AD 2000-22-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Various | Airworthiness Directives; Raytheon Model Hawker 800XP and Hawker 800 (U-125A) Series Airplanes |
Unsafe Condition
Chafing of the wire bundle exiting panel 'JA' due to insufficient clearance from the fuel cross-feed valve operating lever, which could result in a fire in the area of the fuel system in a confined space.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct a one-time detailed visual inspection of the panel 'JA' wire bundle to ensure correct routing and minimum clearance of 0.25-inch from the fuel cross-feed valve operating lever. If chafing is detected, repair the chafed wire and ensure correct routing and clearance. If the wire bundle is not correctly routed or clearance is insufficient, perform a detailed visual inspection for chafing and take corrective actions as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours or 6 months after the effective date of this AD, whichever comes first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Raytheon Model Hawker 800XP series airplanes listed in Raytheon Service Bulletin SB 24-3212, dated August 1999; and Hawker 800 (U-125A) series airplanes listed in Raytheon Service Bulletin SB 24-3213, dated February 2000, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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