ETSO-C145#1 Airborne Navigation Sensors using the GPS augmented by WAAS
Deviate from ETSO-C145 to use RTCA DO-229C (as required in FAA TSO-C145a) instead of RTCA DO-229A.
ETSO-C145#2 Airborne Navigation Sensors using the GPS augmented by WAAS
Deviate from RTCA DO-229C, Paragraph 2.5.9: Integrity Monitoring Test Procedures.
ETSO-C145#3 Airborne Navigation Sensors using the GPS augmented by WAAS
Deviate from RTCA DO-229C, Paragraph 2.5.4: Initial Acquisition Time Test.
ETSO-C145#4 Airborne Navigation Sensors using the GPS augmented by WAAS
Deviate from RTCA DO-229C, Paragraph 2.5.6: Satellite Reacquisition Test.
ETSO-C145#5 Airborne Navigation Sensors using the GPS augmented by WAAS
Deviate from RTCA DO-229C, Paragraph 2.1.4.2.2.4: Wide Area Augmentation System (WAAS) Precision Approach (PA) RAIM Availability for Vertical Alert Limit (VAL) of 15m.
ETSO-C145#6 Airborne Navigation Sensors using the GPS augmented by WAAS
Deviate from RTCA DO-229C, paragraph 2.5.9: RAIM Test Procedures with Selective Availability (SA) Off.
ETSO-C145#7 Airborne Navigation Sensors using the GPS augmented by WAAS
Deviate from RTCA DO-229C paragraph 2.5.8: Accuracy Test.
