233 

Federal Aviation Administration, DOT 

Pt. 60, App. C 

Required as part of MQTG. 

These tests must be run 

with the motion buffet 

mode disabled. 

See paragraph 6.d., of this 

attachment, Motion cueing 

performance signature. 

3.e.1.

..........

Takeoff (all engines). 

As specified by the sponsor 

for flight simulator qualifica-

tion. 

Ground

...................................

Pitch attitude due to initial 

climb must dominate over 

cab tilt due to longitudinal 

acceleration. 

X 

X 

X 

Associated to test number 

1.c.1. 

3.e.2.

..........

Hover performance (IGE and 

OGE). 

As specified by the sponsor 

for flight simulator qualifica-

tion. 

Ground

...................................

X 

X 

Associated to test number 

1.d. 

3.e.3.

..........

Autorotation (entry). 

As specified by the sponsor 

for flight simulator qualifica-

tion. 

Flight

......................................

X 

X 

Associated to test number 1.i. 

3.e.4.

..........

Landing (all engines). 

As specified by the sponsor 

for flight simulator qualifica-

tion. 

Flight

......................................

X 

X 

X 

Associated to test number 

1.j.1. 

3.e.5.

..........

Autorotation (landing). 

As specified by the sponsor 

for flight simulator qualifica-

tion. 

Flight

......................................

X 

X 

Associated to test number 

1.j.4. 

3.e.6.

..........

Control Response 

3.e.6.a.

.......

Longitudinal

...........................

As specified by the sponsor 

for flight simulator qualifica-

tion. 

Flight

......................................

X 

X 

X 

Associated to test number 

2.c.1. 

3.e.6.b.

.......

Lateral.

...................................

As specified by the sponsor 

for flight simulator qualifica-

tion. 

Ground

...................................

X 

X 

X 

Associated to test number 

2.d.1.a. 

3.e.6.c.

........

Directional

..............................

As specified by the sponsor 

for flight simulator qualifica-

tion. 

X 

X 

X 

Associated to test number 

2.d.1.c. 

3.f.

..............

Characteristic Motion (Vibration) Cues—For all of the following tests, the simulator test results must exhibi

t the overall appear-

ance and trends of the helicopter data, with at least three (3) of the predominant frequency ‘‘spikes’’ being present within 

±

2 

Hz. 

....

....

....

Characteristic motion cues 

may be separate from the 

‘‘main’’ motion system. 

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