Text in force at CAR3R-8: from CAR3R-5, effective 1 Oct 1959. OCR text
= * * * * (a) * s fh (2) Power-off and the airplane trimmed at 1.5Vs, or at the minimum trim speed, whichever is higher, (da) It shall be possible to maintain a speed of not more than 1.5Vs, with a pilot control fcrce of not more than 10 pounds during a power-off glide with Janding gear and. wing flaps extended, with the most forward center of gravity position approved at the maximum weight, and regardless of weight.
(e) It shall be possible, without the use of the primary means of longitudinal control, to control the descent of the airPlane with the use of all other normal flight and power controls to a zero rate of descent and to an attitude Suitable for a controlled landing without requiring ex~ ceptional Strength, skill, or alertness on the part of the pilot, or without exceeding the operational and the structural limitations of the airplane. 4. By amending § 3,112 by deleting Paragraph (c) and by amending paraSraph (a) (2) (ii) to read as follows:
(Secs. 313(a), 601, 608, 72 Stat. 752, 775, 776; 49 U.S.C. 1354(a), 1421, 1423) ·