Pt. 60, App. B

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

TABLE B2F - ALTERNATIVE DATA SOURCES, PROCEDURES, AND INSTRUMENTATION LEVEL 6 FTD - 
Continued
QPS Requirements
The standards in this table are required if the data gathering methods described in paragraph 9 of Appendix
B are not used.
Objective test reference number
and title

Alternative data sources, procedures, and instrumentation

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

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

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

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

2.c.11. ..............................................
Handling qualities.
Longitudinal control tests.
Gear and flap/slat operating times.

May use design data, production flight test schedule, or maintenance
specification, together with an SOC.

2.d.2. ................................................
Handling qualities.
Lateral directional tests.
Roll response (rate).

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

2.d.3. ................................................
Handling qualities.
Lateral directional tests.
(a) Roll overshoot.
OR
(b) Roll response to flight deck roll
controller step input.

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

2.d.4. ................................................
Handling qualities.
Lateral directional tests.
Spiral stability.

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

2.d.6.a. .............................................
Handling qualities.
Lateral directional tests.
Rudder response.

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

2.d.7. ................................................
Handling qualities.
Lateral directional tests.
Dutch roll, (yaw damper OFF).

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

2.d.8. ................................................
Handling qualities.
Lateral directional tests.
Steady state sideslip.

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

ATTACHMENT 3 TO APPENDIX B TO PART 60 - 
FLIGHT TRAINING DEVICE (FTD) SUBJECTIVE
EVALUATION
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BEGIN INFORMATION

kpayne on VMOFRWIN702 with $$_JOB

1. DISCUSSION
a. The subjective tests provide a basis for
evaluating the capability of the FTD to perform over a typical utilization period. The
items listed in the Table of Functions and
Subjective Tests are used to determine
whether the FTD competently simulates

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Notes

each required maneuver, procedure, or task;
and verifying correct operation of the FTD
controls, instruments, and systems. The
tasks do not limit or exceed the authorizations for use of a given level of FTD as described on the SOQ or as approved by the
TPAA. All items in the following paragraphs
are subject to examination.
b. All simulated airplane systems functions will be assessed for normal and, where
appropriate, alternate operations. Simulated
airplane systems are listed separately under
 - Any Flight Phase -  to ensure appropriate
attention to systems checks. Operational

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Information

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