AD 87-15-08 R1

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-9-80 (MD-80) Series Airplanes

AD Number
87-15-08 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Fractures in P/N 7958533-517 (Hartwell P/N H2816-3) cowl door latch assemblies, particularly at the attachment hook, could result in cowl door separation during flight.

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

Required Actions

Within 7 days after the effective date, visually inspect cowl door latch assemblies for fractures in accordance with ASB A71-42. If fractures are found, replace all latch assemblies on the affected door before further flight. Repeat inspections every 7 days until replaced with P/N 7958533-519 latch assemblies. For fuselage 1237-1276, install new P/N 7958533-519 latches within 45 days. For fuselage 1277-1368, install within 70 days.

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

Compliance Time

Within the specified timeframes: 7 days for initial inspection, 45 days for fuselages 1237-1276, and 70 days for fuselages 1277-1368, all after April 25, 1988.

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

Affected Aircraft

McDonnell Douglas DC-9-80 series (MD-80) airplanes, Fuselage Numbers 1237 through 1368, including models DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87).

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.