Low-altitude windshear system equipment requirements.

CFR · 2024-01-01 · US · Title 14

(a) (b) (1) The makes/models/series listed below must be equipped with either an approved airborne windshear warning and flight guidance system, an approved airborne detection and avoidance system, or an approved combination of these systems: (i) A-300-600; (ii) A-310—all series; (iii) A-320—all series; (iv) B-737-300, 400, and 500 series; (v) B-747-400; (vi) B-757—all series; (vii) B-767—all series; (viii) F-100—all series; (ix) MD-11—all series; and (x) MD-80 series equipped with an EFIS and Honeywell-970 digital flight guidance computer. (2) All other turbine-powered airplanes not listed above must be equipped with as a minimum requirement, an approved airborne windshear warning system. These airplanes may be equipped with an approved airborne windshear detection and avoidance system, or an approved combination of these systems. (c) (1) Submit a request for approval of a retrofit schedule by June 1, 1990, to the appropriate Flight Standards division manager in the responsible Flight Standards office. (2) Show that all of the certificate holder's airplanes required to be equipped in accordance with this section will be equipped by the final compliance date established for TCAS II retrofit. (3) Comply with its retrofit schedule and submit status reports containing information acceptable to the Administrator. The initial report must be submitted by January 2, 1991, and subsequent reports must be submitted every six months thereafter until completion of the schedule. The repor

official document · source cfr-2024 · id 14:§ 121.358