AD 2000-22-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-9-10 | Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes and C-9 (Military) Airplanes |
Unsafe Condition
Fatigue cracking in the upper cap of the front spar of the left and right engine pylons, which could lead to failure of the upper cap and reduced structural integrity of the airplane.
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Required Actions
Perform new, improved x-ray and eddy current inspections to detect cracks in the upper cap of the front spar of the left and right engine pylons. Conduct repetitive inspections or corrective actions if necessary. Modify the subject area as terminating action for the repetitive inspection requirements.
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Compliance Time
Within 3,600 flight hours after the effective date of this AD, or before the accumulation of 8,000 total flight hours, whichever occurs later.
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Affected Aircraft
McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 series airplanes and C-9 (military) airplanes, as listed in McDonnell Douglas Service Bulletin DC9-54-030, Revision 06, dated November 11, 1999, except for those airplanes on which specific special change notifications or service rework drawings have been accomplished.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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