AD Amdt-39-212
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-8-60 | Airworthiness Directives; McDonnell Douglas Model DC-8-60 Series Airplanes Equipped With Engines Modified by Burbank Aeronautical Corporation II (BAC II) in Accordance With Supplemental Type Certificate (STC) SA4892NM or SA5455NM |
Unsafe Condition
Failure of the cone bolt on the right side of the forward mount of the engine may lead to separation of the engine 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 the bolt if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model DC-8-60 series airplanes equipped with engines modified by Burbank Aeronautical Corporation II (BAC II) under STC SA4892NM or SA5455NM.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.