Engine Break-In Information; Noise Characteristics - Beechcraft Baron G58 Pilot Operating Handbook

Section 4
Normal Procedures

ENGINE BREAK-IN INFORMATION

Refer to Section 7, SYSTEMS DESCRIPTION.

NOISE CHARACTERISTICS

Approach to and departure from an airport should be made so
as to avoid prolonged flight at low altitude near noise-sensitive
areas. Avoidance of noise-sensitive areas, if practical, is pref-
erable to overflight at relatively low altitudes.
For VFR operations over outdoor assemblies of persons, rec-
reational and park areas, and other noise-sensitive areas,
pilots should make every effort to fly not less than 2000 feet
above the surface, weather permitting, even though flight at a
lower level may be consistent with the provisions of govern-
ment regulations.
The preceding recommended procedures
do not apply where they would conflict with
Air Traffic Control clearances or instruc-
tions, or where, in the pilot's judgement, an
altitude of less than 2,000 feet is necessary
to adequately exercise his duty to see and
avoid other airplanes.
Flyover noise level established in compliance with 14 CFR
Part 36 is:
Using Maximum Continuous Power:
Full Throttle at 2700 RPM . . . . . . . . . . . . . . . . . . . . 77.4 dB(A)
No determination has been made by the Federal Aviation
Administration that the noise level of this airplane is or should
be acceptable or unacceptable for operation at, into, or out of
any airport.
4-56
NOTE
Model G58
June, 2011