AD 2009-24-21
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-9-14 | Airworthiness Directives; McDonnell Douglas Model DC-9-14, DC-9-15, and DC-9-15F Airplanes; and McDonnell Douglas Model DC-9-20, DC-9-30, DC-9-40, and DC-9-50 Series Airplanes |
Unsafe Condition
Fatigue cracks in the shock strut cylinder of the main landing gear (MLG), which could result in a collapsed MLG during takeoff or landing, and possible reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the MLG shock strut cylinders for cracks using specified non-destructive testing methods. Review maintenance records to determine MLG service history and number of landings. Perform initial inspection before the accumulation of 60,000 total landings or at the applicable grace period, whichever is later.
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Compliance Time
Before the accumulation of 60,000 total landings on the MLG, or at the applicable grace period specified in Table 1, whichever occurs later.
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Affected Aircraft
All McDonnell Douglas Model DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC-9-34F, DC-9-32F (C-9A, C-9B), DC-9-41, and DC-9-51 airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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