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352 

14 CFR Ch. I (1–1–18 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 

3.b. .............

Leg Balance 

Leg Balance ..........................

Based on Simulator Capa-

bility. 

N/A .........................................

Required as part of the 

MQTG. The test must dem-
onstrate motion system leg 
balance as specified by the 
applicant for flight simulator 
qualification. 

X X X 

3.c. ..............

Turn Around 

Turn Around ..........................

Based on Simulator Capa-

bility. 

N/A .........................................

Required as part of the 

MQTG. The test must dem-
onstrate a smooth turn- 
around (shift to opposite di-
rection of movement) of the 
motion system as specified 
by the applicant for flight 
simulator qualification. 

X X X 

3.d. .............

Motion system repeatability 

With the same input signal, 

the test results must be re-
peatable to within ±0.05g 
actual platform linear accel-
eration in each axis. 

Accomplished in both the 

‘‘ground’’ mode and in the 
‘‘flight’’ mode of the motion 
system operation. 

Required as part of the 

MQTG. The test is accom-
plished by injecting a mo-
tion signal to generate 
movement of the platform. 
The input must be such 
that the rotational accelera-
tions, rotational rates, and 
linear accelerations are in-
serted before the transfer 
from helicopter center of 
gravity to the pilot ref-
erence point with a min-
imum amplitude of 5°/sec/ 
sec, 10°/sec and 0.3g, re-
spectively. 

X  See Paragraph 6.c. in this at-

tachment for additional in-
formation. Note: if there is 
no difference in the model 
for ‘‘ground’’ and ‘‘flight’’ 
operation of the motion 
system, this should be de-
scribed in an SOC and will 
not require tests in both 
modes. 

3.e. .............

Motion cueing performance signature 

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