AD 96-22-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 1000A | Airworthiness Directives; Beech (Raytheon) Model BAe 125 Series 1000A and Model Hawker 1000 Airplanes |
| aircraft | Textron Aviation Inc. | Hawker 1000 | Airworthiness Directives; Beech (Raytheon) Model BAe 125 Series 1000A and Model Hawker 1000 Airplanes |
Unsafe Condition
Failure of the driver link and inadvertent deployment of a thrust reverser during flight, which could result in reduced controllability of the airplane.
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Required Actions
Modify the thrust reversers by accomplishing Modifications 253691 Part A, Part B, and Part E in accordance with Hawker Service Bulletin SB.78-14-3691A,B&E. An alternative method of compliance may be used if approved by the FAA.
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Compliance Time
Within 6 months after the effective date of this AD (December 11, 1996).
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Affected Aircraft
Beech (Raytheon) Model BAe 125 Series 1000A and Model Hawker 1000 airplanes as identified in Hawker Service Bulletin SB.78-14-3691A,B&E.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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