AD 68-14-03 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Erratic functioning of the rudder and elevator feel simulator units and malfunctioning of these units without flight crew warning.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace hydraulic pipe runs in No. 1 and No. 2 systems with specified diameters; replace restrictor assemblies with Hobson P/N CHA 504-502; incorporate a warning indicator assembly in the rudder feel simulator system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 1,000 hours' time in service after the effective date of this AD (April 13, 1983) for the first two actions, and within the next 3,000 hours' time in service after the effective date for the third action.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 and 400 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
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