AD Amdt-39-9913
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Hawker 800 and 1000 and Model DH/BH/HS/BAe 125 | Airworthiness Directives; Raytheon Model Hawker 800 and 1000 and Model DH/BH/HS/BAe 125 Series Airplanes (Including Major Variants C29A, U125, and U125A Series Airplanes) |
Unsafe Condition
Fatigue fracturing of the sidestay jack pivots of the main landing gear (MLG) could result in inability of the MLG to deploy and a consequent wheels-up landing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace sidestay jack pivot assemblies with new, improved assemblies to terminate inspection requirements. Previously required repetitive inspections to detect fatigue cracking are no longer needed after replacement.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Raytheon Model BAe 125-1A through -1000A series, Model Hawker 800 and 1000, including variants C29A, U125, and U125A series 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.