AD 90-19-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (C-29A) | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (U-125) | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes |
Unsafe Condition
Fatigue cracks in the windscreen center pillar and subsequent rapid decompression of the airplane.
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Required Actions
Install reinforcing straps on the bottom aft portion of the upper and lower web sections of the windscreen center pillar assembly in accordance with British Aerospace Service Bulletin 53-65-3168A, Revision 1, dated March 9, 1989. An alternate means of compliance or adjustment of the compliance time may be used when approved by the FAA.
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Compliance Time
Prior to the accumulation of 6,000 landings since new or within 30 days after the effective date of this AD, whichever occurs later, unless previously accomplished.
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Affected Aircraft
Model BAe 125-800A series airplanes, Serial Numbers 258001 through 258090, inclusive, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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