§ 27.175. Demonstration of static longitudinal stability.
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/us/cfr/t14/s§ 27.175·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
(a)Climb. Static longitudinal stability must be shown in the climb condition at speeds from Vy − 10 kt to Vy + 10 kt with—
(1)Critical weight;
(2)Critical center of gravity;
(3)Maximum continuous power;
(4)The landing gear retracted; and
(5)The rotorcraft trimmed at VY.
(b)Cruise. Static longitudinal stability must be shown in the cruise condition at speeds from 0.8 VNE − 10 kt to 0.8 VNE + 10 kt or, if VH is less than 0.8 VNE, from VH −10 kt to VH + 10 kt, with—
(1)Critical weight;
(2)Critical center of gravity;
(3)Power for level flight at 0.8 VNE or VH, whichever is less;
(4)The landing gear retracted; and
(5)The rotorcraft trimmed at 0.8 VNE or VH, whichever is less.
(c)VNE. Static longitudinal stability must be shown at speeds from VNE − 20 kt to VNE with—
(1)Critical weight;
(2)Critical center of gravity;
(3)Power required for level flight at VNE −10 kt or maximum continuous power, whichever is less;
(4)The landing gear retracted; and
(5)The rotorcraft trimmed at VNE − 10 kt.
(d)Autorotation. Static longitudinal stability must be shown in autorotation at—
(1)Airspeeds from the minimum rate of descent airspeed−10 kt to the minimum rate of descent airspeed + 10 kt, with—
(i)Critical weight;
(ii)Critical center of gravity;
(iii)The landing gear extended; and
(iv)The rotorcraft trimmed at the minimum rate of descent airspeed.
(2)Airspeeds from best angle-of-glide airspeed−10 kt to the best angle-of-glide airspeed + 10 kt, with—
(i)Critical weight;
(ii)Critical center of gravity;
(iii)The landing gear retracted; and
(iv)The rotorcraft trimmed at the best angle-of-glide airspeed. (Secs. 313(a), 601, 603, 604, and 605 of the Federal Aviation Act of 1958 (49 U.S.C. 1354(a), 1421, 1423, 1424, and 1425); and sec. 6(c) of the Dept. of Transportation Act (49 U.S.C. 1655(c))) [Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as amended by Amdt. 27-2, 33 FR 963, Jan. 26, 1968; Amdt. 27-11, 41 FR 55468, Dec. 20, 1976; Amdt. 27-14, 43 FR 2325, Jan. 16, 1978; Amdt. 27-21, 49 FR 44433, Nov. 6, 1984; Amdt. 27-34, 62 FR 46173, Aug. 29, 1997; Amdt. 27-44, 73 FR 10999, Feb. 29, 2008]
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- 49 USC 1354(a)
- 49 USC 1655(c)
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§ 27.175
Demonstration of static longitudinal stability.
Cite49 USC 1354(a)
Cite49 USC 1655(c)
Cites 2Cited by 0 across 0 sources