AD 2003-18-10

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 767-200, -300, -300F, and -400ER Series Airplanes

AD Number
2003-18-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-240-AD
FR Citation
68 FR 53503

Applicability

TypeManufacturerModelDetails
aircraft Boeing 767-200 Airworthiness Directives; Boeing Model 767-200, -300, -300F, and -400ER Series Airplanes

Unsafe Condition

Fatigue cracking of principal structural elements (PSE) could adversely affect the structural integrity of the airplanes.

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

Required Actions

Revise the Airworthiness Limitations Section of the Maintenance Planning Data (MPD) Document to incorporate certain inspections and compliance times to detect fatigue cracking of PSEs.

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

Compliance Time

Within 18 months after the effective date of the AD.

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

Affected Aircraft

Boeing Model 767-200, -300, -300F, and -400ER 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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View Official Source ↗ Find More ADs for Boeing 767-200

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