AD 2004-16-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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
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