2.CHAPTER - LIMITATIONS / MAINTENANCE CHECKS
Document: SLSA-MIP-5-4-0-US
Date of Issue: 05/2016
Revision: -
2-7
ANNUAL PERIODICAL INSPECTION OR
INSPECTION AFTER 100 FLIGHT HOURS
Aircraft S/N.:
…………………
Total flight hours:
…………
Registration mark:
…………………
No. of takeoffs:
…………
Type of inspection:
…………………
Page: 1 of 5
Chpt.
Prescribed works
Made by
Checked by
AIRFRAME
3
Fuselage
Visually check surface condition including fiberglass parts -
loosened rivets, deformation, cracks and some other damage.
Check condition of fuselage-wing fairings.
Check condition and attachment of the tailskid.
Check condition and attachment of the canopy.
Check condition and functions of vents.
Check condition of the canopy locks.
Check condition and completeness of emergency equipment.
Check condition of rubber sealing of the cockpit.
Check condition of canopy struts.
4
Wing
Visually check surface condition - loosened rivets,
deformation, cracks and some other damage.
Check play in the wing attachments.
Check condition and attachment of the wing tips.
Check condition of the position lights.
Check conductive wing-fuselage connection.
Aileron
Visually check surface condition - loosened rivets,
deformation, cracks and some other damage.
Check for free travel.
Check hinges.
Check for conductive connection and securing control links.
Flap
Visually check surface condition - loosened rivets,
deformation, cracks and some other damage.
Check for free travel.
Check hinges.
Check condition of the control rods and servo
Check conductive connection.
5
Tail unit
HTU
Summary of Contents for S-LSA
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