AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (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.
Eagle X-TS Series Aeroplanes
AD/X-TS/7 Co-Pilot Rudder Pedal Assembly 1/2005
TX
Applicability: Eagle Aircraft Model X-TS Manufacturer’s Serial Number (MSN) 001-010; and Model X-TS 150 MSN 011-015; and
Model X-TS 150B MSN 016-042.
Requirement: Remove the co-pilot rudder pedal assembly P/N 2720D07-02 and accomplish the Eagle Aircraft Mandatory Service Bulletin (MSB) 1095 dated 16 September 2003. Install placard as per paragraph 8.2 of the MSB 1095.
OR
Install new bush P/N 2720D08-39, stopper P/N 2720D08-44 and rework existing co- pilot rudder pedal assembly P/N 2720D07-02 as per provisions of Eagle Aircraft Service Bulletin (SB) 1096 dated 16 September 2003. [Only for Eagle aircraft model X-TS, ream the hole as per provisions of the SB 1113 if required, for the installation of the new bush].
OR
Replace with new co-pilot rudder pedal assembly P/N 2720D07-10 as per provisions of the SB 1097 dated 16 September 2003.
Note: Department of Civil Aviation Malaysia Airworthiness Directives CAM AD 001-10-2004 dated 30 October 2004 (for model X-TS) and CAM AD 002-10-2004 dated 30 October 2004 (for models X-TS 150 & 150B) refer.
Compliance: Unless accomplished earlier, before further flight.
This Airworthiness Directive becomes effective on 18 November 2004.
Eagle X-TS Series Aeroplanes
AD/X-TS/7 (continued)
Background: Two incidents of loss of rudder control have been reported that involved binding of the rudder control pushrod pivot onto the pivot arms. Such binding may cause loss of co-pilot rudder and brake control creating an unsafe condition and catastrophic consequences.
This Airworthiness Directive addresses the identified unsafe condition.
James Coyne
Delegate of the Civil Aviation Safety Authority 16 November 2004
The above AD is notified in the Commonwealth of Australia Gazette on 18 November 2004.
Overview
The Airworthiness Directive AD/X-TS/7, issued in 2004 under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998, was enacted to address a critical safety issue in the Eagle X-TS Series aeroplanes. Specifically, the directive targets the co-pilot rudder pedal assembly in certain models of the Eagle X-TS, where incidents of loss of rudder control due to binding of the rudder control pushrod pivot had been reported. Such binding could potentially lead to the loss of co-pilot rudder and brake control, creating an unsafe condition with potentially catastrophic consequences. The directive was issued by the Civil Aviation Safety Authority (CASA) delegate, James Coyne, and is intended to ensure that corrective actions are taken before further flight, thereby enhancing aviation safety. This Airworthiness Directive became effective on 18 November 2004.
Scope and Application
The Airworthiness Directive (AD) issued under the Civil Aviation Regulations 1998 targets specific models of Eagle X-TS Series aeroplanes to address a safety concern related to the co-pilot rudder pedal assembly. The AD applies to Eagle Aircraft with specific Manufacturer’s Serial Numbers (MSN), namely, Model X-TS MSN 001-010, Model X-TS 150 MSN 011-015, and Model X-TS 150B MSN 016-042. The directive mandates actions to rectify the unsafe condition identified, which includes the removal or modification of the co-pilot rudder pedal assembly or installation of specific parts as per Eagle Aircraft's Service Bulletins. The directive applies nationally across the Commonwealth of Australia and requires compliance before further flight. The AD was published in the Commonwealth of Australia Gazette on 18 November 2004 and became effective on the same date.
Key Provisions
The Airworthiness Directive (AD/X-TS/7) issued under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998, mandates specific actions for the specified Eagle Aircraft X-TS series aeroplanes (sections 1 and 2). The AD applies to the co-pilot rudder pedal assembly on Eagle X-TS series aeroplanes, specifically those with Manufacturer’s Serial Numbers (MSN) 001-010, MSN 011-015 for model X-TS 150, and MSN 016-042 for model X-TS 150B. The directive requires the removal of the co-pilot rudder pedal assembly P/N 2720D07-02 and the implementation of Eagle Aircraft Mandatory Service Bulletin (MSB) 1095 dated 16 September 2003, or the installation of new components and reassembly according to the provisions of Service Bulletin (SB) 1096, or the replacement with a new co-pilot rudder pedal assembly P/N 2720D07-10 as per SB 1097, all dated 16 September 2003. Additionally, if applicable, the SB 1113 provisions must be followed for the installation of the new bush.
The AD imposes several obligations on the aircraft owners or operators, such as ensuring the specified maintenance actions are carried out on the affected aircraft. Specifically, they must comply with the instructions detailed in the relevant service bulletins (SB 1095, 1096, 1097, and 1113). This includes removing and replacing parts, reassembling components, and installing placards as specified. These actions must be completed before the aircraft can be flown further. The AD also mandates that these actions be taken in accordance with the compliance timeline, which requires completion before further flight, and it became effective on 18 November 2004.
Failure to comply with this Airworthiness Directive can lead to serious consequences. While the specific penalties are not detailed in the text, non-compliance with ADs generally results in civil penalties, including fines, and potentially criminal charges if the non-compliance leads to accidents or unsafe conditions. The maximum penalties can vary but typically include significant fines and imprisonment for individuals found guilty of non-compliance. The directive is backed by the authority of the Civil Aviation Safety Authority (CASA) delegate, James Coyne, and references other airworthiness directives issued by the Department of Civil Aviation Malaysia to reinforce the importance and urgency of the actions required.