Federal Aviation Administration, DOT

Pt. 60, App. B

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.

kpayne on VMOFRWIN702 with $$_JOB

Objective test reference number
and title

Alternative data sources, procedures, and instrumentation

Notes

2.a.6. ................................................
Handling qualities.
Static control tests.
Pitch trim indicator vs. surface position calibration.

Data may be acquired through calculations.

2.a.8. ................................................
Handling qualities.
Static control tests.
Alignment of power lever angle vs.
selected engine parameter (e.g.,
EPR, N1, Torque, Manifold pressure).

Data may be acquired through the use of a temporary throttle quadrant
scale to document throttle position. Use a synchronized video to
record steady state instrument readings or hand-record steady state
engine performance readings.

2.a.9. ................................................
Handling qualities.
Static control tests.
Brake pedal position vs. force.

Use of design or predicted data is acceptable. Data may be acquired
by measuring deflection at  - zero -  and at  - maximum. - 

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 position, and the force/position measurements of flight deck controls.

Power change
dynamics test
is acceptable
using the
same data acquisition
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 position, and the force/position measurements of flight deck controls.

Flap/slat change
dynamics test
is acceptable
using the
same data acquisition
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 position, and the force/position measurements of flight deck controls.

Gear change dynamics test is
acceptable
using the
same data acquisition
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 system 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. Handrecord the flight conditions and airplane configuration.

283

VerDate Sep<11>2014

Information

16:30 Jun 25, 2019

Jkt 247047

PO 00000

Frm 00293

Fmt 8010

Sfmt 8002

Q:\14\14V2.TXT

PC31

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