Federal Aviation Administration, DOT

Pt. 60, App. A

an integration of the parameter(s) in question to obtain a rate of change.

END INFORMATION
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TABLE A2E - ALTERNATIVE DATA SOURCES, PROCEDURES, AND INSTRUMENTATION
QPS REQUIREMENTS
The standards in this table are required if the data gathering methods described in paragraph
9 of
Appendix A are not used.
Table of objective tests

Sim level

kpayne on VMOFRWIN702 with $$_JOB

Notes

Test entry number and title

A

B

Alternative data sources, procedures, and
instrumentation

1.a.1. Performance. Taxi. Minimum Radius turn.

X

X

TIR, AFM, or Design data may be used.

X

Data may be acquired by using a constant
tiller position, measured with a protractor or full rudder pedal application
for steady state turn, and synchronized
video of heading indicator. If less than
full rudder pedal is used, pedal position
must be recorded.

1.a.2. Performance. Taxi Rate
of Turn vs. Nosewheel Steering Angle.

Information

A single procedure may not be
adequate for all airplane
steering systems, therefore
appropriate measurement
procedures must be devised
and proposed for NSPM concurrence.

1.b.1. Performance. Takeoff.
Ground Acceleration Time
and Distance.

X

X

Preliminary certification data may be
used. Data may be acquired by using a
stop watch, calibrated airspeed, and
runway markers during a takeoff with
power set before brake release. Power
settings may be hand recorded. If an inertial measurement system is installed,
speed and distance may be derived
from acceleration measurements.

1.b.2. Performance. Takeoff.
Minimum Control Speed - 
ground (Vmcg) using aerodynamic controls only (per applicable airworthiness standard) or low speed, engine inoperative ground control characteristics.

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.

1.b.3. Performance. Takeoff.
Minimum Unstick Speed (Vmu)
or equivalent test to demonstrate early rotation takeoff
characteristics.

X

X

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

1.b.4. Performance. Takeoff.
Normal Takeoff.

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. AOA can
be calculated from pitch attitude and
flight path.

1.b.5. Performance. Takeoff.
Critical Engine Failure during
Takeoff.

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.

Record airplane dynamic response to engine failure and
control inputs required to correct flight path.

1.b.6. Performance. Takeoff.
Crosswind Takeoff.

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.

The  - 1:7 law -  to 100 feet (30
meters) is an acceptable
wind profile.

Rapid throttle reductions at
speeds near Vmcg may be
used while recording appropriate parameters. The
nosewheel must be free to
caster, or equivalently freed
of sideforce generation.

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