Effective January 1, 2005, any airplane you operate under this part 125 must be equipped and operated according to the following table:
Collision Avoidance Systems
| If you operate 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 following approved units:
(i) TCAS II that meets TSO C-119b (version 7.0), or 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) Piston-powered airplane of more than 33,000 pounds maximum certificated takeoff weight | (1) TCAS I that meets TSO C-118, or a later version, or
(2) A collision avoidance system equivalent to TSO C-118, or a later version, or
(1)(3) A collision avoidance system and Mode S transponder that meet paragraph (a)(1) of this section. |
authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44705, 44710-44711, 44713, 44716-44717, 44722
source: Docket 19779, 45 FR 67235, Oct. 9, 1980, unless otherwise noted.
cite as: 14 CFR 125.224