AD 2005-09-04

Recurring final rule
Data completeness: 80%

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), and MD-88 Airplanes

AD Number
2005-09-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-293-AD
FR Citation
70 FR 21924

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), and MD-88 Airplanes

Unsafe Condition

Fatigue cracking of the main landing gear (MLG) shock strut pistons, which could result in failure of the pistons and consequent damage to the airplane structure or injury to airplane occupants.

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

Required Actions

Inspect MLG shock strut pistons for cracking. Replace cracked pistons with new or serviceable parts. Replace all MLG shock strut pistons with new improved parts to terminate 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-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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