Federal Aviation Administration, DOT

Pt. 36, App. H

spaschal on DSK3GDR082PROD with CFR

angle q (theta) relative to their respective
flight paths.
(c) Level flyover profiles. (1) The noise type
certification level flyover profile is shown in
Figure H2. Airspeed must be stabilized within Section5 knots of the reference airspeed deter-

mined using the procedures in section
H36.3(d). The number of level flights made
with a headwind component must be equal to
the number of level flights made with a tailwind component.

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