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AD/PA-38/27 Amdt 2 - Wing Fatigue
New retirement life = 21,950 hrs - ( 0.3New retirement life = 21,950 hrs - ( 0.3 x hrs accumulated prior to modification )
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New retirement life = 21,950 hrs - ( 0.3 x hrs accumulated prior to modification )
Note 1: Example 1, an aircraft with 9,000 hours already accumulated without the modification:
New retirement life = 21,950 - (0.3 x 9,000) = 19,250 hours.
Example 2, an aircraft with 11,000 hours already accumulated without the modification:
New retirement life = 21,950 - (0.3 x 11,000) = 18,650 hours.
Note 2: For assistance with incorporating this STC, write to the STC owner, Mr Paul
M. Sterling, 13113 SE 228th Place, Kent, WA, USA, 98031.
- Initially, at 100 flight hours after installation of the wing spar strap, then every 100 flight hours thereafter.