ETSO Deviation

Deviate from ETSO‐C90d and SAE AS36100A Section 8 by using different testing restraint conditions.

Deviate from SAE AS-396B §6.2 “Settling error” test method and associated alignment requirement to use DO-334 § 2.4.7 Multi-Axis Dynamic Accuracy Laboratory Test and selectable category Attitude performance, for Directional Gyro mode.

Deviates from ETSO‐C10b section 3.1.1 by using SAE AS8009 “Pressure Altimeter Systems” Revision B dated September 21st, 2005 instead of SAE AS392C.

Replacement of paragraph 5.5.8 of SAE AS5385C “Cargo Restraint Straps - Design Criteria and Testing Methods” by paragraph 5.5.8 of ISO 16049-1-2013 “Air cargo equipment - Restraint straps - Part 1: Design criteria and test requirements”.

Deviate from ED-73E Chapter 5 to resolve contradictions between given test procedures and corresponding requirements.

Deviate from ED-73E Chapter 5 to resolve contradictions between given test procedures and corresponding requirements.

Deviate from ED-102A to resolve contradictions between given test procedures and corresponding requirements.

Deviates from ETSO‐C88a section 3.1.1 by using EUROCAE ED‐26 dated March 30, 1979 instead of SAE AS 8003.

To deviate from RTCA DO-260B Test 2.4.6.1.2 – Step 2 and to test the equipment with regard to bursts only to the actual behavior of a current (year 2015) TIS-B implementation in the US and to limit the use of the TIS function to the US.

To not system perform TIS-B to TIS-B airborne spatial correlation and to limit the use of the TIS-B function to the US.

Deviate from RTCA DO-283A section 2.2.2.7 by cancelling the offset mode after proceeding from a manually defined (present position) hold.

Deviate from RTCA DO-283A sections 2.2.2.7, 2.2.2.9, and 2.4.3.4 by not implementing fixed-radius transitions.