14 CFR 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:
|If you operate in the United States any . . .||Then you must operate that airplane with:|
|(a) Turbine-powered airplane of more than 33,000 pounds maximum certificated takeoff weight||(1) An appropriate class of Mode S transponder that meets 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 passenger-seat configuration, excluding any pilot seat, or 10-30 seats||(1) TCAS I that meets TSO C-118, or a later version, or(2) A collision avoidance 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.|
[Doc. No. FAA-2001-10910, 68 FR 15903, Apr. 1, 2003]
Title 14 published on 2015-01-01.
No entries appear in the Federal Register after this date, for 14 CFR Part 129.