AD 2007-18-52
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-600 | Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes |
Unsafe Condition
Loose or missing parts from the main slat track downstop assemblies could result in a fuel leak and consequent fire.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the main slat track downstop assemblies to verify proper hardware installation, torque the nut and bolt, and take corrective actions if necessary, including installing a new or serviceable part and inspecting the slat can for foreign object debris (FOD) and damage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 10 days after receipt of emergency AD 2007-18-52 for the initial detailed or borescope inspection. Torquing the nut and bolt is due within 24 days after receipt of emergency AD 2007-18-51.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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