AD 91-11-02

final rule
Data completeness: 70%

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

AD Number
91-11-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-263-AD
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Damage to the engine, cone bolts, and pylon, or separation of an engine from the airplane, as a result of the loss of a through-bolt.

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

Required Actions

Inspect the through-bolt nut (P/N SPS83978-1216) for proper torque and conditions per MD-80 Alert Service Bulletin A71-51. Depending on discrepancies found (misaligned torque stripe, torque below 250 in-lb, missing components, etc.), actions include removing/replacing the nut, applying torque, reinstalling components, or repairing with FAA approval. Repeat inspections every 30 calendar days. Install castellated nuts and cotter pins within 18 months of AD effective date to terminate repetitive inspections.

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

Compliance Time

Within seven days after August 29, 1990 (the effective date of Amendment 39-6684, AD 90-12-51). Repeat inspections at intervals not exceeding 30 calendar days. Castellated nuts/cotter pins installation within 18 months after the effective date of this AD (June 24, 1991).

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

Affected Aircraft

McDonnell Douglas Model DC-9-81 (MD-81), -82 (MD-82), -83 (MD-83), -87 (MD-87) series airplanes and Model MD-88 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 8, 2026

Rights: U.S. Government Public Domain

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