Pt. 60, App. A

14 CFR Ch. I (1-1-19 Edition)

states, validation of the effect of the failure
is necessary. Requirements for testing will
be mutually agreed to between the sponsor
and the NSPM on a case-by-case basis.
l. Some tests will not be required for airplanes using airplane hardware in the simulator flight deck (e.g.,  - side stick controller - ). These exceptions are noted in Section 2  - Handling Qualities -  in Table A2A of
this attachment. However, in these cases,
the sponsor must provide a statement that
the airplane hardware meets the appropriate
manufacturer-s specifications and the sponsor must have supporting information to
that fact available for NSPM review.
m. For objective test purposes, see Appendix F of this part for the definitions of  - Near
maximum, -   - Light, -  and  - Medium -  gross
weight.

BEGIN INFORMATION
n. In those cases where the objective test
results authorize a  - snapshot test -  or a  - series of snapshot tests -  results in lieu of a
time-history result, the sponsor or other
data provider must ensure that a steady
state condition exists at the instant of time
captured by the  - snapshot. -  The steady
state condition should exist from 4 seconds
prior to, through 1 second following, the instant of time captured by the snap shot.
o. For references on basic operating
weight, see AC 120-27,  - Aircraft Weight and
Balance; -  and FAA-H-8083-1,  - Aircraft
Weight and Balance Handbook. - 
END INFORMATION
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