AD 2003-06-06

final rule
Data completeness: 70%

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

AD Number
2003-06-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-18-AD
FR Citation
68 FR 14530

Applicability

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

Unsafe Condition

Failure of certain attachment bolts due to manufacturing discrepancies, which could result in reduced structural integrity of the airplane and loss of system function for flaps, controls, and landing gear.

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

Required Actions

Inspect the bolts installed at certain locations in the wing or fuselage. Take corrective actions if necessary.

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

Compliance Time

Within 50 flight hours after the effective date of the AD.

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

Affected Aircraft

Raytheon Model Hawker 800XP and 800 (including variant U-125A) 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.