AIRCRAFT MAINTENANCE MANUAL
DFE-AMM-AR1
Rev. 1 – 07/24/2014
2-13
Event
#
Event description
Inspection
Tick off performed inspection
Carried
out by:
Inspected
by:
after the
first
25
hrs.
after the first
50
hrs.
every
50
hrs.
every
100
hrs.
7.2.
Aileron
7.2.1.
Visually check condition
7.2.2.
Check free movement
7.2.3.
Check aileron hinge
7.2.4.
Check play
7.2.5.
Check security of control rod ends
7.2.6.
Check grounding
7.2.7.
Remove inspection covers from the lower
wing surface to inspect security of control
system joints
7.2.8.
Lubricate per Lubricating Chart and reinstall
covers.
7.3.
Flap
7.3.1.
Fully extend the flaps and visually check
condition
7.3.2.
Check flap hinge
7.3.3.
Check play
7.3.4.
Check condition of flap control pin and wear
of the groove at the flap root
7.3.5.
Lubricate per Lubricating Chart
7.4.
Pitot-static tube
7.4.1.
Check pitot-static tube attachment
7.4.2.
Check pitot-static system for leaks - the
airplane manufacturer uses KPU 3
instrument
7.4.3.
Check hoses under pitot-static tube (in bend)
7.4.4.
Check fall sensor of AOA system if installed.
7.4.5.
Check safety system of AOA system if
installed.
7.5.
Wing suspensions
7.5.1.
Remove wing fillets
7.5.2.
Visually check condition of wing suspensions,
7.5.3.
Check wear, corrosion
7.5.4.
Check security of joints
7.6.
Lubricate per Lubricating Chart
8.
FUSELAGE
8.1.
Fuselage surface
8.1.1.
Visually check condition
- no loose rivets, deformations, cracks or any
other damage, corrosion
- repair small damage or contact the airplane
manufacturer
8.1.2.
Visually check rivets near the landing gear
attachment
8.1.3.
Check condition and attachment of
equipment
- antenna, beacon etc. (Inspect ELT for
condition and function per FAR 91.207 (d)
Verify ME 406 registration date and battery
expiration date.)
8.1.4.
Check tail skid attachment
