AD 90-16-05

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

AD Number
90-16-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-196-AD
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

Structural failure due to cracks in the airframe.

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

Required Actions

Inspect for cracks within one repetitive inspection interval or at the inspection threshold specified in MDC K1579, repeat inspections at intervals per service bulletins. If cracks are found, repair or modify per approved data before further flight. Accomplish structural modifications within 4 years or by specified dates per MDC K1579.

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

Compliance Time

Within one repetitive inspection interval specified in the service bulletins listed in Table 2.1 of MDC K1579 after the effective date of this AD, or at the inspection threshold specified in MDC K1579, whichever is later. Modifications must be done within 4 years after the effective date or by incorporation thresholds listed in the document.

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

Affected Aircraft

McDonnell Douglas DC-8 series airplanes as listed in McDonnell Douglas Report No. MDC K1579, Revision A, dated March 1, 1990.

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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