms of the total system accuracy (taking into account database errors, latency effects, display errors, and uncompensated antenna offsets) within 50 metres (95 %). The availability should be sufficient to prevent distraction or increased workload due to frequent loss of position. When demonstrating compliance with the following requirements of DO-257A, the behaviour of the AMMD system should be evaluated in practice: (i) indication of degraded position accuracy within 1 second (Section 2.2.4 (22)); and (ii) indication of a loss of positioning data within 5 seconds (Section 2.2.4 (23)); conditions to consider are both a loss of the GNSS satellite view (e.g. antenna failure) and a loss of communication between the receiver and the EFB. (2) COTS position source used for applications displaying own-ship position in-flight: Flight trials should demonstrate that the COTS GNSS availability is sufficient to prevent distraction or increased workload due to frequent loss of position. AMC6 NCC.GEN.131(b)(2) Use of electronic flight bags (EFBs) ED Decision 2019/008/R USE OF COMMERCIAL OFF-THE-SHELF (COTS) POSITION SOURCE COTS position sources may be used for AMMD EFB applications and for EFB applications displaying the own-ship position in-flight when the following considerations are complied with: (a) Characterisation of the receiver: The position should originate from an airworthiness approved GNSS receiver, or from a COTS GNSS receiver fully characterised in terms of technical specifications and featuring an adequate number of channels (12 or more). The EFB application should, in addition to position and velocity data, receive a sufficient number of parameters related to the fix quality and integrity to allow compliance with the accuracy requirements (e.g. the number of satellites and constellation geometry parameters such as dilution of position (DOP), 2D/3D fix). (b) Installation aspects: COTS position sources are C-PEDs and their installation and use should follow the requirements of [NCC.GEN.130](#_DxCrossRefBm318087235). If the external COTS position source transmits wirelessly, cybersecurity aspects have to be considered. (c) Practical evaluation: As variables can be introduced by the placement of the antennas in the aircraft and the characteristics of the aircraft itself (e.g. heated and/or shielded windshield effects), the tests have to take place on the type of aircraft in which the EFB will be operated, with the antenna positioned at the location to be used in service. (1) COTS used as a position source for AMMD The test installation should record the data provided by the COTS position source to the AMMD application. The analysis should use the recorded parameters to demonstrate that the AMMD requirements are satisfactorily complied with in terms of the total system accuracy (taking into account database errors, latency effects, display errors, and uncompensated antenna offsets) within 50 metres (95 %). The availability should be sufficient to prevent distraction or increased workload due to frequent loss of position. When demonstrating compliance with the following requirements of DO-257A, the behaviour of the AMMD system should be evaluated in practice: (i) indication of degraded position accuracy within 1 second (Section 2.2.4 (22)); and (ii) indication of a loss of positioning data within 5 seconds (Section 2.2.4 (23)); conditions to consider are both a loss of the GNSS satellite view (e.g. antenna failure) and a loss of communication between the receiver and the EFB. (2) COTS position source used for applications displaying own-ship position in-flight: Flight trials should demonstrate that the COTS GNSS availability is sufficient to prevent distraction or increased workload due to frequent loss of position. ##### AMC6 NCC.GEN.131(b)(2) Use of electronic flight bags (EFBs) *ED Decision 2019/008/R* **USE OF COMMERCIAL OFF-THE-SHELF (COTS) POSITION SOURCE** COTS position sources may be used for AMMD EFB applications and for EFB applications displaying the own-ship position in-flight when the following considerations are complied with: (a) Characterisation of the receiver: The position should originate from an airworthiness approved GNSS receiver, or from a COTS GNSS receiver fully characterised in terms of technical specifications and featuring an adequate number of channels (12 or more). The EFB application should, in addition to position and velocity data, receive a sufficient number of parameters related to the fix quality and integrity to allow compliance with the accuracy requirements (e.g. the number of satellites and constellation geometry parameters such as dilution of position (DOP), 2D/3D fix). (b) Installation aspects: COTS position sources are C-PEDs and their installation and use should follow the requirements of [NCC.GEN.130](#_DxCrossRefBm523089227). If the external COTS position source transmits wirelessly, cybersecurity aspects have to be considered. (c) Practical evaluation: As variables can be introduced by the placement of the antennas in the aircraft and the characteristics of the aircraft itself (e.g. heated and/or shielded windshield effects), the tests have to take place on the type of aircraft in which the EFB will be operated, with the antenna positioned at the location to be used in service. (1) COTS used as a position source for AMMD The test installation should record the data provided by the COTS position source to the AMMD application. The analysis should use the recorded parameters to demonstrate that the AMMD requirements are satisfactorily complied with in terms of the total system accuracy (taking into account database errors, latency effects, display errors, and uncompensated antenna offsets) within 50 metres (95 %). The availability should be sufficient to prevent distraction or increased workload due to frequent loss of position. When demonstrating compliance with the following requirements of DO-257A, the behaviour of the AMMD system should be evaluated in practice: (i) indication of degraded position accuracy within 1 second (Section 2.2.4 (22)); and (ii) indication of a loss of positioning data within 5 seconds (Section 2.2.4 (23)); conditions to consider are both a loss of the GNSS satellite view (e.g. antenna failure) and a loss of communication between the receiver and the EFB. (2) COTS position source used for applications displaying own-ship position in-flight: Flight trials should demonstrate that the COTS GNSS availability is sufficient to prevent distraction or increased workload due to frequent loss of position.