AD/B737/201 Amdt 2 Rudder Control System (Cth)
AIRWORTHINESS DIRECTIVE
On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/B737/201 Amdt 1 and issues the following AD under subregulation 39.001(1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Boeing 737 Series Aeroplanes
| AD/B737/201 Amdt 2 | Rudder Control System | 7/2007 |
Applicability: | All Model 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, and -900 series aircraft. |
Requirement: | Action in accordance with the technical requirements of FAA AD 2007-03-07 Amdt 39-14918. |
Compliance: | As specified in the Requirement document, with a revised effective date of |
| This Amendment becomes effective on 5 July 2007. | |
Background: | The FAA has made determinations that the existing rudder control system design architecture is unsafe due to inherent failure modes, including single-jam modes and certain latent failures or jams, which, when combined with a second failure or jam, could cause an uncommanded rudder hardover event and consequent loss of control of the aircraft. Additionally, the current rudder operational procedure is not effective throughout the entire flight envelope. The actions specified by this Directive are intended to prevent the identified unsafe condition. Amendment 1 was issued in response to a new FAA AD, which was prompted by a report of a fractured rod end of an input control rod of the main rudder power control unit (PCU) and a subsequent report of a fractured rod end of the input control rod of the standby rudder PCU. The additional actions required by this Directive for certain aircraft, are intended to prevent failure of one of the two input control rods of the main rudder PCU, which, under certain conditions, could result in reduced controllability of the aircraft; and to prevent failure of any combination of two input control rods of the main rudder PCU and/or standby rudder PCU, which could cause an uncommanded rudder hardover event and result in loss of control of the aircraft. Amendment 2 is issued to correct a minor typographical error in the Compliance paragraph only. |
| Amendment 1 of this Airworthiness Directive became effective on 12 April 2007. |
David Villiers
Delegate of the Civil Aviation Safety Authority
24 May 2007
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