Summary
We are adopting a new airworthiness directive (AD) for all Boeing Model 737-600, -700, -700C, -800, -900 and -900ER series airplanes. This AD requires repetitive testing of the rudder pedal forces or repetitive detailed inspections of the inner spring of the rudder feel and centering unit, and corrective actions if necessary. This AD also requires replacement of the spring assembly in the rudder feel and centering unit, which terminates the repetitive tests or inspections. This AD results from reports of low rudder pedal forces that were 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. We are issuing this AD to prevent reduced rudder pedal forces, which could result in increased potential for pilot-induced oscillations and reduce the ability of the flightcrew to maintain the safe flight and landing of the airplane.
Directive Details
AD Number
FAA-2009-0212
Document Number
E9-21412
Type
Rule
Publication Date
September 9, 2009
Effective Date
October 14, 2009
Affected Manufacturer
Boeing Model 737-600, -700, -700C, -800, -900 and -900ER Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2009-0212
Topics
Official Documents
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