AD 2000-24-25

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Model Hawker 800A (U-125A) and Hawker 800XP Series Airplanes

AD Number
2000-24-25
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-03-AD
FR Citation
65 FR 77259

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Various Airworthiness Directives; Raytheon Model Hawker 800A (U-125A) and Hawker 800XP Series Airplanes

Unsafe Condition

Excessive clearance of the roller in the drag stay rigging of the nose landing gear, which could result in the inability to extend the nose landing gear and damage to the airplane upon landing.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Within 50 hours time-in-service after the effective date, remove paint from the drag stay arm at its point of contact with the stop bolt, inspect roller clearances, and make necessary adjustments in accordance with Raytheon Aircraft Service Bulletin SB 32-3274.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 50 hours time-in-service after the effective date.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Raytheon Model Hawker 800A (U-125A) and Hawker 800XP series airplanes, as specified in Raytheon Aircraft Service Bulletin SB 32-3274, dated August 1999, 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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