AD 96-11-17
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
Insufficient clearance between flap cables and turnbuckles, airbrakes cables and turnbuckles, and other flight control cables and turnbuckles at keel subframe 15A could result in chafing and damage, leading to fraying or seizing of the flight control cables, which could cause restriction or loss of flight controls.
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Required Actions
Perform a one-time detailed visual inspection for adequate clearances and damage as per SB.27-168. If clearances are outside limits or damage exceeds limits, repair or replace components prior to further flight. Alternative methods of compliance may be approved by the FAA.
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Compliance Time
Within 6 months after the effective date of this AD (July 9, 1996).
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Affected Aircraft
Beech (Raytheon) Model BAe 125 Series 1000A and Model Hawker 1000 airplanes listed in Hawker Service Bulletin SB.27-168, dated July 17, 1995.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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