AD 96-05-01

final rule
Data completeness: 70%

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

AD Number
96-05-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-118-AD
FR Citation
(Federal Register: March 04, 1996 (Volume 61, Number 43))

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-81 (MD-81) Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes
aircraft The Boeing Company DC-9-82 (MD-82) Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes
aircraft The Boeing Company DC-9-83 (MD-83) Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes
aircraft The Boeing Company DC-9-87 (MD-87) Airworthiness Directives; McDonnell Douglas Model DC-9-80 Series Airplanes

Unsafe Condition

Failure of the horizontal stabilizer primary trim motor due to incorrectly manufactured motor shafts could result in reduced controllability of the airplane.

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

Required Actions

Inspect or conduct a records search to determine if the horizontal stabilizer primary trim motor is a suspect unit. Replace or modify the motor if it has a suspect serial number, unless it has been previously modified in accordance with Sundstrand Service Bulletin 9590-27-012.

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

Compliance Time

Effective April 3, 1996.

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Affected Aircraft

McDonnell Douglas Model DC-9-80 series airplanes as listed in MD-80 Alert Service Bulletins A27-342 and A27-342 Revision 1.

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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