4 of 24
P/N 13772-108
Section 9
Cirrus Design
Supplements
SR22
b.
The autopilot must be disconnect during approach if course
deviation exceeds 50%. The approach should only be
continued by “hand-flying” the airplane.
c.
The autopilot must be disengaged at the Decision Height.
d.
12 knot maximum crosswind component between the missed
approach point and outer marker.
e.
The intercept of the localizer shall occur at least 5 miles
outside of the outer marker.
f.
If the crosswind component is greater than 12 knots and less
than 17 knots, the intercept shall occur at least 10 miles
outside of the outer marker.
g.
The intercept angle shall be no greater than a 45-degree
intercept.
h.
The ILS is flown at normal approach speeds, and within any
STC or TC speed constraints and as defined in this flight
manual.
i.
The flaps should be extended in the approach configuration
prior to the Outer Marker. No further changes in the flap
configuration should be made throughout the autopilot-
coupled approach.
j.
The glideslope is approached in such a manner to allow
automatic arming of the glideslope, or if the glideslope is
manually armed no more than 15% above the glideslope.
10. The S-TEC System Fifty Five X Pilot’s Operating Handbook
,
Serials 0002 thru 0434;
P/N 87109 dated 8 November 2000 or
later OR
Serials 0435 and subsequent;
P/N 87247 original release
or later, must be carried in the airplane and available to the pilot
while in flight.
Revision 5: 08-15-07
