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switch.
Do a continuity test of the
wiring. Refer to Chapter 92 for
the wiring diagrams.
AIRCRAFT
Doors DA 40 Series
AMM
Page 102
20 Sep 2007 52-10-00 Doc # 6.02.01
Rev. 5
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AIRCRAFT
DA 40 Series
AMM
Doors
Doc # 6.02.01
Rev. 5 52-10-00 Page 201
20 Sep 2007
Maintenance Practices
1. General
These maintenance practices tell you how to install and remove the canopy and passenger door. They
also tell you how to test and adjust the locking mechanism.
2. Remove/Install the Canopy
A. Remove the Canopy
Detail Steps/Work Items Key Items/References
(1) Open the canopy:
S Pull the canopy handle away from the canopy
frame.
S Lift the canopy open.
Refer to Figure 3.
(2) S/N’s through 40.051:
S Remove the two nuts, washers and bolts
which attach the canopy to the hinge frame.
S/N’s 40.052 and subsequent:
S Remove the four nuts, washers and bolts
which attach the canopy to the hinge frame
bracket.
Refer to Figure 1.
Hold the canopy!
Refer to Figure 2.
Hold the canopy!
(3) Disconnect the plug for the flood light.
(4) Lift the canopy clear of the airplane. Use two persons.
AIRCRAFT
Doors DA 40 Series
AMM
Page 202
20 Sep 2007 52-10-00 Doc # 6.02.01
Rev. 5
B. Install the Canopy
Detail Steps/Work Items Key Items/References
(1) Lift the canopy into position on the airplane. Use two persons.
(2) Engage the tapered ends of the hinge frame in
the tubular brackets on the canopy frame.
Refer to Figure 3.
(3) S/N’s through 40.051:
S Install the two bolts, washers and nuts which
attach the canopy to the hinge frame.
S/N’s 40.052 and subsequent:
S Install the four bolts, washers and nuts which
attach the canopy to the hinge frame bracket.
(4) Connect the plug for the flood light.
(5) Close the canopy.
(6) Operate the canopy lock:
S Hold the canopy closed.
S Push the canopy handle towards the canopy
frame.
S Push up on the rear of the canopy frame.
When the canopy is locked, the canopy
handle must be flush with the canopy
frame.
To make sure that the canopy is locked.
(7) Do a test for correct operation of the door
unlocked warning light (DOOR or DOORS).
Refer to Paragraph 6 in this Section.
AIRCRAFT
DA 40 Series
AMM
Doors
Doc # 6.02.01
Rev. 5 52-10-00 Page 203
20 Sep 2007
3. Remove/Install the Gas Spring Strut for the Canopy
A. Remove the Gas Spring Strut for the Canopy
Detail Steps/Work Items Key Items/References
(1) Remove the canopy. Refer to Paragraph 2.
(2) Remove the nut and washer that attach the strut
to the hinge frame.
Refer to Figure 1 (S/N's through
40.051) or Figure 2 (S/N's 40.052 and
subsequent).
WARNING: MAKE SURE THAT THE STRUT IS FULLY EXTENDED BEFORE YOU
DISCONNECT IT FROM THE HINGE FRAME.
(3) Pull the top of the strut away from the hinge
frame.
Catch the bush and second washer.
(4) Remove these items that attach the bottom of the
strut:
S Nut, washer and bolt.
S Bush.
S Two polyamide spacers.
(5) Remove the strut from the airplane.
B. Install the Gas Spring Strut for the Canopy
Detail Steps/Work Items Key Items/References
(1) Put the strut in position in the airplane. The cylinder goes to the top.
(2) Install the bolt, washer and self-locking nut at the
bottom attachment to the firewall.
Torque 6.4 Nm (4.7 ft.lb.).
Use a new self-locking nut.
(3) Put the washer and bush in position on the hinge
frame.
(4) Move the top eye-end of the strut over the bush
on the hinge frame.
(5) Install the washer and self-locking nut to the
hinge frame.
Torque 6.4 Nm (4.7 ft.lb.).
Use a new self-locking nut.
(6) Install the canopy. Refer to Paragraph 2.
AIRCRAFT
Doors DA 40 Series
AMM
Page 204
20 Sep 2007 52-10-00 Doc # 6.02.01
Rev. 5
4. Remove/Install the Passenger Door
A. Remove the Passenger Door
Detail Steps/Work Items Key Items/References
(1) Open the passenger door:
S Push and hold the safety button next to the
door handle.
S Pull the door handle away from the door
frame.
S Lift the door open.
Refer to Figure 4.
(2) Remove the gas strut:
S Remove the locking clips from the gas strut
top and bottom ball-end fittings.
S Pull the gas strut off the ball end fittings on
the fuselage and clear of the airplane.
Hold the door!
(3) Remove the passenger reading light assembly
　
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