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RA - FLUGZEUGBAU GmbH
SERVICE MANUAL EXTRA 200
CHAPTER 05
PAGE 25
PAGE DATE: 1. July 1996
O 11 Check main bolt sleeves for secure bonding to the spar.
Wing trailing edge
O 12 Check bonding top/bottom for cracks and delaminations by coin
tapping (Refer to Chapter 20-10-05).
Root and Tip
O 13 Check root rib for cracks, delaminations and secure bonding to skin
and spars by coin tapping (Refer to Chapter 20-10-05).
O 14 Inspect tip rib visually for general condition.
O 15 Check metall fittings (power supply support) for secure bonding to
the carbon laminate
Aileron
O 1 Check root and tip rib bonding to the skin laminate by coin tapping.
O 2 Check bonding skin/spar for delaminations by coin tapping.
O 3 Checkbonding top/bottom for cracks and delaminations by coin
tapping (Refer to Chapter 20-10-05).
O 4 Check hinge points (mounting brackets) and actuator for damages and
cracks. Ensure proper attachment.
O 5 Inspect spades visually for general condition. Check spade support
for corrosion, cracks and deformations. Ensure proper attachment to
aileron.
O 6 Inspect ventilation holes for obstruction.
Surface general
O 1 Check painting visually for general condition (blisters etc.).
O 2 Check laminate for erosion, scratches and nicks.
Control system
O 1 Inspect bell cranks for damage, corrosion, security of mounting and
link bolts through wing access holes.
O 2 Inspect control rods for corrosion.
O 3 Check Rod end bearing for free movement and cleanliness.
Inspector:
Mechanic:
Inspections
Date:
Serial No.:
1000 hours
SCHEDULED MAINTENANCE CHECKS
Significant Items Inspection