AD 2012-12-05

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2012-12-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-1255
FR Citation
77 FR 36139

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Fatigue cracking of the intercostals on the forward and aft sides of the forward entry door cutout, which could result in loss of the forward entry door and rapid decompression of the airplane.

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

Required Actions

Inspect for cracking under the stop fittings and intercostal flanges at stringers S-14L, S-15L, and S-16L. Extend the repetitive interval for certain airplanes. Add a one-time inspection to detect missing fasteners. Add repetitive inspections for cracking of the cargo barrier net fitting and stringer S-15L aft intercostal, with repair if necessary. Update or add certain inspection and repair instructions.

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

Compliance Time

Within the applicable repetitive interval or before further flight, depending on the specific inspection requirement.

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

Affected Aircraft

The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, as specified in the AD.

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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