AD 2004-16-12

Recurring final rule
Data completeness: 70%

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

AD Number
2004-16-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2002-NM-186-AD
FR Citation
69 FR 51002

Applicability

TypeManufacturerModelDetails
aircraft Boeing 767-200 Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
engine Pratt & Whitney engines Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
engine General Electric engines Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes

Unsafe Condition

Fatigue cracking in primary strut structure, which could result in separation of the strut and engine from the airplane.

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

Required Actions

For airplanes subject to the first and second existing ADs, rework the aft pitch load fitting and install a new diagonal brace fuse pin. For airplanes subject to the third existing AD, replace the outboard pitch load fitting of the wing front spar with a new, improved fitting, which terminates certain currently required repetitive inspections.

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, powered by Pratt & Whitney or General Electric engines, and certain Boeing Model 767-200 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.