Airworthiness Directives; Boeing Model 747-400, 747-400D, and 747-400F Series Airplanes
airworthiness · Rule · Final rule. · Published 2006-09-08 · Effective 2006-10-13 · 71 FR 52999
Document
Document number
E6-14782
Federal Register citation
71 FR 52999
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2006-09-08
Effective date
2006-10-13
FAA docket
Docket No. FAA-2006-23873
Abstract
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747-400, 747-400D, and 747- 400F series airplanes. The existing AD currently requires reviewing airplane maintenance records; inspecting the yaw damper actuator portion of the upper and lower rudder power control modules (PCMs) for cracking, and replacing the PCMs if necessary; and reporting all airplane maintenance records review and inspection results to the manufacturer. This new AD expands the applicability and discontinues certain requirements of the existing AD. This AD adds repetitive inspections of the PCMs, and replacement of the PCMs if necessary. This AD results from manufacturer findings that the inspections required by the existing AD must be performed at regular intervals. We are issuing this AD to detect and correct cracking in the yaw damper actuator portion of the upper and lower rudder PCMs, which could result in an uncommanded left rudder hardover, consequent increased pilot workload, and possible runway departure upon landing.