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(22) Do a check of the aileron range of
movement.
Refer to the Aileron Control System Test
For Correct Range Of Movement.
(23) Do an inspection of all the controls that you
have adjusted.
− If necessary for your airworthiness
authority, do a second inspection of the
controls.
(24) Install these items:
− Pilots seats.
− Fuselage center access panels.
− Aileron bellcrank access panels under
each wing.
Refer to Chapters:
− 25-10
− 52-40
− 52-40
Flight Controls
DA20-C1 AMM
Page 208
19 Dec 1997 27-10-00 Doc # DA201-C1
Rev. 0
4. Aileron Control Rod Access
Aileron Rod Remove/Install Access References
Between the control stick and
the bellcrank at the forward
control bulkhead.
− Pilots seats. Refer to Chapter 25-10
Between the bellcrank at the
forward control bulkhead and
the bellcrank at the aft control
bulkhead.
− Pilots seats.
− Fuselage center access
panels.
− Baggage compartment
floor.
− Fuel Tank.
Refer to Chapters:
− 25-10
− 52.40
− 25-10
− 28-10
Between the bellcrank at the aft
control bulkhead and the
bellcrank in the left/right wing.
− Wing left/right. Refer to Chapter 57-10.
Between the bellcrank in the
left/right wing and the left/right
aileron.
− Aileron bellcrank access
panels under each wing.
Refer to Chapter 52-40
5. Aileron Bellcrank Access
Bellcrank Access References
Bellcrank at the forward control
bulkhead.
Pilots seats. Refer to Chapter 25-10
Bellcrank at the aft control
bulkhead.
− Pilots seats.
− Baggage compartment
floor.
− Fuel Tank.
− Fuselage center access
panels.
Refer to Chapters:
− 25-10
− 25-10
− 28-10
− 52.40
Bellcrank in the left/right wing. − Aileron bellcrank access
panels under each wing.
Refer to Chapter 52-40
DA20-C1 AMM
Flight Controls
Doc # DA201-C1
Rev. 9 27-20-00 Page 1
29 Apr 2004
CHAPTER 27-20
FLIGHT CONTROLS - RUDDER AND TAB
1. General
The DA20-C1 has the usual rudder control system. Each pilot has a rudder pedal assembly. The
pilot can adjust the pedal position. Control cables connect the pedal assembly to the rudder. A
fixed trim tab gives a small amount of adjustment to the rudder trim. You can only adjust the fixed
trim tab on the ground.
Flight Controls
DA20-C1 AMM
Page 2
29 Apr 2004 27-20-00 Doc # DA201-C1
Rev. 9
A
A
B
B
C
D
C
D
Pilot's Rudder
Pedal Assembly
Co-Pilot's Rudder
Pedal Assembly
Forward Control Bulkhead
Teflon Tubes Which
Guide Cockpit Cables
Pulleys
Bottom of B-Bulkhead
Yoke
Turn-Buckles
Aft Fuselage Cables
With Guide Tubes
Rudder Yoke
Figure 1: Rudder Control System
DA20-C1 AMM
Flight Controls
Doc # DA201-C1
Rev. 9 27-20-00 Page 3
29 Apr 2004
2. Description
The DA20-C1 has a set of rudder control pedals for each pilot. The pedal assembly can be
adjusted. Figure 1 shows you the rudder control system. Figure 2 shows you the rudder pedal
assembly. The system has these parts:
− A rudder pedal assembly for each pilot at the front of the cockpit. The forward part of each
pedal connects to a brake master cylinder (Chapter 32-40).
− An adjuster for each pilot attached to the aft face of the rudder pedal assembly.
− A yoke (lever) assembly in the center of the fuselage behind the seats. The yoke attaches to
the bottom of the B-bulkhead.
− A rudder lower mounting-bracket at the rear of the fuselage. The rudder attaches to the
mounting bracket.
− Cable assemblies.
Six bolts attach each rudder pedal assembly to the cockpit floor.
Each rudder pedal assembly has two pedals. Each pedal has a lever and a foot pad. The pedal
has an “S” shaped tube. The lower part of the “S” shaped tube aligns with the pivot of the pedal.
The upper part of the “S” shaped tube aligns with the foot pad of the pedal.
Four control cables (‘Cockpit cables’) go from the firewall to enter the bottom of each “S” shaped
tube. Each cable goes through a tube and comes out at the top. Each cable goes from the pedal
assembly to the yoke in the center fuselage.
Each outboard control cable goes through teflon tubes in the aft face of the floor panel. Each
　
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