14 C.F.R. § 125.224   Collision avoidance system.


Title 14 - Aeronautics and Space


Title 14: Aeronautics and Space
PART 125—CERTIFICATION AND OPERATIONS: AIRPLANES HAVING A SEATING CAPACITY OF 20 OR MORE PASSENGERS OR A MAXIMUM PAYLOAD CAPACITY OF 6,000 POUNDS OR MORE; AND RULES GOVERNING PERSONS ON BOARD SUCH AIRCRAFT
Subpart F—Instrument and Equipment Requirements

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§ 125.224   Collision avoidance system.

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------------------------------------------------------------------------                                            Then you must operate that        If you operate any . . .                  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 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      (1) TCAS I that meets TSO C- than 33,000 pounds maximum               118, or a later version, or certificated takeoff weight.            (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.------------------------------------------------------------------------

[Doc. No. FAA–2001–10910, 68 FR 15903, Apr. 1, 2003]

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