AD 2004-25-14
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; DC-9-20, DC-9-30, DC-9-40, DC-9-50 Series Airplanes; DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) Airplanes; and Model MD-88 Airplanes |
Unsafe Condition
Corrosion to the retract cylinder support fitting of the main landing gear (MLG) and the cylinder bore in the support fitting, which could result in compromised integrity of the retract cylinder support fitting of the MLG and possible damage to the hydraulic system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the retract cylinder support fitting and the cylinder bore of the support fitting of both main landing gear (MLG) for corrosion, and take corrective action if necessary. Replace cadmium-plated retract cylinder support bushings and bearings of both MLG.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 15,000 flight hours after the effective date of the AD, or prior to the accumulation of 30,000 total flight hours, whichever is later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
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, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and Model MD-88 airplanes; as listed in Boeing Service Bulletin DC9-57-222, dated September 18, 2002; certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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