344 

14 CFR Ch. I (1–1–19 Edition) 

Pt. 60, App. C 

T

ABLE

C2A—F

ULL

F

LIGHT

S

IMULATOR

(FFS) O

BJECTIVE

T

ESTS

—Continued 

QPS requirements 

Information 

Test 

Tolerance(s) 

Flight condition 

Test details 

Simulator 

level 

Notes 

Entry No. 

Title 

B C D 

Entry ......................................

Rotor Speed—

±

3%, Pitch At-

titude—

±

2

°

, Roll Attitude— 

±

3

°

, Yaw Attitude—

±

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 
the cruise condition is se-
lected, comparison must be 
made for the maximum 
range airspeed. If the climb 
condition is selected, com-
parison must be made for 
the maximum rate of climb 
airspeed at or near max-
imum continuous power. 

X X 

1.j. ...............

Landing 
When the speed range for tests 1.j.1., 1.j.2., or 1.j.3. is less than 40 knots, the applicable airspeed tolerance may be applied to either airspeed or ground speed, as appro-
priate. 

1.j.1. ............

All Engines ............................

Airspeed—

±

3 kts., Altitude— 

±

20 ft. (6.1m), Torque— 

±

3%, Rotor Speed—

±

1.5%, 

Pitch Attitude—

±

1.5

°

, Bank 

Attitude—

±

1.5

°

, Heading— 

±

2

°

, Longitudinal Control 

Position—

±

10%, Lateral 

Control Position—

±

10%, 

Directional Control Posi-
tion—

±

10%, Collective 

Control Position—

±

10%. 

Approach ...............................

Record results of the ap-

proach and landing profile 
as appropriate to the heli-
copter model simulated 
(running landing for Level 
B, or approach to a hover 
for Level C and D). For 
Level B, the criteria apply 
only to those segments at 
airspeeds above effective 
translational lift. 

X X X 

1.j.2. ............

One Engine Inoperative. 

Airspeed—

±

3 kts., Altitude— 

±

20 ft. (6.1m), Torque— 

±

3%, Rotor Speed—

±

1.5%, 

Pitch Attitude—

±

1.5

°

, Bank 

Attitude—

±

1.5

°

, Heading— 

±

2

°

, Longitudinal Control 

Position—

±

10%, Lateral 

Control Position—

±

10%, 

Directional Control Posi-
tion—

±

10%, Collective 

Control Position—

±

10%. 

Approach ...............................

Record results for both Cat-

egory A and Category B 
approaches and landing as 
appropriate to helicopter 
model simulated. For Level 
B, the criteria apply only to 
those segments at air-
speeds above effective 
translational lift. 

X X X 

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