[Code of Federal Regulations] [Title 14, Volume 2] [Revised as of January 1, 2007] From the U.S. Government Printing Office via GPO Access [CITE: 14CFR129.18] [Page 1025-1026] TITLE 14--AERONAUTICS AND SPACE CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) PART 129_OPERATIONS: FOREIGN AIR CARRIERS AND FOREIGN OPERATORS OF U.S.-REGISTERED AIRCRAFT ENGAGED IN COMMON CARRIAGE--Table of Contents Sec. 129.18 Collision avoidance system. Effective January 1, 2005, any airplane you, as a foreign air carrier, operate under part 129 must be equipped and operated according to the following table: Collision Avoidance Systems ------------------------------------------------------------------------ If you operate in the United States any Then you must operate that . . . airplane with: ------------------------------------------------------------------------ (a) Turbine-powered airplane of more (1) An appropriate class of than 33,000 pounds maximum Mode S transponder that meets certificated takeoff weight. Technical Standard Order (TSO) C-112, or a later version, and one of the followign approved units; (i) TCAS II that meets TSO C- 119b (version 7.0), or takeoff weight a later version. (ii) TCAS II that meets TSO C- 119a (version 6.04A Enhanced) that was installed in that airplane before May 1, 2003. If that TCAS II version 6.04A Enhanced no longer can be repaired to TSO C-119a standards, it must be replaced with a TCAS II that meets TSO C-119b (version 7.0), or a later version. (iii) A collision avoidance system equivalent to TSO C- 119b (version 7.0), or a later version, capable of coordinating with units that meet TSO C-119a (version 6.04A Enhanced), or a later version. (b) Turbine-powered airplane with a (1) TCAS I that meets TSO C- passenger-seat configuration, 118, or a later version, or excluding any pilot seat, or 10-30 (2) A collision avoidance seats. system equivalent to excluding any TSO C-118, or a later version, or (3) A collision avoidance system and Mode S transponder that meet paragraph (a)(1) of this section. ------------------------------------------------------------------------ [[Page 1026]] [Doc. No. FAA-2001-10910, 68 FR 15903, Apr. 1, 2003]