AD 99-21-06

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9-81, -82, -83, and -87 Series Airplanes (MD-81, -82, -83, and -87), and Model MD-88 Airplanes

AD Number
99-21-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-NM-267-AD
FR Citation
(Federal Register: October 07, 1999 (Volume 64, Number 194))

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-81 (MD-81) Airworthiness Directives; McDonnell Douglas Model DC-9-81, -82, -83, and -87 Series Airplanes (MD-81, -82, -83, and -87), and Model MD-88 Airplanes
aircraft The Boeing Company DC-9-82 (MD-82) Airworthiness Directives; McDonnell Douglas Model DC-9-81, -82, -83, and -87 Series Airplanes (MD-81, -82, -83, and -87), and Model MD-88 Airplanes
aircraft The Boeing Company DC-9-83 (MD-83) Airworthiness Directives; McDonnell Douglas Model DC-9-81, -82, -83, and -87 Series Airplanes (MD-81, -82, -83, and -87), and Model MD-88 Airplanes
aircraft The Boeing Company DC-9-87 (MD-87) Airworthiness Directives; McDonnell Douglas Model DC-9-81, -82, -83, and -87 Series Airplanes (MD-81, -82, -83, and -87), and Model MD-88 Airplanes
aircraft The Boeing Company MD-88 Airworthiness Directives; McDonnell Douglas Model DC-9-81, -82, -83, and -87 Series Airplanes (MD-81, -82, -83, and -87), and Model MD-88 Airplanes

Unsafe Condition

Cracking of the actuator cylinder support brackets of the slat drive mechanism assembly outside the original inspection area could cause inadvertent slat retraction in flight.

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

Required Actions

Perform visual and/or eddy current inspections of the actuator cylinder support brackets per specified intervals and service bulletins. Replace any cracked brackets with new parts prior to further flight. Repeat inspections at intervals not exceeding 3,000 landings until terminating action is taken.

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

Compliance Time

Varies based on inspection type and prior compliance: within 30 days of AD effective date or 10,000 landings, with subsequent intervals up to 3,000 landings.

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

Affected Aircraft

McDonnell Douglas Model DC-9-81, -82, -83, -87 (MD-81, -82, -83, -87), and MD-88 airplanes, all serial numbers.

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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