曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Use this procedure to install the left wing or the right wing. Where a part of the procedure applies
to only one wing it will tell you so.
Detail Steps/Work Items Key Items/References
(1) Do the pre-installation check. Refer to Paragraph C.
WARNING: USE 3 PERSONS TO LIFT THE WING. IF YOU DO NOT, YOU CAN
CAUSE INJURY.
CAUTION: DO NOT LIFT ON THE FLAP. YOU CAN DAMAGE THE FLAP.
CAUTION: DO NOT LET THE SPAR STUBS TOUCH THE CENTER SECTION
SHELLS. YOU CAN DAMAGE THE SHELLS.
Note: Until you install the main bolts, one person must lift the wing tip. One person
must lift the leading edge at the root rib. One person must lift the trailing edge
at the root rib.
(2) Lift the wing into position:
S Move the spar stubs part way into the front
and rear main bulkheads.
S Put the electrical cable, Pitot, static and stall
warning tubes through the conduit in the
leading edge of the center section.
S Align the flap inner rib with the transfer pins
on the transfer lever.
S Move the wing fully into the center section to
engage the A and B-bolts and the flap
transfer pins.
Hold the wing in position.
Hold the wing in position.
Hold the wing in position.
(3) Install the main bolts:
S Hold the weight of the wing.
S Install each bolt.
If necessary, move the wing tip a small
amount up and down to help install the
main bolts.
AIRCRAFT
Wings DA 40 Series
AMM
Detail Steps/Work Items Key Items/References
Page 210
20 Sep 2007 57-10-00 Doc # 6.02.01
Rev. 5
(4) Install the locking tubes on the inboard and
outboard main bolts:
S Install the long end piece in one main bolt.
S Move the tube over the long end piece.
S Install the short end piece in the other main
bolt.
S Move the tube over the short end piece.
S Install the bolt, washer and self-locking nut
through the tube and the long end piece.
Refer to Figure 3.
% Torque: hand tight.
(5) Connect these items under the left pilot’s seat:
S The Pitot hose.
S The static hose.
S The stall warning hose.
For left wing only.
The hose is 8 mm (5/16 in) diameter.
(Green color).
The hose is 8 mm (5/16 in) diameter.
(Purple color).
The hose is 10 mm (3/8 in) diameter.
(Transparent).
(6) Connect the electrical connector in the wing
harness.
Left wing: connector P2400, under the
pilot's seat.
Right wing: connector P2401, under the
co-pilot's seat.
(7) Connect the fuel hose(s) in the stub-wing.
(8) Connect the flap push-rod:
S Install the bolt, washer and self-locking nut.
Through the center section rear panel.
Torque: 6.4 Nm (4.7 ft.lb).
(9) Connect the aileron push-rod:
S Install the bolt, washer and self-locking nut.
Through the center section rear panel.
Torque: 6.4 Nm (4.7 ft.lb).
(10) If you must also install the other wing, do items 1
to 9 again for that wing.
(11) Connect the battery. Refer to Section 24-31 (Lycoming
version) or 24-34 (TAE version).
(12) Do a test for correct operation and range of
movement of the flap system. If necessary, adjust
the flap system.
Refer to Section 27-50.
AIRCRAFT
DA 40 Series
AMM
Wings
Detail Steps/Work Items Key Items/References
Doc # 6.02.01
Rev. 5 57-10-00 Page 211
20 Sep 2007
(13) Do an inspection of the flap controls which you
have connected or adjusted.
S If necessary for your airworthiness authority,
do a second inspection of the controls.
(14) Do a test for correct operation and range of
movement of the aileron system. If necessary,
adjust the aileron system.
Refer to Section 27-10.
(15) Do an inspection of the aileron controls which
you have connected or adjusted.
S If necessary for your airworthiness authority,
do a second inspection of the controls.
(16) Do a functional check of these lights:
S Navigation lights.
S Strobe lights (ACL's).
S Taxi light.
S Landing light.
Refer to Section 33-40.
Left wing only.
Left wing only.
(17) Do a functional check of the Pitot heating system. Left wing only.
Refer to Section 34-10.
(18) Do a Pitot and static system leak test. Left wing only.
Refer to Section 34-10.
(19) Refuel the airplane to the unusable fuel level. Refer to Section 12-10.
(20) Do a fuel quantity indication calibration check. Lycoming version only.
Refer to Section 28-40.
(21) Install these items after access:
S The left/right pilots’ seats.
S Main landing gear access panel.
S Center section rear access panel.
S Inboard fuel tank access panel.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：鉆石40系列AMM 2(147)