AD 2014-23-10

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2014-23-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0195
FR Citation
79 FR 71296

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Cracks found at the cutout in the web of body station frame 303.9 inboard of stringer 16L, which could prevent the left forward entry door from sealing correctly and could cause in-flight decompression of the airplane.

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

Required Actions

Conduct repetitive inspections to detect fuselage frame cracking and take applicable corrective action. Optional terminating action (repair/preventive change) is provided for airplanes subject to AD 2008-17-03.

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

Compliance Time

Before further flight

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, including newly added 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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