97
Federal Aviation Administration, DOT
Pt. 60, App. A
T
ABLE
A2E—A
LTERNATIVE
D
ATA
S
OURCES
, P
ROCEDURES
,
AND
I
NSTRUMENTATION
—Continued
QPS REQUIREMENTS
The standards in this table are required if the data gathering methods described in paragraph
9 of
Appendix A are not used.
Information
Table of objective tests
Sim level
Alternative data sources, procedures, and
instrumentation
Notes
Test entry number and title
A
B
2.e.3. Handling qualities. Land-
ings. Crosswind landing.
X
Data may be acquired by using an inertial
measurement system and a syn-
chronized video of calibrated airplane
instruments and force/position measure-
ments of flight deck controls.
2.e.4. Handling qualities. Land-
ings. One engine inoperative
landing.
X
Data may be acquired by using an inertial
measurement system and a syn-
chronized video of calibrated airplane
instruments and the force/position
measurements of flight deck controls.
Normal and lateral accelerations may
be recorded in lieu of AOA and sideslip.
2.e.5. Handling qualities. Land-
ings. Autopilot landing (if ap-
plicable).
..........
X
Data may be acquired by using an inertial
measurement system and a syn-
chronized video of calibrated airplane
instruments and force/position measure-
ments of flight deck controls.Normal
and lateral accelerations may be re-
corded in lieu of AOA and sideslip.
2.e.6. Handling qualities. Land-
ings. All engines operating,
autopilot, go around.
X
Data may be acquired by using an inertial
measurement system and a syn-
chronized video of calibrated airplane
instruments and force/position measure-
ments of flight deck controls. Normal
and lateral accelerations may be re-
corded in lieu of AOA and sideslip.
2.e.7. Handling qualities. Land-
ings. One engine inoperative
go around.
X
Data may be acquired by using an inertial
measurement system and a syn-
chronized video of calibrated airplane
instruments and force/position measure-
ments of flight deck controls. Normal
and lateral accelerations may be re-
corded in lieu of AOA and sideslip.
2.e.8. Handling qualities. Land-
ings. Directional control (rud-
der effectiveness with sym-
metric thrust).
X
Data may be acquired by using an inertial
measurement system and a syn-
chronized video of calibrated airplane
instruments and force/position measure-
ments of flight deck controls. Normal
and lateral accelerations may be re-
corded in lieu of AOA and sideslip.
2.e.9. Handling qualities. Land-
ings. Directional control (rud-
der effectiveness with asym-
metric reverse thrust).
X
Data may be acquired by using an inertial
measurement system and a syn-
chronized video of calibrated airplane
instruments and force/position measure-
ments of flight deck controls. Normal
and lateral accelerations may be re-
corded in lieu of AOA and sideslip.
2.f. Handling qualities. Ground
effect. Test to demonstrate
ground effect.
X
Data may be acquired by using calibrated
airplane instruments, an inertial meas-
urement system, and a synchronized
video of calibrated airplane instruments
and force/position measurements of
flight deck controls.
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