Cessna 182S Pilot Operating Handbook page 347

I
SECTION 9 - SUPPLEMENTS
SUPPLEMENT 15 - FAA APPROVED
SECTION
2
LIMITATIONS
The following autopilot limitations must be adhered to:
CESSNA
MODEL
1B2S
1. The entire preflight test procedure outlined under Section 4,
paragraph A of this supplement, including steps 1 through 7,
must be successfully completed prior to each flight. Use of the
autopilot or manual electric trim system is prohibited prior to
completion of these tests.
2. During autopilot operation, a pilot with seat belt fastened must
be seated at the left pilot position.
3. The autopilot must be OFF during takeoff and landing.
4. The system is approved for Category I operation only
(Approach mode selected).
5. Autopilot maximum airspeed limitation -- 160 KIAS .
Autopilot minimum airspeed limitation -- BO KIAS.
6. Maximum flap extension -- 10°.
7. Maximum fuel imbalance with autopilot engaged -- 90 Ibs.
B. The autopilot must be disengaged below 200 feet AGL during
approach operations and below BOO feet AGL for all other
phases of flight.
9. Overriding the autopilot to change pitch or roll attitude is
prohibited. (Disengage with AlP DISCfTRIM INT or AP .select
button.)
10. The AUTO PILOT circuit breaker must be pulled following any
inflight illuminatiol) of the red "PITCH TRIM " warning
annunciator (located on the airplane annuciator panel), but only
after first completing the Emergency Procedures (Section 3,
paragraph 1.). The manual electric trim and autopilot autotrim
systems will be disabled with the AUTO PILOT circuit breaker
pulled .
S15-14 Revision 3