TSO-C145a 09/19/02 other than those specified in Sections 2.5.2 through 2.5.10 of RTCA/DO-229C constitutes a deviation to this TSO. d. Environmental Qualifications.
Subject: TSO-C129a, AIRBORNE SUPPLEMENTAL NAVIGATION EQUIPMENT USING THE GLOBAL POSITIONING SYSTEM (GPS) DISTRIBUTION: ZVS-326;A-W (IR)-3; A-X(FS)-3; A-X(CD)-4; A-FFS-1,2,7,8(LTD); Department of Transportation Federal Aviation Administration Aircraft Certification Service TSO-C129a Washington ...
TSO-C145a xx/xx/01 Page2 other than those specified in Sections 2.5.2 through 2.5.9 of RTCA/DO-229Cconstitutesa deviation to this TSO. d. Environmental Qualifications.
d Department of Transportation Federal Aviation Administration Aircraft Certification Service Washington, DC TSO-C129a Date: Technical Standard Order Subject: TSO-C129a, Airborne Supplemental Navigation Equipment Using the Global Positioning System (GPS) DISTRIBUTION: ZVS-326;A-W(IR)-3;A-X(FS)-3 ...
FreeFlight Systems was the first to certify WAAS for navigation, in accordance with TSO-C145a, under the auspices of the FAA's Capstone Project and has shipped more than 12 hundred 1201 WAAS sensors to date.
1201, 1204, 1203 GPS/WAAS SENSOR SYSTEMS HIGHLIGHTS •TSO-C145a certified to fulfill ADS-B and TAWS requirements •First to certify an airborne WAAS sensor •Provides position, velocity, and time •Utilizes Fault Detection and Exclusion •Provides positional information to supportsole ...
Class Beta 3 equipment (and Class Beta 1 or Beta 2 that does not claim the noise credit) previously approved under TSO-C145b fully complies with the requirements of this TSO. b. Airborne navigation sensors, using GPS augmented by SBAS approved under TSO-C145a may still be manufactured under the ...
Section 1.3 provides specific guidance for GTN 6XX/7XX installations. 1.1 FAulT DETECTION AND ExCluSION (FDE) The GARMIN G1000 with GIA 63W, the GNS480/CNX80, and the GNS 400W/500W series products incorporate Fault Detection and Exclusion (FDE) features, satisfying the requirements of TSO-C145a/C146a ...
2.2 En Route and Terminal Equipment a) The avionics for GPS equipment must meet Technical Standard Orders (TSO) C129/C129a (any class) issued by the U.S. Federal Aviation Administration (FAA); WAAS equipment must meet FAA TSO-C145a/C145b /C146a/C146b (Class 1, 2 or 3) or equivalent criteria.
FAULT DETECTION AND EXCLUSION (FDE) The GARMIN G1000 with GIA 63W, the GNS480, and the GNS 400W/500W Series products incorporate Fault Detection and Exclusion (FDE) features, satisfying the requirements of TSO-C145a, TSO-C146a, and "GPS Oceanic/Remote Navigation" per FAA AC 20-138A Appendix 1.
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