AD 67-14-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes |
Unsafe Condition
Fatigue failure of the nose landing gear steering jack cylinder gland nut P/N AB44-229.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace aluminum alloy gland nuts P/N AB44-229 with unused aluminum alloy nuts of the same part number or steel nuts P/N AB44-1793, depending on time in service. For nuts with less than 4,900 hours by AD effective date, replace before 5,000 hours. For 4,900+ hours, replace within next 100 hours. Aluminum alloy replacements must be replaced before 5,000 hours.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before the accumulation of specified hours' time in service as per paragraphs (a) and (b).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.