Text in force at CAR3-14: from CAR3-0, effective 1 Nov 1949. OCR text
(a) Information relative to the following items of performance shall be included:
(1) The stalling speed, Vso, at maximum weight, (2) The stalling speed, Vs1, at maximum weight and with landing gear and wing flaps retracted, (3) The take-off distance determined in accordance with § 3.84, including the air speed at the 50-foot height, and the airplane configuration, if pertinent, variations in subparagraphs (4) The landing distance determined in accordance with § 3.86, including the airplane configuration, if pertinent, (5) The steady rate of climb determined in accordance with § 3.85 (a), (c), and, as appropriate, (b), including the air speed, power, and airplane configuration, if pertinent. (b) The effect of variation in (a) (2) with angle of bank up to 60 degrees shall be included. (c) The calculated approximate effect of variations in subparagraphs (3), (4) and (5) of this paragraph with altitude and temperature shall be included. SUBPART HIDENTIFICATION DATA [3.791 Identification plate. A fireproof identification plate shall be securely attached to the structure in an accessible location where it will not likely be defaced during normal service. The identification plate shall not be placed in a location where it might be expected to be destroyed or lost in the event of an accident. The identification plate shall contain the identification data required by § 2.36.]