AD Amdt-39-10708

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes and Model MD-88 Airplanes

AD Number
Amdt-39-10708
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-NM-20-AD
FR Citation
63 FR 43614

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-9-80 Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes and Model MD-88 Airplanes

Unsafe Condition

Fatigue cracking of certain fuselage skin panels could result in reduced structural integrity of the airplane and consequent loss of pressurization.

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

Required Actions

Conduct repetitive inspections to detect fatigue cracking of certain fuselage skin panels and perform repairs if necessary. An optional preventative modification is available to terminate repetitive inspections for certain airplanes.

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-9-80 series and Model MD-88 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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