AD 95-14-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; British Aerospace Model BAC 1-11 200 and 400 Airplanes |
Unsafe Condition
Reduced structural integrity of the airplane due to fatigue cracking and corrosion in transport category airplanes that are approaching or have exceeded their economic design goal.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install structural modifications listed in Table 1 of British Aerospace Alert Service Bulletin 5-A-PM5995, Issue 3, except Items 6, 11, 13, and 14, in accordance with specified service bulletins. The modifications must be completed prior to reaching the 'Not Exceed Time' interval in the service bulletin or within 15 months after the AD's effective date, whichever is later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to reaching the 'Not Exceed Time' interval specified in Table 1 of British Aerospace Alert Service Bulletin 5-A-PM5995, Issue 3; or within 15 months after the effective date of this AD; whichever occurs later
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
British Aerospace Model BAC 1-11 200 and 400 airplanes, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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