AD 87-03-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800B | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes |
Unsafe Condition
The fuselage canopy upper rail may fail, leading to possible rapid loss of cabin pressurization.
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Required Actions
Modify the fuselage canopy upper rail in accordance with Section 2 of British Aerospace Service Bulletin 53-59-(3031B), dated June 5, 1986. An alternate means of compliance or adjustment of compliance time may be used if approved by the FAA Manager, Standardization Branch, ANM-113.
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Compliance Time
Prior to the accumulation of a total of 3,000 flight cycles or within the next 90 days after the effective date of this AD, whichever occurs later.
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Affected Aircraft
British Aerospace Model BAe 125-800A and -800B series airplanes listed in Service Bulletin 53-59 (3031B), dated June 5, 1986.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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