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57-30 16) Visually inspect the visible portions of the R.H. wing tip for loose rivets, cracks and distortion. 600  
57-60 17) Visually inspect the R.H. aileron attachment and hinge. 600 NOTE 1 
57-60 18) Check the R.H. aileron balancing weight attach fittings for condition. 600 NOTE 1 
57-60 19) Visually inspect the visible portions of the R.H. aileron ; in case of doubt, remove the aileron and inspect for loose rivets, cracks, distortion and evidence of corrosion - refer to 57-60-00 201. 600  
57-60 20) Check the R.H. aileron for freedom of rotation - refer to 27-10-00 201. 600 NOTE 1 
57-50 21) Visually inspect the R.H. flap attachment and hinge. 600 NOTE 1 
57-50 22) Visually inspect the visible portions of the R.H. flap ; in case of doubt, remove the flap and inspect for loose rivets, cracks, distortion and evidence of corrosion - refer to 57-50-00 201. 600  
20-00 23) Reinforce the anticorrosion protection - refer to 600  
 20-00-04 201 and lubricate - refer to 12-21-04 201.   

NOTE 1 : If a 100-hr. inspection has been carried out during the last 3 months, do not perform this operation unless this annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
ADAA
Validity : S / N 1 - 9999 05-20 06Page 219
(EA) JUN 01
 

ATA ANNUAL INSPECTION (Al)
ENGINE COMPARTMENT INSPECTION (AREA 100) AREA OTHER
INSPECTION PERFORMED
BY
71-00 ENGINE COMPARTMENT INSPECTION (AREA 100) 100  
71-00 1) Perform an overall visual inspection of area 100. 100  
11-00 2) Check installation and legibility of exterior placards and markings - refer to 11-20-00 1. 100 NOTE 1 
32-40 3) Visually inspect the brake hydraulic reservoir. Check fluid level - refer to 12-13-01 301. 100  
32-40 4) Change the brake hydraulic fluid - refer to 12-13-01 301, 12-13-02 301. 100 3 years 
71-20 5) Visually inspect the engine mount for distortion, cracks, evidence of corrosion and interference. Check the
protection - refer to 20-00-04 201 and 71-20-00 201. 100 NOTE 1 
71-20 6) Visually check that the engine mount is correctly attached to the firewall. Check the red painted marks on the bolts for alignment. 100 NOTE 1 
71-20 7) Check the engine attaching bolts for proper torque and check the vibration isolators for wear. In case of wear, replace all the vibration isolators - refer to 71-20-00 201. 100 NOTE 1 
21-40 8) Perform a detail examination of air regulation hose(s) and firewall-mounted box(es) for cracks. 100  
　
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