445 

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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