AD 2008-09-17

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, and MD-10-10F Airplanes

AD Number
2008-09-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2008-0015
FR Citation
73 FR 24155

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-10-10 Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, and MD-10-10F Airplanes

Unsafe Condition

Stray nickel or chrome plating deposits, corrosion, and cracking of the air filler valve bore on the main landing gear (MLG) cylinder could result in landing gear failure, significant damage to the airplane, and injury to personnel.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect for the presence of stray nickel or chrome plating deposits on the air filler valve bore of certain main landing gear (MLG) shock strut cylinders. If necessary, perform investigative and corrective actions. Corrective action terminates the repetitive inspections.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, and MD-10-10F airplanes.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗ Find More ADs for McDonnell Douglas DC-10-10

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