Cessna 182S Pilot Operating Handbook page 353

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 15 - FAA APPROVED
CESSNA
MODEL 182S
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NOTE
The following procedures apply to airplane serials
18280165 thru 18280944 incorporating Honeywell
Service Bulletin KC140-M1.
The following voice messages will be annunciated as conditions
warrant:
1. "TRIM IN MOTION, TRIM IN MOTION" - Elevator trim
running for more than 5 seconds.
2. "CHECK PITCH TRIM" - An out of trim condition has existed
for 16 seconds.
A. Airplane Control Wheel -- GRASP FIRMLY and regain
aircraft control.
B. AlP DISCfTRIM INT Switch -- PRESS and HOLD
throughout recovery.
C. AIRCRAFT -- RE-TRIM manually as needed.
D. AUTO PILOT Circu it Breaker -- PULL.
SECTION 4
NORMAL PROCEDURES
A. PREFLIGHT (PERFORM PRIOR TO EACH FLIGHT):
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1. AVIONICS MASTER Switch -- ON.
2. POWER APPLICATION AND SELF-TEST -- A self-test is
performed upon power application to the computer. This test
. is a sequence of internal checks that validate proper system
operation prior to allowing normal system operation. The
sequence is indicated by "PFT" with an increasing number for
the sequence steps. Successful completion of self-test is
identified by all display segments being illuminated (Display
Test). external "Pitch Trim" (AiC System Annunciator Panel)
being illuminated. and the disconnect tone sounding.
S15-20
Revision 3