AD 96-12-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A | Airworthiness Directives; Beech (Raytheon) Model BAe 125 Series 800A and Model Hawker 800 Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (C-29A) | Airworthiness Directives; Beech (Raytheon) Model BAe 125 Series 800A and Model Hawker 800 Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (U-125) | Airworthiness Directives; Beech (Raytheon) Model BAe 125 Series 800A and Model Hawker 800 Airplanes |
| aircraft | Textron Aviation Inc. | Hawker 800 | Airworthiness Directives; Beech (Raytheon) Model BAe 125 Series 800A and Model Hawker 800 Airplanes |
Unsafe Condition
Restricted control of the ailerons due to water accumulation that freezes in the area around an aileron pulley located in the lower area of the fuselage aft of the wing rear spar, which could reduce the pilot's ability to initiate roll control during critical phases of flight.
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Required Actions
Modify the airframe structure in the lower area of the fuselage aft of the wing rear spar in accordance with specified service bulletins. For certain airplanes, perform a functional test to determine if a bolt fouls the flap control system; repair if any foul is detected prior to further flight.
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Compliance Time
Within 6 months after the effective date of this AD, or within 30 days after the effective date for specific airplanes with prior modifications. Compliance is required unless accomplished previously.
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Affected Aircraft
Beech (Raytheon) Model BAe 125 Series 800A (including military variants C-29A and U-125) and Model Hawker 800 airplanes, excluding constructor's numbers 258079, 258213, and 258186 (which has a separate service bulletin requirement).
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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