AD 2004-17-02

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes

AD Number
2004-17-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2004-CE-04-AD
FR Citation
69 FR 51549

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Aircraft Company 65 Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes

Unsafe Condition

Loose bolts not securing the pedestal cross shaft, which could result in limited effectiveness of the control levers and lead to an aborted takeoff.

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

Required Actions

Repetitively inspect the engine controls/cross shaft/pedestal for proper installation and torque, re-torque the cross shaft attach bolt, modify the pedestal, and replace the engine controls cross shaft hardware. Modification of the pedestal and replacement of the hardware terminate the repetitive inspection requirements.

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 this AD.

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

Affected Aircraft

Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series airplanes, with specific model and serial number ranges listed in the AD.

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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