AD 96-17-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 1000A | Airworthiness Directives; Beech (Raytheon) Model Hawker 1000 and BAe 125-1000A Series Airplanes |
| aircraft | Textron Aviation Inc. | Hawker 1000 | Airworthiness Directives; Beech (Raytheon) Model Hawker 1000 and BAe 125-1000A Series Airplanes |
Unsafe Condition
Failure of a fuel hose assembly on the auxiliary power unit (APU) due to heat damage caused by incorrect routing or bleed air leakage, which could result in a malfunction of the APU, a potential fuel fire in the fuselage rear bay, and reduced structural integrity of the surrounding structure.
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Required Actions
Within 30 days after May 23, 1995, perform inspections of the fuel feed hose assemblies, air leak detection system, and bleed air system per SB 49-44. Thereafter, daily inspections for fuel hose discolouration are required. Within 200 flight hours after this AD's effective date, replace the existing conduit with improved conduit per SB.49-47-25A825A to terminate prior inspection requirements.
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Compliance Time
Within 30 days after May 23, 1995 and within 200 flight hours after the effective date of this AD (September 24, 1996).
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Affected Aircraft
Beech (Raytheon) Model Hawker 1000 and BAe 125-1000A series airplanes post modification 259722C, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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