342 

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 

1.c.3. ...........

One Engine inoperative, re-

jected take off. 

Airspeed—

±

3 kt, Altitude— 

±

20 ft (6.1m), Torque— 

±

3%, Rotor Speed—

±

1.5%, 

Pitch Attitude—

±

1.5

°

, Roll 

angle—

±

1.5

°

, Heading— 

±

2

°

, Longitudinal Control 

Position—

±

10%, Lateral 

Control Position—

±

10%, 

Directional Control Posi-
tion—

±

10%, Collective 

Control Position—

±

10%, 

Distance—

±

7.5% or 

±

30m 

(100ft). 

Ground, Takeoff ....................

Time history from the take off 

point to touch down. Test 
conditions near limiting per-
formance. 

X X 

1.d. .............

Hover 

Performance ..........................

Torque—

±

3%, Pitch Atti-

tude—

±

1.5

°

, Bank Atti-

tude—

±

1.5

°

, Longitudinal 

Control Position—

±

5%, 

Lateral Control Position— 

±

5%, Directional Control 

Position—

±

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. 

X X 

1.e. .............

Vertical Climb 

Performance ..........................

Vertical Velocity—

±

100 fpm 

(0.50 m/sec) or 

±

10%, Di-

rectional Control Position— 

±

5%, Collective Control Po-

sition—

±

5%. 

From OGE Hover ..................

Record results for light and 

heavy gross weights. May 
be a series of snapshot 
tests. 

X X 

1.f. ..............

Level Flight 

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