325
Federal Aviation Administration, DOT
Pt. 60, App. D
Entry
..............................
Rotor Speed—
±
3% Pitch Attitude
±
2
°
Roll Attitude—
±
3
°
Yaw Atti-
tude—
±
5
°
Airspeed—
±
5 kts.
Vertical Velocity—
±
200 fpm
(1.00 m/sec) or 10%.
Cruise;
or
Climb
.......
Record results of a rapid throttle
reduction to idle. If accom-
plished in cruise, results must
be for the maximum range air-
speed. If accomplished in
climb, results must be for the
maximum rate of climb air-
speed at or near maximum
continuous power.
X X
1.j.
..........................
Landing.
1.j.1.
.......................
All Engines
....................
Airspeed—
±
3 kts, Altitude—
±
20 ft
(6.1 m) Torque—
±
3%, Rotor
Speed—
±
1.5%, Pitch Attitude—
±
1.5
°
, Bank Attitude—
±
1.5
°
,
Heading—
±
2
°
, Longitudinal
Control Position—
±
10%, Lat-
eral Control Position—
±
10%,
Directional Control Position—
±
10%, Collective Control Posi-
tion—
±
10%.
Approach
..................
Record results of the approach
and landing profile (running
landing or approach to a
hover). The criteria apply only
to those segments at airspeeds
above effective translational lift.
Record the results from 200 ft
AGL (61 m) to the landing or to
where the hover is established
prior to landing.
X
1.j.2. through 1.j.3
Reserved.
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