Cessna 182 1978 - Elevator Control System

MODEL 182 & T182 SERIES SERVICE MANUAL
SECTION 8
ELEVATOR CONTROL SYSTEM
Page No. Page No.
TABLE
OF CONTENTS Aerofiche/Manual
TABLE OF CONTENTS Aerofiche/Manual
ELEVATOR
CONTROL SYSTEM
. . 1K1/8-1
Bellcrank ...........
1K2/8-2
Description ..........
1K1/8-1 Removal/Installation
...... 1K2/8-2
Trouble
Shooting ........
1K1/8-1
Arm Assembly
.........
1K6/8-6
Control Column
. ........ 1K2/8-2
Removal/Installation ...... 1K6/8-6
Elevators .. . .... . 1K2/8-2
Cables and Pulleys .. .
. .. 1K6/8-
RemovaLInstallation ...... 1K2/8-2 Removal Installtion
Repair ..........
1K2/8-2
Rigging ........... 1K/8
8-1. ELEVATOR CONTROL SYSTEM. (See tube, cables and pulleys. The elevator control cables,
figure 8-1.) at their aft ends, are attached to a bellcrank mounted
on a bulkhead
in the tailcone. A
push-pull tube con-
8-2.
DESCRIPTION. The elevators are operated by
nects this bellcrank to the elevator arm
assembly, in-
power transmitted through fore-and-aft
movement of stalled between the
elevators. An elevator trim tab
the pilot or copilot
control wheels. The system is is
installed in the trailing edge of the right elevator
comprised of control
columns, an elevator torque
and is described in Section 9.
8-3. TROUBLE SHOOTING.
NOTE
Due to remedy procedures in the following trouble shooting
chart it may
be necessary to re-rig system,
refer to para-
graph 8-14.
TROUBLE
PROBABLE
CAUSE REMEDY
NO RESPONSE TO CONTROL Forward or aft end of push-pull Attach push-pull tube correctly.
WHEEL FORE-AND-AFT tube disconnected.
MOVEMENT.
Cables disconnected.
Attach cables and rig system
in
accordance
with paragraph
8-14.
Revision 1 8-1