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Model; 172N Skyhawk; Horizontal Stab Structure; ATA 5511
Model; 172N Skyhawk; Horizontal Stab Structure; ATA 5511
During an inspection of the horizontal stabilizer spar, the technician found a crack around the center-lightening hole. Spar (P/N 0532001-98) and reinforcement (P/N 0532001-97) were both cracked.
The submitter stated that both cracks are inboard of the stabilizer attachment holes.
Part total time-8,135 hours.
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