AD 2002-10-03

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 Airplanes

AD Number
2002-10-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-197-AD
FR Citation
67 FR 34823

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas Various Airworthiness Directives; McDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 Airplanes

Unsafe Condition

Fatigue cracking of the main landing gear (MLG) shock strut pistons, which could result in failure during landing or jacking of the airplane.

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

Required Actions

Replace certain main landing gear (MLG) shock strut piston assemblies with new or serviceable, improved assemblies.

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-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 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

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