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65 

Federal Aviation Administration, DOT 

Pt. 60, App. A 

3.f.4.

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

Buffet with speedbrakes 

deployed.

Simulator test results must 

exhibit the overall appear-

ance and trends of the air-

plane data, with at least 

three (3) of the predomi-

nant frequency ‘‘spikes’’ 

being present within 

±

Hz.

Flight

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

3.f.5.

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

Buffet at approach-to-stall 

Simulator test results must 

exhibit the overall appear-

ance and trends of the air-

plane data, with at least 

three (3) of the predomi-

nant frequency ‘‘spikes’’ 

being present within 

±

Hz.

Flight

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

The test must be conducted for ap-

proach to stall. Post stall characteris-

tics are not required.

3.f.6.

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

Buffet at high airspeeds 

or high Mach.

Simulator test results must 

exhibit the overall appear-

ance and trends of the air-

plane data, with at least 

three (3) of the predomi-

nant frequency ‘‘spikes’’ 

being present within 

±

Hz.

Flight

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

The test may be con-

ducted during either 

a high speed ma-

neuver (e.g., ‘‘wind- 

up’’ turn) or at high 

Mach. 

3.f.7.

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

In-flight vibrations for pro-

peller driven airplanes.

Simulator test results must 

exhibit the overall appear-

ance and trends of the air-

plane data, with at least 

three (3) of the predomi-

nant frequency ‘‘spikes’’ 

being present within 

±

Hz.

Flight (clean configura-

tion).

4. Visual System. 

4.a.

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

Visual System Response Time: (Choose either test 4.a.1. or 4.a.2. to satisfy test 4.a., Visual System Respo

nse Time Test. 

This test also suffices for motion system response timing and flight deck instrument response timing. Motion onset should 

occur before the start of the visual scene change (the start of the scan of the first video field containing different informat

ion) 

but must occur before the end of the scan of that video field. Instrument response may not occur prior to motion onset. 

See additional informa-

tion in this attach-

ment; also see 

Table A1A, entry 

2.g. 

4.a.1.

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

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