ICON A5 - Condition and 100-Hour Inspection-Forward Fuselage and Hull

3-16 INSPECTIONS / CONDITION INSPECTIONS AND 100-HOUR INSPECTIONS
ICON A5 / MAINTENANCE MANUAL CHANGE C2
CHAPTER 3
3.3.5 Condition and 100-Hour Inspection—Forward Fuselage and Hull
Correct all unsatisfactory items prior to flight
S=Satisfactory, U=Unsatisfactory
S U Comments
Inspect bulkheads and skins for cracks
Inspect for delaminated skin/voids (Visually check. If
anomalies found, perform tap test See “Manual Tap Test”
on page 3-55.)
Inspect the security of all internal systems
Inspect windows/canopy for cracks and fit
Inspect canopy latching mechanism, hinges, and lock
Check that windshield and windows are bonded to frames
with no delaminations
Inspect rudder pedals and master cylinders for
security/leaks
Check rudder pedal adjust mechanism for correct
function.
(See “Inspect Rudder Pedal Rigging” on page 9-83.)
Inspect wing-to-fuselage root rib for cracks and
delaminations
Inspect systems and structure behind main bulkhead
access panel (fuse box, ECU, relay panel, landing gear,
water rudder actuator, and cables)
Inspect roll cable tension.
(See “Inspect Roll Cable Tension” on page 9-13.)
Check control sticks for freedom of movement
Check flap control operation and flap
actuator/bellcrank/cables
Check control cables, bellcranks and pulleys for corrosion,
attachment, and operation (See “Inspect Control Cables”
on page 9-8.)
Ensure the cockpit instruments are properly marked
Inspect DAC/MSC/instruments/lines for security and
condition