Eagle ICA-D212-725, Инструкция по эксплуатации

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ICA-D212-725 (05)
Page 10 of 25
CHAPTER 05 – INSPECTION AND COMPONENT OVERHAUL SCHEDULE (05-00-00)
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COPYRIGHT
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2007 BY DART AEROSPACE LTD.
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THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO
ANY OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision: 4
Date: 11.06.01
5.4 25 HOURS/30 DAYS – PART B
Data Reference
Inspection Task Description
Initial
Mech Other
5.3.6.3 Nicks, scratches, and corrosion damage up to
0.020” (0.50mm) deep is acceptable but must be polished
out to a maximum depth of 0.020” (0.50mm) using
scotchbrite.
5.3.6.4 Inspect the bearings and bolts for looseness.
Loose bearings should be replaced per Chapter 71. If bolts
are loose, holes should be checked for elongation.
Maximum hole elongation is 0.025” (0.63mm).
5.3.6.5 Check turnbuckle nut torque. Proper range is
400-600 in-lbs (45.2-67.8 Nm). Ensure stud threads are
visible through witness holes.
5.3.6.6 If lockwire is found broken, loose or missing or if
turnbuckle jam nut torque is found to be loose, check engine
alignment per the Chapter 71.