AD 2008-12-04

Recurring final rule
Data completeness: 80%

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

AD Number
2008-12-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-29333
FR Citation
73 FR 32991

Applicability

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

Unsafe Condition

Fatigue-related cracks along the chemically milled steps of the fuselage skin, which could grow and lead to skin bay flaps opening and causing decompression.

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

Required Actions

Inspect for cracks along the chemically milled steps of the fuselage skin and for missing or loose fasteners in the area of preventative modifications or repairs. Replace time-limited repairs with permanent repairs if applicable. Take applicable corrective actions to end repetitive inspections if necessary.

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

Compliance Time

Within 50 flight hours after the effective date of the AD.

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Affected Aircraft

Boeing Model 737-600, -700, -700C, -800, and -900 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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View Official Source ↗ Find More ADs for Boeing 737-600

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