AD 78-01-15

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

AD Number
78-01-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-8-11 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-12 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-21 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-33 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-41 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-42 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-43 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-51 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

Unsafe Condition

Failure of the elevator geared tab crank arms and jamming of the elevator surface.

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

Required Actions

Within 12 months after the effective date, modify the elevator leading edge cutouts and covers, modify and reidentify the elevator geared tab links, modify rod ends as required, and chamfer the horizontal stabilizer box fittings. Within 18 months after the effective date, install an elevator position indicator system. Within 30 days after the effective date, install a placard or update the Operations Manual and check list as specified.

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

Compliance Time

Within the next 12 months after the effective date of this AD, unless already accomplished

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

Affected Aircraft

MCDONNELL DOUGLAS Model DC-8 Series airplanes certificated in all categories.

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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