AD 2004-25-15

final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Aircraft Company, Model 390, Premier 1 Airplanes

AD Number
2004-25-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA 2004-19119
FR Citation
69 FR 75223

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Aircraft Company Airworthiness Directives; Raytheon Aircraft Company, Model 390, Premier 1 Airplanes

Unsafe Condition

Damage to the left and/or right main landing gear (MLG) wire harness assemblies, which resulted in various system failures/anomalies due to erroneous air/ground status signals.

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

Required Actions

Inspect the routing and security of the left and right main landing gear (MLG) squat switch wire harness installations for damage. Repair any damage or replace components, and reinstall the squat switch wire harness. For specific serial numbers, also inspect the squat switch bracket for corrosion or cracking and replace if damaged.

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

Compliance Time

Within 30 days after the effective date of this AD, January 18, 2005.

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

Affected Aircraft

Raytheon Aircraft Company, Model 390 Premier I airplanes with serial numbers RB-1, RB-4 through RB-84, RB-87 through RB-90, RB-92 through RB-96, RB-99 through RB-101, and RB-103 through RB-106.

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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