AD 99-21-32

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model MD-90-30 Series Airplanes

AD Number
99-21-32
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-NM-340-AD
FR Citation
(Federal Register: October 20, 1999 (Volume 64, Number 202))

Applicability

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

Unsafe Condition

Interference between the elevator cable pulley and the shroud frame of the ventral stairway could result in pitch oscillation of the airplane, consequent damage to the elevator cable pulley, and reduced controllability.

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Required Actions

Perform a one-time general visual inspection to measure clearance and detect interference between the elevator cable pulley and the shroud frame of the ventral stairway within 12 months after the effective date. Modify the shroud frame of the ventral stairway in accordance with the referenced service bulletin.

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Compliance Time

Within 12 months after the effective date

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Affected Aircraft

McDonnell Douglas Model MD-90-30 series airplanes listed in Service Bulletin MD90-27-026, 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 8, 2026

Rights: U.S. Government Public Domain

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