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From the passenger compartment
behind the pilot’s seat.
Torque: 16 Nm (11.8 ft.lb).
(6) Fasten the press-studs which attach the seat
cushion.
(7) Tighten the velcro at the top of the stick gaiter. Make sure that the aileron and elevator
controls are free to move throughout
their range.
% 3. Remove/Install a Pilot's Seat Access Panel (if installed)
% A. Remove a Pilot's Seat Access Panel
% Detail Steps/Work Items Key Items/References
% 1. Remove the cloth coating from the seat.
2. Remove the 12 (10) bolts which attach the
% access panel to the seat.
%
% 3. Move the access panel clear of the airplane.
AIRCRAFT
DA 40 Series
AMM Equipment/Furnishings
Doc # 6.02.01
Rev. 5 25-10-00 Page 203
20 Sep 2007
% B. Install a Pilot's Seat Access Panel
% Detail Steps/Work Items Key Items/References
% 1. Move the access panel in place in the seat.
2. Install the 12 (10) bolts which attach the access
% panel to the seat.
%
% 3. Fasten the cloth coating on the seat.
% 4. Remove/Install the Access Panel of the Passenger Seat (if installed)
% A. Remove the Passenger Seat Access Panel
% Detail Steps/Work Items Key Items/References
(1) Remove the cloth coating from the passenger
% seat.
%
% (2) Remove the 12 fixing bolts of the access panel.
% (3) Remove the access panel.
AIRCRAFT
Equipment/Furnishings
DA 40 Series
AMM
Page 204
20 Sep 2007 25-10-00 Doc # 6.02.01
Rev. 5
% B. Install the Passenger Seat Access Panel
% Detail Steps/Work Items Key Items/References
(1) Put the access panel in place on the passenger
% seat.
%
% (2) Install the access panel with the12 fixing bolts.
% (3) Fasten the cloth coating on the passenger seat.
5. Remove/Install the Passenger Seat
A. Remove the Passenger Seat
Detail Steps/Work Items Key Items/References
(1) Release the press-studs at the front of the seat
cushion.
Refer to Figure 2. Move the cushion
back far enough to give access to the
attaching bolts for the seat.
(2) Remove the 6 bolts with washer plates which
attach the seat pan to the anchor plates.
(3) Remove the 2 bolts with washer plates which
attach the front of the seat pan to the rib on top of
the rear main bulkhead.
(4) Fold the seat-backs forward. Lift the release catch at the left side of
each seat-back.
(5) Remove the 5 bolts with washer plates which
attach the rear of the seat pan to the baggage
compartment frame.
(6) Remove the two seat belt attach points in center
section of seat.
(7) Lift the seat forward and up out of the cockpit.
AIRCRAFT
DA 40 Series
AMM Equipment/Furnishings
Doc # 6.02.01
Rev. 5 25-10-00 Page 205
20 Sep 2007
B. Install the Passenger Seat
Detail Steps/Work Items Key Items/References
(1) Examine the crash elements. Look specially for
delamination and buckling.
Refer to Figure 2.
(2) Do a check for unwanted items in the area below
the seat.
For example: tools.
(3) Put the seat in position in the fuselage with the
seat-backs folded forward.
Lift the release catch at the left side of
each seat-back.
(4) Attach seat belt fastener to center section of seat.
(5) Install the 5 bolts with washer plates which attach
the rear of the seat pan to the baggage
compartment frame.
Torque: 6.4 Nm (4.7 ft.lb).
(6) Install the 6 bolts with washer plates which attach
the seat pan to the anchor plates.
Torque: 16 Nm (11.8 ft.lb).
(7) Install the 2 bolts with washer plates which attach
the front of the seat pan to the rib on top of the
rear main bulkhead.
Torque: 6.4 Nm (4.7 ft.lb).
(8) Fasten the press-studs which hold the seat
cushion.
AIRCRAFT
Equipment/Furnishings
DA 40 Series
AMM
Page 206
20 Sep 2007 25-10-00 Doc # 6.02.01
Rev. 5
6. Remove/Install a Safety Belt
This procedure applies to the pilots' seats and the passenger seat.
A. Remove a Safety Belt
Detail Steps/Work Items Key Items/References
(1) Remove the seat. Refer to Paragraph 2 or 3.
(2) Remove the self-locking nuts, washer plates and
bolts which attach the straps to the seat.
Refer to Figure 3.
For the pilots' seats only:
S Make a note of the position of the
anchor plates which these bolts
also hold.
(3) Move the straps through the holes in the seat pan
and remove them.
(4) Release the bolt and washer which attach the
inertia reel and its cover to the structure.
(5) Release the bolt, washer plate and spring washer
　
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