AD 2003-04-20

final rule
Data completeness: 70%

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

AD Number
2003-04-20
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-15-AD
FR Citation
68 FR 9521

Applicability

TypeManufacturerModelDetails
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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