AD Amdt-39-10015

Recurring final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Series Airplanes

AD Number
Amdt-39-10015
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 96-NM-188-AD
FR Citation
62 FR 24567

Applicability

TypeManufacturerModelDetails
aircraft British Aerospace Model BAC 1-11 200 and 400 Series Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Series Airplanes

Unsafe Condition

Fatigue cracking of the lugs of the engine mounting beams could result in reduced structural capability of the engine mount.

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

Required Actions

Perform repetitive ultrasonic inspections to detect cracking of the engine mounting beam lugs and replace the beam with a serviceable part 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

British Aerospace Model BAC 1-11 200 and 400 series airplanes

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

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