162
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.c.10.
......
Short Period Dynamics
.......
±
1.5
°
pitch angle or
±
2
°
/sec
pitch rate,
±
0.10g accel-
eration..
Cruise
..................................
CCA: Test in Non-normal control state.
X
2.d.
...........
Lateral Directional Tests
Power setting is that required for level flight unless otherwise specified.
2.d.1.
........
(Reserved)
2.d.2.
........
Roll Response (Rate)
.........
±
10% or
±
2
°
/sec roll rate
....
Cruise, and Approach or
Landing.
Record results for normal roll controller
deflection (one-third of maximum roll
controller travel). May be combined with
step input of flight deck roll controller
test (see 2.d.3.).
X X
2.d.3.
........
Roll Response to Flight
deck Roll Controller Step
Input.
±
10% or
±
2
°
bank
angle
.....
Approach
or
Landing
..........
Record from initiation of roll through 10
seconds after control is returned to neu-
tral and released. May be combined
with roll response (rate) test (see
2.d.2.). CCA: Test in Non-normal con-
trol state.
X
2.d.4.a.
.....
Spiral Stability
.....................
Correct trend and
±
3
°
or
±
10% bank angle in 30
seconds.
Cruise
..................................
Record results for both directions. As an
alternate test, demonstrate the lateral
control required to maintain a steady
turn with a bank angle of 30
°
. CCA:
Test in Non-normal control state.
X
Airplane data averaged
from multiple tests in
same direction may be
used.
2.d.4.b.
.....
Spiral Stability
.....................
Correct trend
.......................
Cruise
..................................
C
CA: Test in Non-normal control state.
X
Airplane data averaged
from multiple tests in
same direction may be
used.
2.d.5.
........
(Reserved)
VerDate Mar<15>2010
20:48 Jan 30, 2014
Jkt 232047
PO 00000
Frm 00172
Fmt 8010
Sfmt 8002
Q:\14\14V2.TXT
ofr150
PsN: PC150