We completed 7 Spar Modifications on time and on budget this year alone with bookings going into next year.
Effective June 22, 2005 there where 2 New AD’S on the Aircraft listed below.
AD 2005-12-12 Applies to 401, 401A, 401B, 402, 402A, 402B, 411, 411A.This AD supersedes AD 79-10-15 which required repetitive inspections for fatigue cracks in the lower wing spars & forward lower wing attachment fittings. It complies with Cessna Supplemental Inspection Document (SID) 57-10-08 which makes the Modification due when the aircraft reaches 20 years.
AD 2005-12-13 Applies to 402C & 414A. This AD supersedes AD 2005-05-52 which required repetitive inspections for fatigue cracks in the lower wing spars & forward lower wing attachment fittings. It complies with Cessna Supplemental Inspection Document 57-10-16 which makes the Modification due when the aircraft reaches 20 years.
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