AD 95-09-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-8-61 | Airworthiness Directives; McDonnell Douglas Model DC-8-60 Series Airplanes |
| aircraft | The Boeing Company | DC-8-62 | Airworthiness Directives; McDonnell Douglas Model DC-8-60 Series Airplanes |
| aircraft | The Boeing Company | DC-8-62F | Airworthiness Directives; McDonnell Douglas Model DC-8-60 Series Airplanes |
| aircraft | The Boeing Company | DC-8-63 | Airworthiness Directives; McDonnell Douglas Model DC-8-60 Series Airplanes |
| aircraft | The Boeing Company | DC-8-63F | Airworthiness Directives; McDonnell Douglas Model DC-8-60 Series Airplanes |
Unsafe Condition
Failure of the cone bolt on the right side of the forward mount of the engine due to corrosion pitting at the base of the bolt thread, which may lead to engine separation during a critical phase of flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the cone bolt on the right side of the forward mount of each engine to determine its part number. Replace bolts with BAC II part number DC-8-21005-7 with Barry Controls part number 96013-1 prior to further flight. Submit a report to the FAA within 10 days of replacement.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 days after the effective date of this AD for inspections; prior to further flight for replacements.
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Affected Aircraft
McDonnell Douglas Model DC-8-61, -62, -62F, -63, and -63F airplanes equipped with engines modified by BAC II under STC SA4892NM or SA5455NM.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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