MAINTENANCE MANUAL
Page 05-26
Effectivity: All
Issue 2 | Rev. 0
INSPECTION AFTER FIRST 25 FH
Page: 3 of 6
Ref. Prescribed works Made by Checked by
3. NOSE LANDING GEAR
32-20 Check nose landing gear leg for condition and
attachment.
32-20 Check joints for tightening and security.
Tire
12-10 Check pressure; inflate to required pressure as
required.
32-50 Check control rods for condition, rod ends for
security.
4. MAIN LANDING GEAR
Main landing gear legs
32-10 Check fiberglass legs for condition, cracks; repaint
damaged areas. Contact airplane manufacturer if
cracks were found.
32-10 Check joints for tightening and security.
Tires
12-10 Check pressure; inflate to required pressure as
required.
Brakes
12-10 Check brake system for leaks; add brake fluid and
bleed the system if a brake pedal has soft movement.
4. WING
Wing
57-10
57-20
57-30
Check wing structure / skin for condition, loosened
rivets, deformation, cracks, corrosion and some other
damage; contact airplane manufacturer if any
damage were found.
27-10 Check control system joints inside the wing for
security.
Aileron
57-51 Check aileron structure / skin for condition.
Notes:
Date: ........................................ Signature: ........................................