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penetrant inspection in case of engine
removal.
71-20 2) 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 X 0 NOTE 1
71-20 3) Visually check that the engine mount is correctly attached to the firewall. Check the red painted marks on the bolts for
alignment. 100 X X 0 NOTE 1
71-20 4) 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 X X 0 NOTE 1
71-60 Air intake
71-60 1) Visually inspect the inlet pipes, the
manifolds and their attach fittings. 100 X X X 0 NOTE 1
71-60 2) Visually inspect the hoses (corrugated
hoses). 100 X X X 0 NOTE 1
71-60 3) Visually inspect the air filter(s) - refer to the spare filter package instructions. 100 X X X X
71-60 4) Replace the air filter(s). 100 1 year
71-60 5) Visually inspect the deflectors, the inlet box and the air intake flap ; clean if necessary. 100 X X X 0 NOTE 1
Inspect for cracks and distortion, and check the attach fittings for condition.
NOTE 1 : If a 100-hr. inspection has been carried out during the ast 3 months, do not perform the operations identified with a "0" unless the annual inspection replaces a 100-hr. inspection. For US registered aircraft, perform all operations.
AHAA
Validity : S / N 1 - 9999 05-20 01Page 239
(IN JUN 01
ATA OPERATIONS Area INSPECTIONS
1st
25 hrs 50
hrs 100
hrs Major Ann. Other
71-60 6) Perform an operational test of the air intake flap. 100 X X 0 NOTE 1
72-00 ENGINE
72-00 General
72-00 1) Perform an overhaul of the engine. 100 Refer to
05-10-00
72-30 Cylinders section
72-30 1) Measure and record the cylinder
compression values in the engine log book -refer to the latest issue of LYCOMING 100 X X 0 NOTE 1
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