AD Amdt-39-10642
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-100 | Airworthiness Directives; Boeing Model 737-100, -200, -200C Series Airplanes |
Unsafe Condition
Fatigue cracking on the lower flange of the forward engine mount support (FEMS) fitting, broken bolts, bolts with loose or detached nuts on the upper inboard attachment, and cracked or severed lugs at the outboard support link attachment of the FEMS fitting.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections to detect fatigue cracking and discrepancies of the FEMS fitting and its attachments. Repair as necessary if cracks or discrepancies are found.
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
Boeing Model 737-100, -200, and -200C 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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