§ 29.29. Empty weight and corresponding center of gravity.
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/us/cfr/t14/s§ 29.29·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
(a)The empty weight and corresponding center of gravity must be determined by weighing the rotorcraft without the crew and payload, but with—
(1)Fixed ballast;
(2)Unusable fuel; and
(3)Full operating fluids, including—
(i)Oil;
(ii)Hydraulic fluid; and
(iii)Other fluids required for normal operation of rotorcraft systems, except water intended for injection in the engines.
(b)The condition of the rotorcraft at the time of determining empty weight must be one that is well defined and can be easily repeated, particularly with respect to the weights of fuel, oil, coolant, and installed equipment. (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. 5084, 29 FR 16150. Dec. 3, 1964, as amended by Amdt. 29-15, 43 FR 2326, Jan. 16, 1978]
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- 49 USC 1354(a)
- 49 USC 1655(c)
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§ 29.29
Empty weight and corresponding center of gravity.
Fed. Reg.×1
Cite49 USC 1354(a)
Cite49 USC 1655(c)
Cites 2Cited by 1 across 1 source