176
14 CFR Ch. I (1–1–14 Edition)
Pt. 60, App. B
T
ABLE
B2F—A
LTERNATIVE
D
ATA
S
OURCES
, P
ROCEDURES
,
AND
I
NSTRUMENTATION
L
EVEL
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.
Information
Objective test reference number
and title
Alternative data sources, procedures, and instrumentation
Notes
2.c.1. ................................................
Handling qualities.
Longitudinal control tests.
Power change force.
Data may be acquired by using an inertial measurement system and a
synchronized video of the calibrated airplane instruments, throttle po-
sition, and the force/position measurements of flight deck controls.
Power change
dynamics test
is acceptable
using the
same data ac-
quisition
methodology.
2.c.2. ................................................
Handling qualities.
Longitudinal control tests.
Flap/slat change force.
Data may be acquired by using an inertial measurement system and a
synchronized video of calibrated airplane instruments, flap/slat posi-
tion, and the force/position measurements of flight deck controls.
Flap/slat change
dynamics test
is acceptable
using the
same data ac-
quisition
methodology.
2.c.4. ................................................
Handling qualities.
Longitudinal control tests.
Gear change force.
Data may be acquired by using an inertial measurement system and a
synchronized video of the calibrated airplane instruments, gear posi-
tion, and the force/position measurements of flight deck controls.
Gear change dy-
namics test is
acceptable
using the
same data ac-
quisition
methodology.
2.c.5. ................................................
Handling qualities.
Longitudinal control tests.
Longitudinal trim.
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 engine instrument
readings.
2.c.6. ................................................
Handling qualities.
Longitudinal control tests.
Longitudinal maneuvering stability
(stick force/g).
Data may be acquired through the use of an inertial measurement sys-
tem and a synchronized video of the 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
Data may be acquired through the use of a synchronized video of the
airplane flight instruments and a hand held force gauge.
2.c.8. ................................................
Handling qualities.
Longitudinal control tests.
Stall Warning (activation of stall
warning device).
Data may be acquired through a synchronized video recording of a
stop watch and the calibrated airplane airspeed indicator. Hand-
record the flight conditions and airplane configuration.
Airspeeds may
be cross
checked with
those in the
TIR and AFM.
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.
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