AD 2011-06-12

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Model MD-90-30 Airplanes

AD Number
2011-06-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-1202
FR Citation
76 FR 15800

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Model MD-90-30 Airworthiness Directives; The Boeing Company Model MD-90-30 Airplanes

Unsafe Condition

Cracking of the left and right upper center skin panels of the horizontal stabilizer, specifically at the aft inboard corner, which might ultimately lead to the loss of overall structural integrity of the horizontal stabilizer.

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

Required Actions

Perform eddy current inspections to detect cracking of the left and right upper center skin panels of the horizontal stabilizer. If no crack is found, repeat inspections at specified intervals. If a crack is found, replace the skin panel with a serviceable one before further flight.

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

Compliance Time

Within 3,778 flight cycles after the effective date of this AD or before the accumulation of 20,000 total flight cycles, whichever occurs later.

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

Affected Aircraft

The Boeing Company Model MD-90-30 airplanes, certificated in any category.

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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