AD 91-15-06

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes

AD Number
91-15-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-279-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-8-61F Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes
aircraft The Boeing Company DC-8-62F Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes
aircraft The Boeing Company DC-8-63F Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes
aircraft The Boeing Company DC-8-71F Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes
aircraft The Boeing Company DC-8-72F Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes
aircraft The Boeing Company DC-8-73F Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes
aircraft The Boeing Company DC-8F-54 Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes
aircraft The Boeing Company DC-8F-55 Airworthiness Directives; MCDONNELL DOUGLAS DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F Series Airplanes

Unsafe Condition

Inadvertent opening of the forward upper cargo door in flight could result in loss of pressurization and reduced controllability of the aircraft.

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

Required Actions

Within four months after the effective date, perform magnetic particle inspections on cargo door latch spool fitting attach bolts or replace non-Inconel bolts with new bolts. Replace non-passing bolts before further flight. Replace all non-Inconel bolts with Inconel bolts within two years.

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

Compliance Time

Within four months after the effective date of this AD, and thereafter at intervals not to exceed one year

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

Affected Aircraft

All Model DC-8F, DC-8-61F, -62F, -63F, -71F, -72F, and -73F 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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