284 

14 CFR Ch. I (1–1–19 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.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.

A

TTACHMENT

3 

TO

A

PPENDIX

B 

TO

P

ART

60— 

F

LIGHT

T

RAINING

D

EVICE

(FTD) S

UBJECTIVE

 

E

VALUATION

 

lllllllllllllllllllllll

B

EGIN

I

NFORMATION

 

1. D

ISCUSSION

 

a. The subjective tests provide a basis for 

evaluating the capability of the FTD to per-
form 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 

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 authoriza-
tions for use of a given level of FTD as de-
scribed on the SOQ or as approved by the 
TPAA. All items in the following paragraphs 
are subject to examination. 

b. All simulated airplane systems func-

tions 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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