348 

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 

2.b.3.b. .......

Lateral ....................................

Roll Rate—

±

10% or 

±

3

°

/sec., 

Roll Attitude Change— 

±

10% or 

±

3

°

. 

Hover Augmentation On and 

Off. 

Record results for a step con-

trol input. The Off-axis re-
sponse must show correct 
trend for unaugmented 
cases. 

X 

X  This is a ‘‘short time’’ test 

conducted in a hover, in 
ground effect, without en-
tering translational flight, to 
provide better visual ref-
erence. 

2.b.3.c. ........

Directional ..............................

Yaw Rate—

±

10% or 

±

2

°

/sec., 

Heading Change—

±

10% or 

±

2

°

. 

Hover Augmentation On and 

Off. 

Record results for a step con-

trol input. The Off-axis re-
sponse must show correct 
trend for unaugmented 
cases. 

X 

X  This is a ‘‘short time’’ test 

conducted in a hover, in 
ground effect, without en-
tering translational flight, to 
provide better visual ref-
erence. 

2.b.3.d. .......

Vertical ...................................

Normal Acceleration—

±

0.1 g.  Hover Augmentation On and 

Off. 

Record results for a step con-

trol input. The Off-axis re-
sponse must show correct 
trend for unaugmented 
cases. 

X X 

2.c. ..............

Longitudinal Handling Qualities 

2.c.1. ...........

Control Response ..................

Pitch Rate—

±

10% or 

±

2

°

/ 

sec., Pitch Attitude 
Change—

±

10% or 

±

1.5

°

. 

Cruise Augmentation On and 

Off. 

Results must be recorded for 

two cruise airspeeds to in-
clude minimum power re-
quired speed. Record data 
for a step control input. 
The Off-axis response 
must show correct trend for 
unaugmented cases. 

X X X 

2.c.2. ...........

Static Stability ........................

Longitudinal Control Position: 

±

10% of change from trim 

or 

±

0.25 in. (6.3 mm) or 

Longitudinal Control Force 
: 

±

0.5 lb. (0.223 daN) or 

±

10%. 

Cruise or Climb. Autorotation. 

Augmentation On and Off. 

Record results for a minimum 

of two speeds on each side 
of the trim speed. May be 
a series of snapshot tests. 

X X X 

2.c.3. ...........

Dynamic Stability 

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