Previous Page Page 333 Next Page  
background image

323 

Federal Aviation Administration, DOT 

Pt. 60, App. D 

1.c.1.

......................

All Engines

....................

Airspeed—

±

3 kt, Altitude—

±

20 ft 

(6.1 m) Torque—

±

3%, Rotor 

Speed—

±

1.5%, Vertical Veloc-

ity—

±

100 fpm (0.50 m/sec) or 

10%, Pitch Attitude—

±

1.5

°

Bank Attitude—

±

2

°

, Heading— 

±

2

°

, Longitudinal Control Posi-

tion—

±

10%, Lateral Control Po-

sition—

±

10%, Directional Con-

trol Position—

±

10%, Collective 

Control Position—

±

10%.

Ground/Takeoff and 

Initial Segment of 

Climb.

Record results of takeoff flight 

path (running takeoff and take-

off from a hover). The criteria 

apply only to those segments 

at airspeeds above effective 

translational lift. Results must 

be recorded from the initiation 

of the takeoff to at least 200 ft 

(61 m) AGL.

1.c.2. through 1.c.3 

Reserved. 

1.d.

........................

Hover. 

Performance

..................

Torque—

±

3%, Pitch Attitude— 

±

1.5

°

, Bank Attitude—

±

1.5

°

Longitudinal Control Position— 

±

5%, Lateral Control Position— 

±

5%, Directional Control Posi-

tion—

±

5%, Collective Control 

Position—

±

5%.

In Ground Effect 

(IGE); and Out of 

Ground Effect 

(OGE).

Record results for light and heavy 

gross weights. May be a series 

of snapshot tests.

1.e.

........................

Vertical Climb. 

Performance

..................

Vertical Velocity—

±

100 fpm (0.50 

m/sec) or 

±

10%, Directional 

Control Position—

±

5%, Collec-

tive Control Position—

±

5%.

From 

OGE 

Hover

.....

Record results for light and heavy 

gross weights. May be a series 

of snapshot tests.

1.f.

.........................

Level Flight. 

Performance and 

Trimmed Flight Con-

trol Positions.

Torque—

±

3% Pitch Attitude— 

±

1.5

° 

Sideslip Angle—

±

2

° 

Lon-

gitudinal Control Position—

±

5% 

Lateral Control position—

±

5% 

Directional Control Position— 

±

5% Collective Control Posi-

tion—

±

5%.

Cruise (Augmentation 

On and Off).

Record results for two gross 

weight and CG combinations 

with varying trim speeds 

throughout the airspeed enve-

lope. May be a series of snap-

shot tests.

This test validates perform-

ance at speeds above 

maximum endurance air-

speed. 

1.g.

........................

Climb. 

VerDate Mar<15>2010 

20:48 Jan 30, 2014

Jkt 232047

PO 00000

Frm 00333

Fmt 8010

Sfmt 8002

Q:\14\14V2.TXT

ofr150

PsN: PC150

  Previous Page Page 333 Next Page