AD 2002-26-10

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas DC-9-10, -20, -30, -40, and -50 Series Airplanes

AD Number
2002-26-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-78-AD
FR Citation
68 FR 473

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-9-10 Airworthiness Directives; McDonnell Douglas DC-9-10, -20, -30, -40, and -50 Series Airplanes

Unsafe Condition

Cracking of the fuselage skin and doubler at all corners of the forward lower cargo doorjamb, which could result in rapid decompression of the fuselage and reduced structural integrity.

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

Required Actions

Inspect the corners of the forward lower cargo doorjamb using high-frequency eddy current inspections for certain conditions. Perform low-frequency eddy current or X-ray inspections to detect cracks. Modify the structure if necessary. Retain the existing requirements for a one-time visual inspection and various follow-on repetitive inspections.

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

Compliance Time

Not specified in the provided text.

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

Affected Aircraft

McDonnell Douglas DC-9-10, -20, -30, -40, and -50 series 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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View Official Source ↗ Find More ADs for McDonnell Douglas DC-9-10

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