224 

14 CFR Ch. I (1–1–14 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 applie

d 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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