59
Federal Aviation Administration, DOT
Pt. 60, App. A
2.d.8.
.............
Steady State Sideslip
.....
For given rudder position
±
2
°
bank angle,
±
1
°
side-
slip angle,
±
10% or
±
2
°
ai-
leron,
±
10% or
±
5
°
spoiler
or equivalent roll, con-
troller position or force.
Additionally, for those sim-
ulators of airplanes with
reversible flight control
systems:
±
10% or
±
3 lb
(1.3 daN) wheel force
±
10% or
±
5 lb (2.2 daN)
rudder pedal force.
Approach
or
Landing
...
Use at least two rudder positions, one of
which must be near maximum allow-
able rudder. Propeller driven airplanes
must test in each direction. May be a
series of snapshot test results.
X X X X
2.e.
................
Landings.
2.e.1.
.............
Normal Landing
..............
±
3 kt airspeed,
±
1.5
°
pitch
angle,
±
1.5
°
angle of at-
tack,
±
10% or
±
10 ft (3 m)
height. Additionally, for
those simulators of air-
planes with reversible
flight control systems:
±
10% or
±
5 lbs (
±
2.2 daN)
stick/column force.
Landing
........................
Record results from a minimum of 200 ft
(61 m) AGL to nosewheel touchdown.
CCA: Test in Normal and Non-normal
control states.
X
X
X
Tests should be con-
ducted with two nor-
mal landing flap set-
tings (if applicable).
One should be at or
near maximum cer-
tificated landing
weight. The other
should be at light or
medium landing
weight.
2.e.2.
.............
Minimum Flap Landing
...
±
3 kt airspeed,
±
1.5
°
pitch
angle,
±
1.5
°
angle of at-
tack,
±
10% or
±
10 ft (3 m)
height. Additionally, for
those simulators of air-
planes with reversible
flight control systems:
±
10% or
±
5 lbs (2.2 daN)
stick/column force.
Minimum Certified
Landing Flap Con-
figuration.
Record results from a minimum of 200 ft
(61 m) AGL to nosewheel touchdown
with airplane at near Maximum Land-
ing Weight.
X X
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