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57-60 30) Check the R.H. aileron balancing weight attach fittings for condition. 600
57-60 31) Visually inspect the R.H. aileron hinge fittings, check the ball joints, the attach fittings and the stops. 600
57-60 32) 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 33) Check the R.H. aileron for freedom of rotation - refer to 27-10-00 201. 600
57-50 34) 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
57-50 35) Visually inspect the R.H. flap hinge fittings, check the ball joints and the attach fittings. 600
20-00 36) Reinforce the anticorrosion protection - refer to 600
20-00-04 201 and lubricate - refer to 12-21-04 201.
52-40 37) Install sealed inspection doors 613, 614 - refer
to 52-40-00 201. 600
57-30 38) Install wing tip 617 (if not riveted) - refer to 57-30-00 201. 600
12-10 39) Fill the fuel tanks and inspect for leaks - refer to 000
12-11-01 301, 28-10-00 601.
NOTE : Before and during refueling, perform
operational tests of fuel gages - refer to
28-40-01 401 and low fuel level detectors (if installed) - refer to 28-40-04 201.
AIAA
Validity : S / N 1 - 9999 05-20-05 (JA) Page 224
JUN 01
ATA "80A" MAJOR INSPECTION
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
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) Thoroughly inspect the whole engine mount ; in case of doubt, perform a fluorescent penetrant inspection - refer to 20-00-14 301 and 71-20-00 201. 100
Systematically perform a fluorescent penetrant
inspection in case of engine removal.
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