AD 90-25-04

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 Series Airplanes

AD Number
90-25-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-71-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 Series 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 Series 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 Series 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 Series 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 Series Airplanes

Unsafe Condition

The engine forward mount cone bolts may have incorrect part numbers or indications of shear section cut-out, which could cause the engine to depart the aircraft during a hard landing, sudden engine seizure, or when encountering high velocity vertical gusts during flight.

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

Required Actions

Within 30 days after the effective date, perform a one-time visual or ultrasonic inspection of both engine forward mount cone bolts to verify correct part numbers (Barry K2219-9SA3 or McDonnell Douglas 7938004-503). Replace incorrect or defective bolts before further flight. Incorporate a maintenance program revision requiring visual or ultrasonic inspections at each engine change, replacing incorrect bolts before engine installation.

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

Compliance Time

Within 30 days after the effective date of this AD, unless accomplished since December 21, 1989.

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

Affected Aircraft

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