AD 97-18-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A | Airworthiness Directives; Raytheon Model BAe 125-800A Series Airplanes, and Model Hawker 800 and Hawker 800XP Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (C-29A) | Airworthiness Directives; Raytheon Model BAe 125-800A Series Airplanes, and Model Hawker 800 and Hawker 800XP Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (U-125) | Airworthiness Directives; Raytheon Model BAe 125-800A Series Airplanes, and Model Hawker 800 and Hawker 800XP Series Airplanes |
| aircraft | Textron Aviation Inc. | Hawker 800 | Airworthiness Directives; Raytheon Model BAe 125-800A Series Airplanes, and Model Hawker 800 and Hawker 800XP Series Airplanes |
| aircraft | Textron Aviation Inc. | Hawker 800 (U-125A) | Airworthiness Directives; Raytheon Model BAe 125-800A Series Airplanes, and Model Hawker 800 and Hawker 800XP Series Airplanes |
| aircraft | Textron Aviation Inc. | Hawker 800XP | Airworthiness Directives; Raytheon Model BAe 125-800A Series Airplanes, and Model Hawker 800 and Hawker 800XP Series Airplanes |
Unsafe Condition
Overbias or overbalance of the rudder during single engine handling could result in reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the rudder in accordance with Raytheon Service Bulletin SB.55-36-25F017A&B. An alternative method of compliance may be used if approved by the FAA.
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Compliance Time
Within 100 hours time-in-service or within 6 months after the effective date of this AD, whichever occurs first.
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Affected Aircraft
Raytheon Model BAe 125-800A series airplanes, and Model Hawker 800 and Hawker 800XP series airplanes where Raytheon Modification 25F017A&B has not been installed.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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