AD 2003-04-20
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | DH | Airworthiness Directives; Raytheon Model DH.125, HS.125, and BH.125 Series Airplanes; Model BAe.125 Series 800A, 800A (C-29A), 800A (U-125), 800B, 1000A, and 1000B Airplanes; and Model Hawker 800, 800 (including variant U-125A), 1000, and 800XP Airplanes |
Unsafe Condition
Separation of the cylinder head lugs of the main landing gear (MLG) actuator, which could prevent the MLG from extending and result in a partial gear-up landing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the cylinder head lugs of the main landing gear actuator for cracking or corrosion. Perform follow-on/corrective actions as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance time specified in the existing AD, with clarified compliance times for certain airplanes as outlined in this amendment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Raytheon Model DH.125, HS.125, BH.125, and BAe.125 (U-125 and C-29A) series airplanes; Model Hawker 800, Hawker 800 (including variant U-125A), Hawker 800XP, and Hawker 1000 airplanes.
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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