AD 2004-01-02

final rule
Data completeness: 70%

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

AD Number
2004-01-02
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2002-NM-152-AD
FR Citation
69 FR 1511

Applicability

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

Unsafe Condition

Loss of the fuse pin of the pitch load fitting due to fatigue caused by improper clearance between the fuse pin and bushing, which could result in increased loads in the wing-to-strut joints and consequent separation of the strut and engine from the wing.

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

Required Actions

Modify the aft pitch load fitting of the diagonal brace of the nacelle strut of each wing.

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

Boeing Model 767-200, -300, and -300F 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.