Page
29
Section 4
Maintenance & Inspection
Dragonfly 912
FUSELAGE
STEP
INSTRUCTIONS for Assembly, for Disassembly reverse the order!
PART NO.
STAGE CERT.
1
Bolt AN4-27A, 1/4" washer, root supp aft brkt lower,
push rod guide aft root,
Engine Mount Rotax 912,
push rod guide aft root, root supp aft brkt lower, 1/4" washer, AN4 full nut.
Tight.
(Over-tightening this bolt will keep pushrod from moving freely. Re-torque after
pushrod is in place).
DFP 013
DFW 042
2
Bolt AN4-47A, root supp fwd,
saddle fwd root supp aluminium,
root tube, saddle fwd root supp aluminium, root supp, 1/4" washer, AN4 full nut.
Very
tight.
DFK 011
3
Slide
spacer strut 1”,
into root supp aft. . Bolt AN4-24A, 1/4" washer each side, aft root supp brkt upper,
spacer aft root supp 1” x 6.5mm x .3125”,
root supp aft, spacer strut 1”, root supp aft, spacer aft root supp 1” x 6.5mm x .3125”,
aft root supp brkt upper, 1/4" washer, AN4 full nut.
Very tight.
DFG 003
DFP 030
4
5/16 full nut,
bolt mid root tube mount 5/16” x 9.125”,
5/16" washer,
root supp mid,
saddle mid root supp 1.125”,
tang mid root, boom tube, tang mid root, saddle mid root supp 1.125”, root supp mid,
5/16" washer, AN5 full nut.
Very tight.
DFO 007
DFB 002
DFP 009
5
Bolt AN4-47A, 1/4" washer, root supp mid,
saddle mid root supp aluminium,
root tube, saddle mid root supp aluminium, root supp mid, 1/4" washer, AN4 full nut.
Very tight.
DFK 012
6
Bolt AN4-23A, 1/4" washer, flap adjuster assembly,
spacer stand off .375”,
root supp aft, spacer stand off .375”, flap adjuster assembly, 1/4" washer, AN4 half
nut.
Tight.
DFG 008
7
Drill 5/32" hole in bottom centre of saddle mid root supp 1.125” stopping short of bolt
through saddle.
screw pan head 10
#
x 3/4”,
cable clamp 1/4”,
saddle mid root supp 1.125”.
DFT 512
DFT 431
(1)
Recommended Special Tools:
None
(2)
The parts needed to perform the task:
Replace worn/damaged parts as needed, listed above. Max. Wear (defined 1.1.8.1)
(3)
Type of maintenance:
Inspection=Line & Replacement=Heavy
(when it involves replacement of structural components.)
(4)
Certification needed to accomplish the task:
Line=LSRI Inspection or above, Heavy=LSRM Maintenance or above.
see:
3 Level of Certification in this manual
(5)
Detailed instructions and diagrams as needed to perform the task, listed above and adjacent page.
Every Annual or 100 Hrs., Inspect for Cracks, Corrosion, Elongation of holes & Fasteners for Wear & Security.
(6)
Method to test/inspect to verify the task was accomplished properly.
Insure that all procedures were followed correctly
and there is proper non-binding movement to moving parts and that fasteners were tightened as instructed. When flight
controls are involved, assure that they are operating properly.
Section 4 Fuselage
Section 4
Содержание 912 Dragonfly
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