Pt. 60, App. A

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

TABLE A2E - ALTERNATIVE DATA SOURCES, PROCEDURES, AND INSTRUMENTATION - 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.

kpayne on VMOFRWIN702 with $$_JOB

Table of objective tests

Sim level

Notes
Alternative data sources, procedures, and
instrumentation

Test entry number and title

A

B

2.a.9. Handling qualities. Static
control tests. Brake pedal position vs. force and brake system pressure calibration.

X

X

Use of design or predicted data is acceptable. Data may be acquired by measuring deflection at  - zero -  and  - maximum -  and calculating deflections between the extremes using the airplane
design data curve.

2.c.1. Handling qualities. Longitudinal control tests. Power
change dynamics.

X

X

Data may be acquired by using an inertial
measurement system and a synchronized video of calibrated airplane
instruments and throttle position.

2.c.2. Handling qualities. Longitudinal control tests. Flap/slat
change dynamics.

X

X

Data may be acquired by using an inertial
measurement system and a synchronized video of calibrated airplane
instruments and flap/slat position.

2.c.3. Handling qualities. Longitudinal control tests. Spoiler/
speedbrake change dynamics.

X

X

Data may be acquired by using an inertial
measurement system and a synchronized video of calibrated airplane
instruments and spoiler/speedbrake position.

2.c.4. Handling qualities. Longitudinal control tests. Gear
change dynamics.

X

X

Data may be acquired by using an inertial
measurement system and a synchronized video of calibrated airplane
instruments and gear position.

2.c.5. Handling qualities. Longitudinal control tests. Longitudinal trim.

X

X

Data may be acquired through use of an
inertial measurement system and a synchronized video of flight deck controls
position (previously calibrated to show
related surface position) and the engine
instrument readings.

2.c.6. Handling qualities. Longitudinal control tests. Longitudinal maneuvering stability
(stick force/g).

X

X

Data may be acquired through the use of
an inertial measurement system and a
synchronized video of calibrated airplane instruments; a temporary, high
resolution bank angle scale affixed to
the attitude indicator; and a wheel and
column force measurement indication.

2.c.7. Handling qualities. Longitudinal control tests. Longitudinal static stability.

X

X

Data may be acquired through the use of
a synchronized video of airplane flight
instruments and a hand held force
gauge.

2.c.8. Handling qualities. Longitudinal control tests. Stall
characteristics.

X

X

Data may be acquired through a synchronized video recording of a stop
watch and calibrated airplane airspeed
indicator. Hand-record the flight conditions and airplane configuration.

2.c.9. Handling qualities. Longitudinal control tests. Phugoid
dynamics.

X

X

Data may be acquired by using an inertial
measurement system and a synchronized video of calibrated airplane
instruments and force/position measurements of flight deck controls.

X

Data may be acquired by using an inertial
measurement system and a synchronized video of calibrated airplane
instruments and force/position measurements of flight deck controls.

2.c.10. Handling qualities. Longitudinal control tests. Short
period dynamics.

Information

Airspeeds may be cross
checked with those in the
TIR and AFM.

126

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