AD Amdt-39-10058
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Pilatus | Britten-Norman Ltd | Airworthiness Directives; Pilatus Britten-Norman Ltd. BN-2A and BN-2A Mk 111 Series Airplanes |
Unsafe Condition
Failure of the pilot's rudder bar assembly due to cracks and loose fasteners in the left-hand rudder bar assembly and insufficient wall thickness of the slider tube unit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the left-hand rudder bar assembly and determine the wall thickness of the slider tube unit. Replace the left-hand slider tube with a new strengthened slider tube unit to terminate repetitive inspections required by AD 75-24-07 R1.
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
Pilatus Britten-Norman Ltd. BN-2A and BN-2A Mk 111 series airplanes subject to AD 75-24-07 R1
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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