160
14 CFR Ch. I (1–1–14 Edition)
Pt. 60, App. B
T
ABLE
B2A—F
LIGHT
T
RAINING
D
EVICE
(FTD) O
BJECTIVE
T
ESTS
—Continued
QPS requirements
Test
Tolerances
Flight conditions
Test details
FTD
level
Information
Entry No.
Title
5 6
Notes
2.a.9.
........
Brake Pedal Position vs.
Force.
±
5 lb (2.2 daN) or 10%
force.
Ground
................................
Two data points are required: Zero and
maximum deflection. Computer output
results may be used to show compli-
ance.
X
Test not required unless
RTO credit is sought.
2.b.
...........
(Reserved)
2.c.
...........
Longitudinal Control Tests
Power setting is that required for level flight unless otherwise specified.
2.c.1.
........
Power Change Force
..........
±
5 lb (2.2 daN) or,
±
20%
pitch conrol force.
Approach
.............................
May be a series of snapshot test results.
Power change dynamics test as de-
scribed in test 2.c.1 of Table A2A of this
part will be accepted. CCA: Test in Nor-
mal and Non-normal control states.
X X
2.c.2.
........
Flap/Slat Change Force
......
±
5 lb (2.2 daN) or,
±
20%
pitch conrol force.
Takeoff through initial flap
retraction, and approach
to landing.
May be a series of snapshot test results.
Flap/Slat change dynamics test as de-
scribed in test 2.c.2 of Table A2A of this
part will be accepted. CCA: Test in Nor-
mal and Non-normal control states.
X X
2.c.3.
........
(Reserved)
2.c.4.
........
Gear Change Force
............
±
5 lb (2.2 daN) or,
±
20%
pitch conrol force.
Takeoff (retraction) and Ap-
proach (extension).
May be a series of snapshot test results.
Gear change dynamics test as de-
scribed in test 2.c.4 of Table A2A of this
part will be accepted. CCA: Test in Nor-
mal and Non-normal control states.
X X
2.c.5.
........
Longitudinal Trim
................
±
0.5
°
trim surface angle
±
1
°
elevator
±
1
°
pitch angle
±
5% net thrust or equiva-
lent.
Cruise, Approach, and
Landing.
Record steady-state condition with wings
level and thrust set for level flight. May
be a series of snapshot tests Level 5
may use equivalent stick and trim con-
trollers in lieu of elevator and trim sur-
face. CCA: Test in Normal and Non-
normal control states.
X X
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