AD 95-15-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | BAe 146-100A | Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-200A | Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A Airplanes |
| aircraft | BAE Systems (Operations) Limited | BAe 146-300A | Airworthiness Directives; British Aerospace Model BAe 146-100A, -200A, and -300A Airplanes |
Unsafe Condition
Low frequency constant amplitude oscillations of the elevator control system and non-centering of the pitch control upon autopilot disconnect, which can cause uncommanded descent and reduced controllability.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the elevator control system in accordance with British Aerospace Service Bulletin SB.27-77-00955A&C, Revision 2, dated March 10, 1989. Operators may request alternative methods of compliance or adjusted timelines via the FAA's Standardization Branch.
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Compliance Time
Within 60 days after the effective date of this AD (August 23, 1995).
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Affected Aircraft
British Aerospace Model BAe 146-100A, -200A, and -300A airplanes listed in SB.27-77-00955A&C, Revision 2.
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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