Pt. 60, App. C

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

TABLE C2E - ALTERNATIVE DATA SOURCES, PROCEDURES, AND INSTRUMENTATION - Continued
[The standards in this table are required if the data gathering methods described in paragraph 9 of Appendix C are not used]
QPS requirements
Table of objective tests

kpayne on VMOFRWIN702 with $$_JOB

Test entry number and title

Level
By
only

1.h.2. Autorotation Performance and Trimmed Flight
Control Positions.
1.j.1. Performance. Running Landing All Engines.

X

1.j.2. Performance. Running Landing One Engine
Inoperative.
1.j.3. Performance. Balked
Landing.

X

2.a.1. Handling Qualities.
Static Control Checks.
Cyclic Controller Position
vs. Force.
2.a.2. Handling Qualities.
Static Control Checks.
Collective/Pedals vs.
Force.
2.a.3. Handling Qualities.
Brake Pedal Force vs.
Position.

X

2.a.4. Handling Qualities.
Trim System Rate (all
applicable systems).
2.a.6. Handling Qualities.
Control System Freeplay.
2.c.1. Longitudinal Handling
Qualities. Control Response.
2.c.2. Longitudinal Handling
Qualities. Static Stability.

X

X

X

X

X

X
X

X

2.c.3.a. Longitudinal Handling Qualities. Dynamic
Stability, Long Term Response.
2.c.3.b. Longitudinal Handling Qualities. Dynamic
Stability, Short Term Response.
2.c.4. Longitudinal Handling
Qualities. Maneuvering
stability.
2.d.1.a. Lateral Handling
Qualities. Control Response.
2.d.1.b Directional Handling
Qualities. Control Response..
2.d.2. Handling Qualities.
Directional Static Stability.

X

2.d.3.a. Handling Qualities.
Dynamic Lateral and Directional Stability LateralDirectional Oscillations.
2.d.3.b. Handling Qualities.
Dynamic Lateral and Directional Stability Spiral
Stability.

X

Information

Alternative data sources, procedures, and instrumentation
Data may be acquired by using a synchronized video of the calibrated helicopter instruments and the force/position measurements of flight deck controls.
Data may be acquired by using a synchronized video of the calibrated helicopter instruments and the force/position measurements of flight deck controls.
Data may be acquired by using a synchronized video of the calibrated helicopter instruments and the force/position measurements of flight deck controls.
Data may be acquired by using a synchronized video of the calibrated helicopter instruments and the force/position measurements of flight deck controls. The synchronized video must record
the time of the  - balk landing -  decision.
Control positions can be obtained using continuous control position
recordings. Force data may be acquired by using a hand held
force gauge so that the forces can be cross-plotted against control position in each of the control axes.
Control positions can be obtained using continuous control position
recordings. Force data may be acquired by using a hand held
force gauge so that the forces can be cross-plotted against control position in each of the control axes.
Brake pedal positions can be obtained using continuous position recordings. Force data may be acquired by using a hand held force
gauge so that the forces can be cross-plotted against brake pedal
position.
Control positions can be obtained using continuous control position
recordings plotted against time to provide rate in each applicable
system.
Data may be acquired by direct measurement.
Data may be acquired by using an inertial measurement system, a
synchronized video of the calibrated helicopter instruments and
the force/position measurements of flight deck controls.
Data may be acquired by using an inertial measurement system, a
synchronized video of the calibrated helicopter instruments and
the force/position measurements of flight deck controls.
Data may be acquired by using an inertial measurement system, a
synchronized video of the calibrated helicopter instruments and
the force/position measurements of flight deck controls.

X

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

X

Data may be acquired by using an inertial measurement system, a
synchronized video of the calibrated helicopter instruments and
the force/position measurements of flight deck controls.
Data may be acquired by using an inertial measurement system, a
synchronized video of the calibrated helicopter instruments and
the force/position measurements of flight deck controls.
Data may be acquired by using an inertial measurement system
and a synchronized video of calibrated helicopter instruments and
force/position measurements of flight deck directional controls.
Data may be acquired by using an inertial measurement system
and a synchronized video of calibrated helicopter instruments and
force/position measurements of flight deck directional controls.
Data may be acquired by using an inertial measurement system
and a synchronized video of the calibrated helicopter instruments,
the force/position measurements of flight deck controls, and a
stop watch.
Data may be acquired by using an inertial measurement system
and a synchronized video of the calibrated helicopter instruments,
the force/position measurements of flight deck controls, and a
stop watch.

X

X

X

X

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Notes