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Federal Aviation Regulation Appendix F to Part 36 - Flyover Noise Requirements for Propeller-Driven Small Airplane and Propeller-Driven, Commuter Category Airplane Certification Tests Prior to December 22, 1988
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Appendix F to Part 36 — Flyover Noise Requirements for Propeller-Driven Small Airplane and Propeller-Driven, Commuter Category Airplane Certification Tests Prior to December 22, 1988
F36.1 Scope.
F36.101 General test conditions.
F36.103 Acoustical measurement system.
F36.105 Sensing, recording, and reproducing equipment.
F36.107 Noise measurement procedures.
F36.109 Data recording, reporting, and approval.
F36.111 Flight procedures.
F36.201 Correction of data.
F36.203 Validity of results.
F36.301 Aircraft noise limits.
Section F36.1 Scope. This appendix prescribes noise level limits and procedures for measuring and correcting noise data for the propeller driven small airplanes specified in §§36.1 and 36.501(b).
Sec. F36.101 General test conditions.
Sec. F36.103 Acoustical measurement system. The acoustical measurement system must consist of approved equipment equivalent to the following:
Sec. F36.105 Sensing, recording, and reproducing equipment.
(b) The characteristics of the system must comply with the recommendations in International Electrotechnical Commission (IEC) Publication No. 179, entitled “Precision Sound Level Meters” as incorporated by reference in Part 36 under §36.6 of this part.
Sec. F36.107 Noise measurement procedures.
Sec. F36.109 Data recording, reporting, and approval.
Sec. F36.111 Flight procedures.
Sec. F36.201 Correction of data.
V y =Speed for best rate of climb in the same units as rate of climb.
Sec. F36.203 Validity of results.
Sec. F36.301 Aircraft noise limits.
[Doc. No. 13243, 40 FR 1035, Jan. 6, 1975; 40 FR 6347, Feb. 11, 1975, as amended by Amdt. 36–6, 41 FR 56064, Dec. 23, 1976; Amdt. 36-6, 42 FR 4113, Jan. 24, 1977; Amdt. 36–9, 43 FR 8754, Mar. 2, 1978; Amdt. 36–13, 52 FR 1836, Jan. 15, 1987; Amdt. 36–16, 53 FR 47400, Nov. 22, 1988]
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