AD 2009-19-02

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, -900 and -900ER Series Airplanes

AD Number
2009-19-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2009-0212
FR Citation
74 FR 46324

Applicability

TypeManufacturerModelDetails
aircraft Boeing 737-600 Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, -900 and -900ER Series Airplanes

Unsafe Condition

Reports of low rudder pedal forces caused by a broken inner spring in the rudder feel and centering unit. A broken inner spring in conjunction with a broken outer spring would significantly reduce rudder pedal forces.

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

Required Actions

Repetitive testing of the rudder pedal forces or repetitive detailed inspections of the inner spring of the rudder feel and centering unit, with corrective actions if necessary. Replacement of the spring assembly in the rudder feel and centering unit to terminate the repetitive tests or inspections.

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

All Boeing Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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