Authorization for ferry flight with one engine inoperative.

CFR · 2024-01-01 · US · Title 14

(a) (1) The airplane model has been test flown and found satisfactory for safe flight in accordance with paragraph (b) or (c) of this section, as appropriate. However, each operator who before November 19, 1966, has shown that a model of airplane with an engine inoperative is satisfactory for safe flight by a test flight conducted in accordance with performance data contained in the applicable Airplane Flight Manual under paragraph (a)(2) of this section need not repeat the test flight for that model. (2) The approved Airplane Flight Manual contains the following performance data and the flight is conducted in accordance with that data: (i) Maximum weight. (ii) Center of gravity limits. (iii) Configuration of the inoperative propeller (if applicable). (iv) Runway length for takeoff (including temperature accountability). (v) Altitude range. (vi) Certificate limitations. (vii) Ranges of operational limits. (viii) Performance information. (ix) Operating procedures. (3) The operator has FAA approved procedures for the safe operation of the airplane, including specific requirements for— (i) Limiting the operating weight on any ferry flight to the minimum necessary for the flight plus the necessary reserve fuel load; (ii) A limitation that takeoffs must be made from dry runways unless, based on a showing of actual operating takeoff techniques on wet runways with one engine inoperative, takeoffs with full controllability from wet runways have been approved for the specific model ai

official document · source cfr-2024 · id 14:§ 91.611