AD 2008-11-03

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes

AD Number
2008-11-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-29069
FR Citation
73 FR 29407

Applicability

TypeManufacturerModelDetails
aircraft Boeing 737-100 Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes

Unsafe Condition

Fatigue cracking in structural significant items (SSIs) due to approaching or exceeding the design service objective.

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

Required Actions

Revise the FAA-approved maintenance inspection program to include inspections for damage tolerance ratings of SSIs. Perform repetitive inspections to detect cracks in all SSIs. Repair any cracked structure.

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

Compliance Time

Before further flight.

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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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