AD 2007-18-52

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, -900, and -900ER Series Airplanes

AD Number
2007-18-52
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-29089
FR Citation
72 FR 53928

Applicability

TypeManufacturerModelDetails
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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