AD 2013-16-17

final rule
Data completeness: 80%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2013-16-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2012-0931
FR Citation
78 FR 52419

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Fatigue cracking of the wing trailing edge structure, which could result in compromised structural integrity of the airplane.

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

Required Actions

Revise the maintenance inspection program to include inspections that will give no less than the required damage tolerance rating (DTR) for certain structural significant items (SSIs), and 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

The Boeing Company Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F 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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